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Sample records for boeing company usa

  1. 78 FR 23866 - Airworthiness Directives; the Boeing Company

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-23

    ... Directives; the Boeing Company AGENCY: Federal Aviation Administration (FAA), Department of Transportation... (NPRM) that proposed a new airworthiness directive (AD) for certain The Boeing Company Model 777-200...

  2. 77 FR 69739 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-11-21

    ...-212-AD; Amendment 39-17238; AD 2012-22-02] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 747-400, -400D, and -400F series...): 2012-22-02 The Boeing Company: Amendment 39-17238; Docket No. FAA- 2012-0498; Directorate...

  3. 78 FR 72564 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-03

    ...-135-AD; Amendment 39-17684; AD 2013-24-10] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 757 and Model 767 airplanes...): 2013-24-10 The Boeing Company: Amendment 39-17684; Docket No. FAA- 2012-1229; Directorate...

  4. 78 FR 6254 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-30

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company... directive (AD) for all The Boeing Company Model 737-300, -400, and -500 series airplanes. That NPRM proposed... all The Boeing Company Model 737-300, -400, and -500 series airplanes. That NPRM published in...

  5. 78 FR 22215 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-15

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company... Boeing Company Model 757 series airplanes equipped with Rolls-Royce RB211 engines. The existing AD..., 2004), and adding the following new AD: The Boeing Company: Docket No. FAA-2013-0326;...

  6. 77 FR 34876 - Airworthiness Directives; The Boeing Company

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-12

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company...: We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 777.... 39.13 by adding the following new airworthiness directive (AD): The Boeing Company: Docket No....

  7. 78 FR 72558 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-03

    ...-194-AD; Amendment 39-17687; AD 2013-24-13] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 737-100, -200, -200C, -300, -400... airworthiness directive (AD): 2013-24-13 The Boeing Company: Amendment 39-17687; Docket No. FAA-...

  8. 78 FR 38550 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-06-27

    ...-226-AD; Amendment 39-17493; AD 2013-13-05] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for all The Boeing Company Model 747SP series airplanes, and certain The Boeing Company Model 747-100B SUD and 747-300 series airplanes. This AD was prompted by...

  9. 78 FR 6202 - Airworthiness Directives; the Boeing Company

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-30

    ...-191-AD; Amendment 39-17326; AD 2013-02-05] RIN 2120-AA64 Airworthiness Directives; the Boeing Company... airworthiness directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER...): 2013-02-05 The Boeing Company: Amendment 39-17326; Docket No. FAA-2011-0258; Directorate...

  10. 78 FR 52419 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-23

    ...-128-AD; Amendment 39-17555; AD 2013-16-17] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for all The Boeing Company Model 727, 727C, 727-100, 727-100C, 727... airworthiness directive (AD): 2013-16-17 The Boeing Company: Amendment 39-17555 ; Docket No. ]...

  11. 78 FR 6200 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-30

    ...-131-AD; Amendment 39-17328; AD 2013-02-07] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, -900...): 2013-02-07 The Boeing Company: Amendment 39-17328; Docket No. FAA-2012-0183; Directorate...

  12. 78 FR 22172 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-15

    ...-070-AD; Amendment 39-17412; AD 2013-07-08] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 757 airplanes. This AD was...): 2013-07-08 The Boeing Company: Amendment 39-17412; Docket No. FAA- 2011-1094; Directorate...

  13. 77 FR 75402 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-12-20

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company...). SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 757... directive (AD): The Boeing Company: Docket No. FAA-2012-1229; Directorate Identifier 2012-NM-135-AD....

  14. 78 FR 28729 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-16

    ...-172-AD; Amendment 39-17455; AD 2013-10-02] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... superseding an existing airworthiness directive (AD) for certain The Boeing Company Model 757-200 and -200PF... following new AD: 2013-10-02 The Boeing Company: Amendment 39-17455; Docket No. FAA- 2012-1109;...

  15. 78 FR 22178 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-15

    ...-094-AD; Amendment 39-17413; AD 2013-07-09] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 737-700, -700C, -800, and -900ER... The Boeing Company: Amendment 39-17413 ; Docket No. FAA- 2010-1042; Directorate Identifier...

  16. 78 FR 70851 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-11-27

    ...-209-AD; Amendment 39-17675; AD 2013-24-01] RIN 2120-AA64 Airworthiness Directives; The Boeing Company.... SUMMARY: We are adopting a new airworthiness directive (AD) for The Boeing Company Model 747-8 and 747-8F... The Boeing Company: Amendment 39-17675; Docket No. FAA- 2013-0974; Directorate Identifier...

  17. 78 FR 72561 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-03

    ...-241-AD; Amendment 39-17685; AD 2013-24-11] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 747-100, 747-100B, 747-100B SUD... airworthiness directive (AD): 2013-24-11 The Boeing Company: Amendment 39-17685; Docket No. FAA-...

  18. 78 FR 28767 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-16

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company...). SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 747... directive (AD): The Boeing Company: Docket No. FAA-2013-0420; Directorate Identifier 2011-NM-241-AD....

  19. 78 FR 8999 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-02-07

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company...). SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 747... airworthiness directive (AD): The Boeing Company: Docket No. FAA-2013-0089; Directorate Identifier...

  20. 77 FR 51724 - Airworthiness Directives; The Boeing Company

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-27

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company... directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, - 900, and -900ER series... apply to certain The Boeing Company Model 737-600, -700, -700C, - 800, -900, and -900ER series...

  1. 78 FR 72550 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-03

    ...-057-AD; Amendment 39-17681; AD 2013-24-07] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 707 airplanes; and Model 720 and... considered the comment received. The Boeing Company stated that it supports the NPRM (78 FR 49237, August...

  2. 78 FR 49379 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-14

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company...). SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 757... directive (AD): The Boeing Company: Docket No. FAA-2013-0693; Directorate Identifier 2013-NM-059-AD....

  3. 77 FR 73282 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-12-10

    ...-268-AD; Amendment 39-17278; AD 2012-24-08] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, -900... airworthiness directive (AD): 2012-24-08 The Boeing Company: Amendment 39-17278; Docket No. FAA-...

  4. 78 FR 22182 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-15

    ...-107-AD; Amendment 39-17411; AD 2013-07-07] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for all The Boeing Company Model 737-600, -700, -700C, -800, -900... The Boeing Company: Amendment 39-17411; Docket No. FAA- 2012-0933; Directorate Identifier...

  5. 78 FR 3365 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-16

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company...). SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Airplanes... holidays. For service information identified in this proposed AD, contact Boeing Commercial...

  6. 78 FR 52836 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-27

    ...-352-AD; Amendment 39-17529; AD 2013-15-13] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for all The Boeing Company Model 757 airplanes. This AD was prompted... October 1, 2013. ADDRESSES: For service information identified in this AD, contact Boeing...

  7. 78 FR 52838 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-27

    ...-354-AD; Amendment 39-17533; AD 2013-15-17] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, -900... information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services...

  8. 78 FR 22185 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-15

    ...-140-AD; Amendment 39-17415; AD 2013-07-11] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... superseding an existing airworthiness directive (AD) for certain The Boeing Company Model 777-200, -200LR... (74 FR 62217, November 27, 2009), and adding the following new AD: 2013-07-11 The Boeing...

  9. 78 FR 6251 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-30

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company...). SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 767... FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): The Boeing...

  10. 78 FR 6247 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-30

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; the Boeing Company... Company Model 757 airplanes. The existing AD currently requires revising the maintenance program by..., 2012), for all The Boeing Company Model 757 airplanes. That AD superseded AD 2008-10-11, Amendment...

  11. 78 FR 43839 - Airworthiness Directives; the Boeing Company

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-22

    ... Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; the Boeing Company... Company Model 747 series airplanes. The existing AD currently requires repetitive detailed inspections to..., 1994), and adding the following new AD: The Boeing Company: Docket No. FAA-2013-0625;...

  12. 76 FR 68666 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-11-07

    ... Airworthiness Directives; The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT... (AD) for certain The Boeing Company Model 737-100, -200, -200C, and -300 series airplanes. This proposed AD was prompted by a report from the airplane manufacturer that airplanes were assembled with...

  13. 78 FR 13463 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-02-28

    ...-042-AD; Amendment 39-17284; AD 2012-25-03] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to certain The Boeing Company Model 757 airplanes. That AD incorrectly identified certain...

  14. 78 FR 12231 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-02-22

    ...-016-AD; Amendment 39-17366; AD 2013-02-51] RIN 2120-AA64 Airworthiness Directives; The Boeing Company.... SUMMARY: We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 787-8 airplanes. This emergency AD was sent previously to all known U.S. owners and operators of these...

  15. 77 FR 26945 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-05-08

    ...-058-AD; Amendment 39-17041; AD 2012-09-06] RIN 2120-AA64 Airworthiness Directives; The Boeing Company... new airworthiness directive (AD) for certain The Boeing Company Model 737-700 series airplanes. This AD was prompted by reports that the aft seat leg fittings span the station (STA) 521.45...

  16. 78 FR 23691 - Airworthiness Directives; the Boeing Company

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-22

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; the Boeing Company... airworthiness directive (AD) for certain The Boeing Company Model 777-200 series airplanes. The proposed...

  17. 78 FR 23685 - Airworthiness Directives; The Boeing Company

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-22

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company... airworthiness directive (AD) for certain The Boeing Company Model 777-200 and -300 series airplanes....

  18. 78 FR 23690 - Airworthiness Directives; The Boeing Company

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-22

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; The Boeing Company... airworthiness directive (AD) for certain The Boeing Company Model 777-200 series airplanes. The proposed...

  19. 77 FR 55681 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-11

    ... Material of the Components of the Horizontal Stabilizer For airplanes identified in Boeing 707 Alert...-17176; AD 2012-17-13] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY... -100B short body series airplanes; Model 707-300, -300B, -300C, and - 400 series airplanes; and...

  20. 78 FR 27020 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-09

    ...-186-AD; Amendment 39-17429; AD 2012-18-13 R1] RIN 2120-AA64 Airworthiness Directives; The Boeing... revising an existing airworthiness directive (AD) for all The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series ] airplanes. That AD currently requires repetitive inspections to...

  1. 76 FR 77937 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-15

    ...). SUMMARY: We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model 777... lower housing to verify that the cross bolts are correctly installed and that there are no missing fuse..., contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC...

  2. 76 FR 66200 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-10-26

    .... Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2011-1094... following new airworthiness directive (AD): The Boeing Company: Docket No. FAA-2011-1094;...

  3. The Boeing Company's Manufacturing Technology Student Internship. Evaluation Report.

    ERIC Educational Resources Information Center

    Owens, Thomas R.

    The Boeing Company contracted with the Northwest Regional Educational Laboratory to evaluate its student internship program, part of a "school-to-work" effort modeled after the nationally recognized Tech Prep initiative. The company's involvement in the Tech Prep Program has been implemented in three phases: (1) the initial phase helped…

  4. 77 FR 21429 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-10

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 777 airplanes. This AD was... these airplanes. DATES: This AD is effective May 15, 2012. The Director of the Federal Register...

  5. 78 FR 57542 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-19

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM... Boeing Company Model 777-200 and -300 series airplanes. AD 2012-12-08 requires an inspection for the part... determined that additional airplanes may be subject to the identified unsafe condition. This proposed...

  6. 78 FR 25374 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-01

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2012-1073; Directorate Identifier 2012-NM...): 2013-08-13 The Boeing Company: Amendment 39-17430; Docket No. FAA- 2012-1073; Directorate...

  7. 77 FR 47330 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-08

    ... to supersede an existing airworthiness directive (AD) that applies to certain The Boeing Company Model 767-200, -300, -300F, and - 400ER series airplanes. The proposed AD would have continued to... installed, and related investigative and corrective actions if necessary. That proposed AD would have...

  8. 77 FR 3587 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-25

    ... new airworthiness directive (AD) for certain Model 767-200 and 767-300 series airplanes. This AD was... potential loss of several functions essential for safe flight. DATES: This AD is effective February 29, 2012...) Applicability This AD applies to The Boeing Company Model 767-200 and 767-300 series airplanes, certificated...

  9. 76 FR 76066 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-06

    ... certain The Boeing Company Model 777 airplanes. This proposed AD was prompted by reports of corrosion... pins with new or reworked pivot pins having improved corrosion resistance, doing repetitive inspections... received reports of corrosion damage on the outer diameter chrome surface of the horizontal...

  10. 78 FR 27310 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-10

    ...-essential electrical systems through a switch in the flight compartment in the event of smoke or flames. In... the passenger cabin, a switch is needed in the flight compartment to enable the flightcrew to turn off... utility bus switch; and doing other specified actions. For the Boeing Company Model 737-300, -400,...

  11. 78 FR 21576 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-11

    ...). SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 757...: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206- 544... invite you to send any written relevant data, views, or arguments about this proposal. Send your...

  12. 78 FR 65185 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-31

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 727 airplanes. This AD...

  13. 77 FR 1618 - Special Conditions: The Boeing Company, Model 767-300; Seats With Inflatable Lapbelts

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-11

    ... Federal Aviation Administration 14 CFR Part 25 Special Conditions: The Boeing Company, Model 767-300... conditions; request for comments. SUMMARY: These special conditions are issued for the Boeing Model 767- 300... for the installation of inflatable lapbelts on ] Boeing Model 767-300 series airplanes. The Model...

  14. 77 FR 71723 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-12-04

    ... Boeing Service Bulletin 737-52-1079. Or, (2) Those airplanes on which the door assembly having P/N 65... cargo door, in accordance with Boeing Service Bulletin 737-52-1079, Revision 5, dated May 16, 1996... frame and the cross beams of the aft cargo door, in accordance with Boeing Service Bulletin...

  15. 78 FR 47549 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-06

    ... been modified as specified in Boeing Service Bulletin 737-52-1079. Or, (2) Those airplanes on which the... cross beams of the aft cargo door, in accordance with Boeing Service Bulletin 737-52-1079, Revision 5... Bulletin 737-52-1079, Revision 5, dated May 16, 1996; Boeing Alert Service Bulletin 737-52A1079, Revision...

  16. Technology transfer personnel exchange at the Boeing Company

    SciTech Connect

    Antoniak, Z.I.

    1993-03-01

    The objective of the exchange was to transfer Pacific Northwest Laboratory (PNL) technology and expertise in advanced ceramic fabric composites (ACFC) to the Boeing Defense Space Group (Boeing Aerospace). Boeing Aerospace was especially interested in applying PNL-developed ACFC technology to its current and future spacecraft and space missions. Boeing has on-going independent research and development (R D) programs on advanced radiators and heat pipes, therefore, PNL research in ceramic fabric heat pipes was of particular interest to Boeing. Thus, this exchange assisted in the transfer of PNL's ACFC heat pipe technology and other, related research capabilities to private industrial application. The project was proposed as an initial step in building a long-term collaborative relationship between Boeing and PNL that may result in future Cooperative Research and Development Agreements (CRADAs) and/or other types of collaborative efforts.

  17. Technology transfer personnel exchange at the Boeing Company

    SciTech Connect

    Antoniak, Z.I.

    1993-03-01

    The objective of the exchange was to transfer Pacific Northwest Laboratory (PNL) technology and expertise in advanced ceramic fabric composites (ACFC) to the Boeing Defense & Space Group (Boeing Aerospace). Boeing Aerospace was especially interested in applying PNL-developed ACFC technology to its current and future spacecraft and space missions. Boeing has on-going independent research and development (R&D) programs on advanced radiators and heat pipes, therefore, PNL research in ceramic fabric heat pipes was of particular interest to Boeing. Thus, this exchange assisted in the transfer of PNL`s ACFC heat pipe technology and other, related research capabilities to private industrial application. The project was proposed as an initial step in building a long-term collaborative relationship between Boeing and PNL that may result in future Cooperative Research and Development Agreements (CRADAs) and/or other types of collaborative efforts.

  18. 77 FR 7521 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-13

    ... report of a rudder hard-over event on a Model 747-400 series airplane, caused by a rudder power control... condition could result in a hard-over of the rudder surface leading to an increase in pilot workload and a... surface hard-over. Boeing pointed out that the secondary retention device incorporated in Boeing...

  19. 78 FR 14734 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-07

    ... conclusively determines the serial number of the horizontal stabilizer. STC Winglet Comment Aviation Partners Boeing stated that the installation of winglets per Supplemental Type Certificate (STC) ST00830SE...

  20. 77 FR 31762 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-05-30

    ... Part Surface Inspection (Impedance Plane Display), of Part 6, Eddy Current, of the Boeing 707, 720... Subject 51-00-00 Figure 24, Steel Part Surface Inspection (Impedance Plane Display), of Part 6,...

  1. 78 FR 42411 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-16

    ... correct an acronym from ``TFE'' to ``PTFE.'' Boeing stated that the proper acronym for polytetrafluoroethylene is ``PTFE.'' We disagree with changing the acronym in this AD. The service information required...

  2. 77 FR 26993 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-05-08

    ... require replacing titanium seat track bolts with corrosion resistant steel (CRES) bolts, repetitive... procedures for replacing titanium seat track bolts with CRES bolts, repetitive inspections for cracking of... include contacting Boeing for repair instructions, repairing, replacing missing or severed titanium...

  3. The Boeing Company Applied Academics Project Evaluation: Year Four. Evaluation Report.

    ERIC Educational Resources Information Center

    Wang, Changhua; Owens, Thomas R.

    This paper describes fourth-year outcomes (1993-94) of the Boeing Company-funded Applied Academics Project. Since the 1990-91 school year, the company has provided funds to improve and expand applied academics in 60 Washington high schools. Data were collected from pre- and post-surveys of students enrolled in the project's Applied Mathematics…

  4. 78 FR 61388 - TA-W-82,705, the Boeing Company Boeing Commercial Aircraft, (BCA) Including On-Site Leased...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-03

    ...) Including On-Site Leased Workers From Chipton Ross, Inc., CTS Technical Services, Inc., Moseley Technical... Workers From Adecco, USA, Inc., Cascade Engineering, CDI Corporation, Chipton Ross, Inc., Comforce... Boeing Commercial Aircraft, (BCA) Including On-Site Leased Workers From Adecco USA, Inc., Chipton...

  5. 77 FR 5996 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-07

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are adopting a... series airplanes. This AD was prompted by a report from the airplane manufacturer that airplanes were assembled with air distribution ducts in the environmental control system (ECS) wrapped with Boeing...

  6. 78 FR 20229 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-04

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are..., -800, -900, and -900ER series airplanes. That AD currently requires repetitive inspections of the aft... Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle,...

  7. 78 FR 21236 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-10

    ..., August 16, 2012) on Winglets Aviation Partners Boeing (APB) stated that it has reviewed the NPRM (77 FR... that the installation of winglets, per Supplemental Type Certificate (STC) ST01518SE, ``does not affect them.'' We infer that APB means the installation of these winglets does not affect accomplishing...

  8. 77 FR 61542 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-10

    ... flange of the inboard track at the rear spar attachment of each outboard flap, and eventual rework of the... the rear spar attachment of each outboard flap, and eventual rework of the flap track assembly and..., repair or rework the flap track per the ``Repair and Rework Instructions'' specified in Boeing AOM...

  9. 78 FR 33193 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-06-04

    ... hidden parts of the airplane. The FAA made this safety determination based on tests of aged BMS 8-39... (such as the installation of felt on Model 767 airplanes per Figure 18 of Boeing Special Attention... retardant properties, which deteriorate over time, can provide a fuel source for an ignition event in...

  10. 78 FR 52875 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-27

    ... fillet radius of the rib chord, and a large repair or preventive modification if necessary... repetitive inspections for cracks along the upper fillet radius of the rib chord. Boeing Service Bulletin 727..., and do a detailed (close visual) inspection for cracking along the upper fillet radius of the...

  11. 77 FR 64711 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-23

    ... Nesemeier, Senior Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft... on the SNPRM (77 FR 31758, May 30, 2012) and the FAA's response to each comment. Support for the SNPRM (77 FR 31758, May 30, 2012) Boeing supports the SNPRM (77 FR 31758, May 30, 2012). Requests To...

  12. 77 FR 36139 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-18

    ... significant economic impact, positive or negative, on a substantial number of small entities under the... current inspections for cracking of the frame, HFEC inspections for cracking of the reinforcement angle..., and reinforcement angle, in accordance with the Accomplishment Instructions of Boeing Alert...

  13. 78 FR 59304 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-26

    ... plastic tie straps, and inspecting for and repairing damaged wire bundles. We are proposing this AD to... each metal clamp with a plastic tie strap. While Boeing Service Bulletin 737-21-1186, dated April 17.... If any metal clamp is found installed, before further flight, replace each metal clamp with a...

  14. 78 FR 38608 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-06-27

    ... result in uncontrolled decompression. DATES: We must receive comments on this proposed AD by August 12... result in uncontrolled decompression. Relevant Service Information We reviewed Boeing Alert Service... unsafe condition described previously is likely to exist or develop in other products of the same...

  15. 78 FR 40050 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-03

    ... reports of skin wear damage on airplanes on which Boeing Material Specifications (BMS) 10-86 Teflon-filled... ] inspection interval specified in AD 2009-14-02. The wear occurred through both the Teflon filled coating and... per 10-86 Teflon-filled coating per hour = $680 cycle. inspection cycles. [retained actions...

  16. 78 FR 68693 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-11-15

    ... supplemental type certificate (STC) ST00830SE ( http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0... track bolt and splice part kits when frame replacements are required. The commenter stated that Boeing... found missing from the structure during the accomplishment of the tasks required by paragraph (g)...

  17. 78 FR 33012 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-06-03

    ..., or because of isolated situations or incidents such as material defects, poor fabrication quality, or... AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H... availability of this material at the FAA, call 425-227-1221. Examining the AD Docket You may examine the...

  18. 78 FR 31389 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-24

    ... ``New Inspections and Corrective Actions to Ensure Cross Beam Reinforcement,'' and suggested language... door. Boeing added that the current language in the NPRM and this service information leave open the..., and (4) Will not have a significant economic impact, positive or negative, on a substantial number...

  19. 77 FR 41934 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-17

    ... loss of boost pump pressure of the fuel feed system, followed by loss of fuel system suction feed..., which in the event of total loss of the fuel boost pumps could result in dual engine flameout, inability... previous NPRM during maintenance operations. Relevant Service Information We reviewed Boeing Alert...

  20. 78 FR 73460 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-06

    ... driven pump (ADP) turbine gearbox assembly (TGA), which resulted in the release of high energy fragments... striking passengers, or penetrating the wing-to-body fairing and striking ground handling or maintenance... maintenance personnel, causing serious injury. Relevant Service Information We reviewed Boeing...

  1. 77 FR 39188 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-02

    ... number 989. CAL stated that, in the Boeing 767 Airplane Maintenance Manual there are two fuel pump wire... sleeves of the fuel tank boost pumps and override/jettison pumps; replacement of the sleeves with new... proposing this supplemental NPRM to detect and correct chafing of the fuel pump wire insulation...

  2. 77 FR 36206 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-18

    ..., -200LR, -300, and -300ER series airplanes. This proposed AD was prompted by reports of in-service events related to electrical power system malfunctions resulting in damage to electrical load management system... Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H-65,...

  3. 77 FR 10411 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-22

    ... to sustain limit flight and pressure loads. DATES: We must receive comments on this proposed AD by... pressure loads. Relevant Service Information We reviewed Boeing Alert Service Bulletin 777-53A0043, dated.... operators Inspections for Group 1 126 work-hours x $0 $10,710 per $267,750 per inspection cycle....

  4. 77 FR 3579 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-25

    ... proximity switch, and testing to ensure positive door locking and corrective action if necessary. For... assembly, relocating and adjusting the sensor target and the sensor proximity switch, and testing to ensure... switch on the new bracket in accordance with the Accomplishment Instructions of Boeing Service...

  5. 77 FR 52212 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-29

    ... Delta requested that the exceptions to certain compliance times in paragraph (p)(2) of the NPRM (76 FR..., 2011) and the FAA's response to each comment. Request To Add Compliance Time for Group 2 Airplanes... a 90-day compliance time for airplanes in Group 2. The commenter stated that Boeing...

  6. 77 FR 54850 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-06

    ..., inspecting certain fasteners in the fuel tanks and determining the method of attachment of the vortex... of attachment of the vortex generators, and corrective action if necessary. That AD resulted from... inspecting the vortex generator attachment. Boeing has since revised this service bulletin. We have...

  7. 76 FR 62661 - Airworthiness Directives; The Boeing Company Model 767-200 and -300 Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-10-11

    ... Model 767-200 and - 300 Series Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION... certain Model 767-200 and 767-300 series airplanes. This proposed AD would require installing cargo... (b) None. Applicability (c) This AD applies to The Boeing Company Model 767-200 and 767- 300...

  8. 76 FR 1979 - Airworthiness Directives; The Boeing Company Model 757 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-01-12

    ... certification basis of the airplane, and the approval must specifically refer to this AD. Material Incorporated...-16576; AD 2011-02-03] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Model 757 Airplanes... -300 series airplanes. This AD requires an inspection of the two spring arms in the spin...

  9. The Boeing Company's Manufacturing Technology Student Internship. Evaluation Report (1994-95).

    ERIC Educational Resources Information Center

    Wang, Changhua; Owens, Thomas R.

    An evaluation was conducted of the Boeing Company's summer internship program for students enrolled in a manufacturing technology program after grades 11, 12, and 13 (first year of community college). The evaluation included the following activities: a review of documents describing the internship structure, student selection process, and…

  10. The Boeing Company's Manufacturing Technology Student Internship. Final Evaluation Report for 1996.

    ERIC Educational Resources Information Center

    Owens, Tom

    A study evaluated The Boeing Company's Student Internship Program for students enrolled in a manufacturing technology program. The programs in the Seattle (Washington) and Portland (Oregon) areas provided students with three progressive internship levels offered in the summers of grades 11, 12, and 13 (the first year of community college). The…

  11. 75 FR 38001 - Airworthiness Directives; The Boeing Company Model 747 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-07-01

    ...-073-AD; Amendment 39-16352; AD 2010-14-07] RIN 2120-AA64 Airworthiness Directives; The Boeing Company...). ACTION: Final rule. SUMMARY: The FAA is superseding an existing airworthiness directive (AD), which applies to certain Model 747 airplanes. That AD currently requires repetitive inspections of the...

  12. 76 FR 63163 - Airworthiness Directives; The Boeing Company Model 777-200, -200LR, -300, and -300ER Series...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-10-12

    ..., -300, and -300ER Series Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final... Boeing Company Model 777-200, -200LR, -300, and -300ER series airplanes; certificated in any category;...

  13. 77 FR 12166 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-29

    ... Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are... series airplanes. That AD currently requires inspecting certain power feeder wire bundles for damage... certain airplanes. This AD was prompted by a report that a power feeder wire bundle chafed against...

  14. 78 FR 12991 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-02-26

    ... Company Model 767 airplanes. One AD currently requires a functional check of the shear rivets in all six elevator power control actuator (PCA) bellcrank assemblies to determine the condition of the shear rivets... to prevent continued operation with yielded or failed shear rivets in the elevator PCA...

  15. 76 FR 10288 - Airworthiness Directives; The Boeing Company Model 767-200, -300, -300F, and -400ER Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-02-24

    ... Model 767-200, -300, -300F, and -400ER Series Airplanes AGENCY: Federal Aviation Administration (FAA... airworthiness directive (AD) that applies to The Boeing Company Model 767-200, -300, and -300F series airplanes..., October 5, 2005), for certain Model 767-200, -300, and -300F series airplanes. That AD...

  16. 75 FR 25124 - Airworthiness Directives; The Boeing Company Model 737-200, -300, -400, and -500 Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-05-07

    ... Model 737-200, -300, -400, and -500 Series Airplanes AGENCY: Federal Aviation Administration (FAA), DOT... (AD) for certain Model 737-200, -300, -400, and -500 series airplanes. This proposed AD would require...) None. Applicability (c) This AD applies to The Boeing Company Model 737-200, -300, - 400, and...

  17. 76 FR 2846 - Airworthiness Directives; The Boeing Company Model 777-200, -200LR, -300, and -300ER Series...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-01-18

    ... Company Model 777-200, - 200LR, -300, and -300ER Series Airplanes AGENCY: Federal Aviation Administration... Attention Service Bulletin 777-29-0032, dated August 9, 2007 (for Model 777-200, -200LR, -300, and -300ER..., -200LR, -300, and -300ER airplanes that require rubber FOD shields). Boeing Special Attention...

  18. 75 FR 17889 - Airworthiness Directives; The Boeing Company Model 777-200, -200LR, -300, and -300ER Series...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-04-08

    ... Model 777-200, - 200LR, -300, and -300ER Series Airplanes AGENCY: Federal Aviation Administration (FAA... directive (AD) for certain Model 777-200, -200LR, -300, and -300ER series airplanes. This proposed AD would...) This AD applies to The Boeing Company Model 777-200, -200LR, -300, and -300ER series...

  19. Site Environmental Report for Calendar Year 1999. DOE Operations at The Boeing Company, Rocketdyne

    SciTech Connect

    2000-09-01

    OAK A271 Site Environmental Report for Calendar Year 1999. DOE Operations at The Boeing Company, Rocketdyne. This Annual Site Environmental Report (ASER) for 1999 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of the Rocketdyne Santa Susana Field Laboratory (SSFL). In the past, these operations included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials under the former Atomics International Division. Other activities included the operation of large-scale liquid metal facilities for testing of liquid metal fast breeder components at the Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility within Area IV. All nuclear work was terminated in 1988, and subsequently, all radiological work has been directed toward decontamination and decommissioning (D&D) of the previously used nuclear facilities and associated site areas. Large-scale D&D activities of the sodium test facilities began in 1996. This Annual Site Environmental Report provides information showing that there are no indications of any potential impact on public health and safety due to the operations conducted at the SSFL. All measures and calculations of off-site conditions demonstrate compliance with applicable regulations, which provide for protection of human health and the environment.

  20. 75 FR 22514 - Airworthiness Directives; The Boeing Company Model 747-200B Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-04-29

    ... Boeing to the stretched upper deck (SUD) configuration require inspection for cracking of the stringer 6... stretched upper deck (SUD) configuration require inspecting the stringer 6 lap joint upper fastener row for... results from reviews done by Boeing, which show that airplanes modified to the stretched upper deck...

  1. Site Environmental Report for Calendar Year 2003 DOE Operations at The Boeing Company, Rocketdyne Propulsion & Power

    SciTech Connect

    Liu, Ning; Rutherford, Phil; Samuels, Sandy; Lee, Majelle

    2004-09-30

    This Annual Site Environmental Report (ASER) for 2003 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of Boeing Rocketdyne’s Santa Susana Field Laboratory (SSFL). In the past, the Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations at ETEC included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities at ETEC involved the operation of large-scale liquid metal facilities that were used for testing liquid metal fast breeder components. All nuclear work was terminated in 1988; all subsequent radiological work has been directed toward decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. Closure of the liquid metal test facilities began in 1996. Results of the radiological monitoring program for the calendar year 2003 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling.

  2. Site Environmental Report for Calendar Year 2001. DOE Operations at The Boeing Company, Rocketdyne Propulsion & Power

    SciTech Connect

    Rutherford, Phil; Samuels, Sandy; Leee, Majelle

    2002-09-01

    This Annual Site Environmental Report (ASER) for 2001 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of the Boeing Rocketdyne Santa Susana Field Laboratory (SSFL). In the past, these operations included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials under the former Atomics International (AI) Division. Other activities included the operation of large-scale liquid metal facilities for testing of liquid metal fast breeder components at the Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility within Area IV. All nuclear work was terminated in 1988, and subsequently, all radiological work has been directed toward decontamination and decommissioning (D&D) of the previously used nuclear facilities and associated site areas. Closure of the sodium test facilities began in 1996. Results of the radiological monitoring program for the calendar year of 2001 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling. All radioactive wastes are processed for disposal at DOE disposal sites and other sites approved by DOE and licensed for radioactive waste. Liquid radioactive wastes are not released into the environment and do not constitute an exposure pathway. No structural debris from buildings, released for unrestricted use, was transferred to municipal landfills or recycled in 2001.

  3. View of hammer nameplate (Chambersburg Engineering Company, Chambersburg, Penna USA) ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    View of hammer nameplate (Chambersburg Engineering Company, Chambersburg, Penna USA) and view north of Tony Talotta (heavy forger), Paul Azcharka (hammer operator), and Morty Hoffman (hammer operator helper) forging eyebolts. - Naval Base Philadelphia-Philadelphia Naval Shipyard, Structure Shop, League Island, Philadelphia, Philadelphia County, PA

  4. 75 FR 8279 - Airworthiness Directives; The Boeing Company Model 747 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-02-24

    ... considered the following comments on the original NPRM. Request To Revise Costs of Compliance Northwest Airlines requests that we revise the ``Costs of Compliance'' section of the original NPRM to include Boeing's current cost of the modification kit. Northwest Airlines states that the current cost is...

  5. 75 FR 17887 - Airworthiness Directives; The Boeing Company Model 767 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-04-08

    ... require doing a detailed inspection for foreign objects debris and damage to the wall of the track housing... retracted. This condition, if not corrected, could result in a fuel leak and an increased risk of fire... increased risk of fire. Relevant Service Information We have reviewed Boeing Special Attention...

  6. 75 FR 39811 - Airworthiness Directives; The Boeing Company Model 777 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-07-13

    ... slat main track slat cans, which can allow fuel leakage into the fixed wing leading edge in excess of... slat cans, which can allow fuel leakage into the fixed wing leading edge in excess of the capacity of... tracks do not penetrate into the wing fuel tank at these locations. Boeing also states that, for...

  7. 76 FR 12617 - Airworthiness Directives; The Boeing Company Model 777-200 and -300 Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-03-08

    ...-essential electrical systems through a switch in the flight compartment in the event of smoke or flames. In... passenger cabin, a switch is needed in the flight compartment to enable the flightcrew to turn off... two new cabin power control switches. Boeing Service Bulletin 777-24-0074, Revision 1, dated October...

  8. 75 FR 15357 - Airworthiness Directives; The Boeing Company Model 767 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-03-29

    ... airplanes. This proposed AD would require repetitive inspections to detect fatigue cracking in the upper... this AD to detect and correct fatigue cracking in the upper wing skin at the fastener holes common to... October 28, 1999. Further Boeing analysis has determined the cracks to be a result of fatigue due...

  9. 75 FR 59167 - Airworthiness Directives; The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-09-27

    ... 2 June 7, 2010. 737 78 1079. Boeing Service Bulletin 4 June 16, 2005. 737 78 1069. Boeing Service...-1079 describes procedures for essentially the same actions (including inspections and modification......... Optional action..... Optional action. (Boeing Service Bulletin 737-78- 1079) (if done as an option...

  10. 76 FR 426 - Airworthiness Directives; The Boeing Company Model 737-300, -400, and -500 Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-01-05

    ... specified in paragraph 1.E., ``Compliance'' of Boeing Special Attention Service Bulletin 737-54- 1044, dated... Service Bulletin 737-54-1044, dated December 10, 2007; or Boeing Alert Service Bulletin 737-54A1044... inspection at the time specified in paragraph 1.E. of Boeing Special Attention Service Bulletin...

  11. 75 FR 57882 - Airworthiness Directives; The Boeing Company Model 737-300, -400, and -500 Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-09-23

    ... those described in Boeing Special Attention Service Bulletin 737-54-1044, dated December 10, 2007... Service Bulletin 737-54- 1044, dated December 10, 2007; except, where the service bulletin specifies a... Instructions of Boeing Special Attention Service Bulletin 737-54-1044, dated December 10, 2007; or Boeing...

  12. 76 FR 15864 - Airworthiness Directives; The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-03-22

    .... Relevant Service Information We reviewed Boeing Special Attention Service Bulletin 737-78-1083, dated June... Information Appendix A of Boeing Special Attention Service Bulletin 737-78- 1083, dated June 30, 2010... Appendix A of Boeing Special Attention Service Bulletin 737-78-1083, dated June 30, 2010. Appendix A...

  13. CCiCap: Boeing

    NASA Video Gallery

    NASA announced today its plans to partner with The Boeing Company for the next phase of the agency's Commercial Crew Program (CCP). Called Commercial Crew integrated Capability (CCiCap), the initia...

  14. 76 FR 53346 - Airworthiness Directives; The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-08-26

    ... Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes AGENCY... Jersey Avenue, SE., Washington, DC 20590. Hand Delivery: Deliver to Mail address above between 9 a.m. and...) This AD applies to The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83),...

  15. 76 FR 18022 - Airworthiness Directives; The Boeing Company Model DC-9-14, DC-9-15, and DC-9-15F Airplanes; and...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-04-01

    ... Model DC-9-14, DC-9- 15, and DC-9-15F Airplanes; and DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series..., Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT...) This AD applies to The Boeing Company Model DC-9-14, DC-9- 15, DC-9-15F, DC-9-21, DC-9-31,......

  16. 76 FR 52225 - Airworthiness Directives; The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-08-22

    ... Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes AGENCY... Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590. FOR FURTHER INFORMATION... ADs (b) None. Applicability (c) This AD applies to The Boeing Company Model DC-9-81 (MD-81),...

  17. 76 FR 1993 - Airworthiness Directives; The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-01-12

    ... Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes AGENCY... Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590. FOR FURTHER INFORMATION.... Applicability (c) This AD applies to The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83...

  18. 76 FR 41651 - Airworthiness Directives; The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-07-15

    ... Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes AGENCY... Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590. FOR FURTHER INFORMATION...) This AD applies to The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83),...

  19. 76 FR 39251 - Airworthiness Directives; The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-07-06

    ... Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes AGENCY... Jersey Avenue, SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Roger Durbin, Aerospace.... Applicability (c) This AD applies to all The Boeing Company Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83...

  20. 78 FR 36084 - Special Conditions: The Boeing Company, Model 717-200 Series Airplanes; Seats With Inflatable...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-06-17

    ... flammability of the airbag material. The Boeing Model 717-200 series airplanes will use the similar airbag... Series Airplanes; Seats With Inflatable Lapbelts AGENCY: Federal Aviation Administration (FAA), DOT... the Boeing Model 717- 200 series airplanes. These airplanes will have a novel or unusual...

  1. 76 FR 4567 - Airworthiness Directives; The Boeing Company Model 737-600, -700, -700C, -800, and -900 Series...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-01-26

    ... Attention Service Bulletin 737-30-1058, Revision 3, dated July 7, 2010. The service information describes..., certificated in any category, as identified in Boeing Special Attention Service Bulletin 737-30- 1058, Revision... accordance with the Accomplishment Instructions of Boeing Special Attention Service Bulletin...

  2. 76 FR 62649 - Airworthiness Directives; The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-10-11

    ... accordance with Boeing Special Attention Service Bulletin 737-78-1074, Revision 1, dated September 15, 2005... Bulletin 737- 78-1074, Revision 1, dated September 15, 2005, and that the replacement of the non-fireproof... airplanes, which is what is listed in Boeing Special Attention Service Bulletin 737-78-1074, Revision...

  3. Site environmental report for calendar year 2002. DOE operations at the Boeing Company, Rocketdyne Propulsion and Power

    SciTech Connect

    2003-09-30

    This Annual Site Environmental Report (ASER) for 2002 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of Boeing' s Santa Susana Field Laboratory (SSFL)). In the past, the Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations at ETEC included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities at ETEC involved the operation of large-scale liquid metal facilities that were used for testing liquid metal fast breeder components. All nuclear work was terminated in 1988, and, subsequently, all radiological work has been directed toward decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. Closure of the liquid metal test facilities began in 1996. Results of the radiological monitoring program for the calendar year 2002 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property ( land, structures, waste), and recycling. All radioactive w astes are processed for disposal at DOE disposal sites and/or other licensed sites approved by DOE for radioactive waste disposal. No liquid radioactive wastes are released into the environment, and no structural debris from buildings w as transferred to municipal landfills or recycled in 2002.

  4. 75 FR 38394 - Airworthiness Directives; The Boeing Company Model 747-100, -200B, and -200F Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-07-02

    ... ] trim out all three fastener rows of the overlapping skin common to the lap joint.'' Boeing states that... ``remove'' means to trim out all three fastener rows of the overlapping skin common to the lap...

  5. Site Environmental Report for Calendar Year 2000. DOE Operations at The Boeing Company, Rocketdyne Propulsion & Power

    SciTech Connect

    Rutherford, Phil; Samuels, Sandy; Lee, Majelle

    2001-09-01

    This Annual Site Environmental Report (ASER) for 2000 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of the Rocketdyne Santa Susana Field Laboratory (SSFL). In the past, these operations included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials, under the former Atomics International (AI) Division. Other activities included the operation of large-scale liquid metal facilities for testing of liquid metal fast breeder components at the Energy Technology Engineering Center (ETEC), a government-owned company-operated, test facility within Area IV. All nuclear work was terminated in 1988, and subsequently, all radiological work has been directed toward decontamination and decommissioning (D&D) of the previously used nuclear facilities and associated site areas. Large-scale D&D activities of the sodium test facilities began in 1996. Results of the radiological monitoring program for the calendar year of 2000 continue to indicate no significant releases of radioactive material from Rocketdyne sites. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling. All radioactive wastes are processed for disposal at DOE disposal sites and other sites approved by DOE and licensed for radioactive waste. Liquid radioactive wastes are not released into the environment and do not constitute an exposure pathway.

  6. The Boeing Company's Tech Prep Story: A Community College Bridge to the School-to-Work Strategy.

    ERIC Educational Resources Information Center

    Gayton, Carver; Parnell, Dale

    1996-01-01

    Reviews the Boeing Tech Prep Program, an associate degree program combining high school and community college vocational and academic curricula. Describes the three phases of the program's development: the provision of seed grants to schools, the development of an associate degree program, and the institution of an internship program. (MAB)

  7. 75 FR 57885 - Airworthiness Directives; The Boeing Company Model 737-600, -700, -700C, -800, and -900 Series...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-09-23

    ... undetected output from a single radio altimeter channel, which resulted in premature autothrottle retard during approach. We are proposing this AD to detect and correct erroneous output from a radio altimeter... holidays. For service information identified in this proposed AD, contact Boeing Commercial...

  8. 76 FR 13541 - Airworthiness Directives; The Boeing Company Model 757-200, -200CB, and -300 Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-03-14

    ... target and the sensor proximity switch, and testing to ensure positive door locking and corrective action... relocating and adjusting the sensor target and the sensor proximity switch to forward locations on the... a new target and the switch is remounted on the new bracket. Boeing Service Bulletin...

  9. Engineering--A Career for 330 Women at Boeing

    ERIC Educational Resources Information Center

    Minor, Barbara

    1974-01-01

    Describes the efforts of the Boeing Company to encourage and hire women for engineering jobs. Much of the article is devoted to women employed by Boeing in engineering jobs and their comments about engineering as a career for women. (BR)

  10. Pollution Control Companies U.S.A., 1972.

    ERIC Educational Resources Information Center

    1972

    This book is intended to serve as a useful guide and directory to the present industries embracing the field of environmental control, with emphasis on the prevention and abatement of pollution in its broadest aspects. The volume is divided into two sections: the first section is an alphabetical listing of approximately 1,500 companies or company…

  11. 76 FR 38074 - Airworthiness Directives; The Boeing Company Model 747-100, 747-100B, 747-200B, 747-200C, 747...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-06-29

    ... stretched- upper-deck configuration, as identified in Boeing Alert Service Bulletin 747-53A2303, dated June... is measured from the time of the stretched- upper-deck modification. (i) If no cracking is...

  12. Site Environmental Report for Calendar Year 2011. DOE Operations at The Boeing Company Santa Susana Field Laboratory, Area IV

    SciTech Connect

    Liu, Ning; Rutherford, Phil; Dassler, David

    2012-09-01

    This Annual Site Environmental Report (ASER) for 2011 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of Boeing’s Santa Susana Field Laboratory (SSFL). The Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations in Area IV included development, fabrication, operation and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities in the area involved the operation of large-scale liquid metal facilities that were used for testing non-nuclear liquid metal fast breeder reactor components. All nuclear work was terminated in 1988, and all subsequent radiological work has been directed toward environmental restoration and decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. Liquid metal research and development ended in 2002. Since May 2007, the D&D operations in Area IV have been suspended by the DOE, but the environmental monitoring and characterization programs have continued. Results of the radiological monitoring program for the calendar year 2011 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling.

  13. Site Environmental Report for Calendar Year 2009. DOE Operations at The Boeing Company Santa Susana Field Laboratory, Area IV

    SciTech Connect

    Liu, Ning; Rutherford, Phil; Amar, Ravnesh

    2010-09-01

    This Annual Site Environmental Report (ASER) for 2009 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of Boeing’s Santa Susana Field Laboratory (SSFL). The Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations in Area IV included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities in the area involved the operation of large-scale liquid metal facilities that were used for testing non-nuclear liquid metal fast breeder reactor components. All nuclear work was terminated in 1988, and all subsequent radiological work has been directed toward decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. Liquid metal research and development ended in 2002. Since May 2007, the D&D operations in Area IV have been suspended by the DOE, but the environmental monitoring and characterization programs have continued. Results of the radiological monitoring program for the calendar year 2009 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling.

  14. Site Environmental Report For Calendar Year 2012. DOE Operations at The Boeing Company Santa Susana Field Laboratory, Area IV

    SciTech Connect

    Liu, Ning; Rutherford, Phil; Dassler, David

    2013-09-01

    This Annual Site Environmental Report (ASER) for 2012 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of Boeing’s Santa Susana Field Laboratory (SSFL). The Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations in Area IV included development, fabrication, operation and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities in the area involved the operation of large-scale liquid metal facilities that were used for testing non-nuclear liquid metal fast breeder reactor components. All nuclear work was terminated in 1988, and all subsequent radiological work has been directed toward environmental restoration and decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. Liquid metal research and development ended in 2002. Since May 2007, the D&D operations in Area IV have been suspended by the DOE, but the environmental monitoring and characterization programs have continued. Results of the radiological monitoring program for the calendar year 2012 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling.

  15. Site Environmental Report for Calendar Year 2006. DOE Operations at The Boeing Company Santa Susana Field Laboratory, Area IV

    SciTech Connect

    Liu, Ning; Rutherford, Phil

    2007-09-01

    This Annual Site Environmental Report (ASER) for 2006 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of Boeing’s Santa Susana Field Laboratory (SSFL). In the past, the Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations in Area IV included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities in the area involved the operation of large-scale liquid metal facilities that were used for testing non-nuclear liquid metal fast breeder components. All nuclear work was terminated in 1988; all subsequent radiological work has been directed toward decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. Closure of the liquid metal test facilities began in 1996. Results of the radiological monitoring program for the calendar year 2006 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling.

  16. Site Environmental Report for Calendar Year 2007. DOE Operations at The Boeing Company, Santa Susana Field Laboratory, Area IV

    SciTech Connect

    Liu, Ning; Rutherford, Phil; Lenox, Art; Blair, Lori; Amar, Ravnesh; Costa, Paul; Galvez, Lydia; Jameson, Blythe; Galvez, Lydia

    2008-09-30

    This Annual Site Environmental Report (ASER) for 2007 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of Boeing’s Santa Susana Field Laboratory (SSFL). The Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations in Area IV included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities in the area involved the operation of large-scale liquid metal facilities that were used for testing non-nuclear liquid metal fast breeder components. All nuclear work was terminated in 1988; all subsequent radiological work has been directed toward decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. In May 2007, the D&D operations in Area IV were suspended until DOE completes the SSFL Area IV Environmental Impact Statement (EIS). The environmental monitoring programs were continued throughout the year. Results of the radiological monitoring program for the calendar year 2007 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling. All radioactive wastes are processed for disposal at DOE disposal sites and/or other licensed sites approved by DOE for radioactive waste disposal. No liquid radioactive wastes were released into the environment in 2007.

  17. Site Environmental Report for Calendar Year 2004. DOE Operations at The Boeing Company Santa Susana Field Laboratory

    SciTech Connect

    Liu, Ning; Rutherford, Phil; Lee, Majelle

    2005-09-01

    This Annual Site Environmental Report (ASER) for 2004 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of Boeing’s Santa Susana Field Laboratory (SSFL). In the past, the Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations in Area IV included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities in the area involved the operation of large-scale liquid metal facilities that were used for testing non-nuclear liquid metal fast breeder components. All nuclear work was terminated in 1988; all subsequent radiological work has been directed toward decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. Closure of the liquid metal test facilities began in 1996. Results of the radiological monitoring program for the calendar year 2004 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling.

  18. Site Environmental Report for Calendar Year 2008. DOE Operations at The Boeing Company Santa Susana Field Laboratory, Area IV

    SciTech Connect

    Liu, Ning; Rutherford, Phil; Amar, Ravnesh

    2009-09-01

    This Annual Site Environmental Report (ASER) for 2008 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of Boeing’s Santa Susana Field Laboratory (SSFL). The Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations in Area IV included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities in the area involved the operation of large-scale liquid metal facilities that were used for testing non-nuclear liquid metal fast breeder reactor components. All nuclear work was terminated in 1988; all subsequent radiological work has been directed toward decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. In May 2007, the D&D operations in Area IV were suspended by the DOE. The environmental monitoring programs were continued throughout the year. Results of the radiological monitoring program for the calendar year 2008 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling.

  19. Site Environmental Report for Calendar Year 2010. DOE Operations at The Boeing Company Santa Susana Field Laboratory, Area IV

    SciTech Connect

    Liu, Ning; Rutherford, Phil; Amar, Ravnesh

    2011-09-01

    This Annual Site Environmental Report (ASER) for 2010 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of Boeing’s Santa Susana Field Laboratory (SSFL). The Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations in Area IV included development, fabrication, and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities in the area involved the operation of large-scale liquid metal facilities that were used for testing non-nuclear liquid metal fast breeder reactor components. All nuclear work was terminated in 1988, and all subsequent radiological work has been directed toward decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. Liquid metal research and development ended in 2002. Since May 2007, the D&D operations in Area IV have been suspended by the DOE, but the environmental monitoring and characterization programs have continued. Results of the radiological monitoring program for the calendar year 2010 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling.

  20. Site Environmental Report for Calendar Year 2013. DOE Operations at The Boeing Company, Santa Susana Field Laboratory, Area IV

    SciTech Connect

    2014-06-30

    This Annual Site Environmental Report (ASER) for 2013 describes the environmental conditions related to work performed for the Department of Energy (DOE) at Area IV of the Santa Susana Field Laboratory (SSFL). The Energy Technology Engineering Center (ETEC), a government-owned, company-operated test facility, was located in Area IV. The operations in Area IV included development, fabrication, operation and disassembly of nuclear reactors, reactor fuel, and other radioactive materials. Other activities in the area involved the operation of large-scale liquid metal facilities that were used for testing non-nuclear liquid metal fast breeder reactor components. All nuclear work was terminated in 1988, and all subsequent radiological work has been directed toward environmental restoration and decontamination and decommissioning (D&D) of the former nuclear facilities and their associated sites. Liquid metal research and development ended in 2002. Since May 2007, the D&D operations in Area IV have been suspended by the DOE, but the environmental monitoring and characterization programs have continued. Results of the radiological monitoring program for the calendar year 2013 continue to indicate that there are no significant releases of radioactive material from Area IV of SSFL. All potential exposure pathways are sampled and/or monitored, including air, soil, surface water, groundwater, direct radiation, transfer of property (land, structures, waste), and recycling. Due to the suspension of D&D activities in Area IV, no effluents were released into the atmosphere during 2013. Therefore, the potential radiation dose to the general public through airborne release was zero. Similarly, the radiation dose to an offsite member of the public (maximally exposed individual) due to direct radiation from SSFL is indistinguishable from background. All radioactive wastes are processed for disposal at DOE disposal sites and/or other licensed sites approved by DOE for radioactive waste

  1. 78 FR 47778 - The Boeing Company Boeing Commercial Aircraft (BCA) Auburn, Washington; The Boeing Company Boeing...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-06

    ...), Puyallup, Washington (TA-W-82,705B), North 8th and Logan Avenue North, Renton, Washington (TA-W-82,705C... Aircraft (BCA), North 8th, Logan Avenue North, 10-16 Building 535 Garden Avenue North and 10-18...

  2. Commercial Crew Program: Boeing Breakout Video

    NASA Video Gallery

    NASA and The Boeing Company of Houston signed a funded Space Act Agreement (SAA) in March 2011 for the company’s CST-100. Under the $92.3 million agreement, NASA’s Commercial Crew Program (...

  3. 75 FR 10669 - Airworthiness Directives; The Boeing Company Model 747-100, 747-200B, 747-300, and 747SR Series...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-03-09

    ... Model 747-100, 747- 200B, 747-300, and 747SR Series Airplanes AGENCY: Federal Aviation Administration... Model 747-100, 747-200B, 747-300, and 747SR series airplanes. This AD requires installation of a... airworthiness directive (AD) that would apply to certain Boeing Model 747-100, 747-200B, 747-300, and...

  4. 75 FR 38007 - Airworthiness Directives; The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-07-01

    ..., and 747SP Series Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule... SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400F, 747SR, and 747SP series airplanes. This...). This AD results from reports of duct assemblies in the ECS with burned Boeing Material...

  5. 75 FR 18446 - Airworthiness Directives; The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-04-12

    ..., and 747SP Series Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of..., and 747SP series airplanes. This proposed AD would require reworking or replacing certain duct... assemblies in the ECS with burned Boeing Material Specification (BMS) 8-39 polyurethane foam insulation....

  6. 75 FR 9760 - Airworthiness Directives; The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-03-04

    ... cracks in the wing and horizontal stabilizer side-of-body joints and the fuselage skin circumferential... from Boeing analysis indicating that the wing and horizontal stabilizer side-of-body joints, and the..., FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington...

  7. 75 FR 61337 - Airworthiness Directives; The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-10-05

    ... Li, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601... required by this AD to the Boeing Commercial Airplanes ODA rather than a Designated Engineering... Li, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office,...

  8. 76 FR 13067 - Airworthiness Directives; The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-03-10

    ... engine mount and adjacent support structure, and visual inspections of the internal angle and external... forward engine mount and adjacent support structure, and visual inspections of the internal angle and... Include an Option To Support the Engine Boeing requested that we revise paragraph (k) of the NPRM...

  9. Boeing CST-100 Mock-Up Undergoes Airbag Stabilization Test

    NASA Video Gallery

    The Boeing Company's mock-up CST-100 spacecraft was put through water landing development tests Oct. 1-5, 2012, at Bigelow Aerospace's headquarters outside of Las Vegas. Engineers with Bigelow have...

  10. Boeing P-26A

    NASA Technical Reports Server (NTRS)

    1937-01-01

    Boeing P-26A: Popularly called the 'Peashooter,' the Boeing P-26A was the Boeing model 266. Powered by the Pratt & Whitney Wasp radial engine, the P-26 was the Army's front-line fighter during the mid-1930's. The P-26 held the distinction of being the Army's first monoplane fighter. This example had a reference line painted on its side by the NACA shortly after its arrival at Langley Field.

  11. Loftin Collection - Boeing Aircraft

    NASA Technical Reports Server (NTRS)

    1933-01-01

    Either a F2B-1 or F3B-1, both aircraft were built by Boeing and both were powered by Pratt and Whitney Wasp engines. These fighters were intended for Navy shipboard use. Boeing F3B-1: While most Boeing F3B-1s served the U. S. Navy aircraft carriers the Lexington and the Saratoga, this example flew in NACA hands at the Langley Memorial Aeronautical Laboratory in the late 1920's. Also known as the Boeing Model 77, the aircraft was the next to last F3B-1 build in November 1928.

  12. Boeing YP-29A

    NASA Technical Reports Server (NTRS)

    1938-01-01

    Boeing YP-29A: The YP-29A originally was an enclosed cockpit fighter with a NACA cowling around the Pratt and Whitney Wasp power plant, but was modified to this configuration with a Townend ring around the Wasp and an open cockpit. The redesigned headrest which extended to the tail surfaces was reminiscent of, and substantially larger than that on the Boeing

  13. Transonic CFD applications at Boeing

    NASA Technical Reports Server (NTRS)

    Tinoco, E. N.

    1989-01-01

    The use of computational methods for three dimensional transonic flow design and analysis at the Boeing Company is presented. A range of computational tools consisting of production tools for every day use by project engineers, expert user tools for special applications by computational researchers, and an emerging tool which may see considerable use in the near future are described. These methods include full potential and Euler solvers, some coupled to three dimensional boundary layer analysis methods, for transonic flow analysis about nacelle, wing-body, wing-body-strut-nacelle, and complete aircraft configurations. As the examples presented show, such a toolbox of codes is necessary for the variety of applications typical of an industrial environment. Such a toolbox of codes makes possible aerodynamic advances not previously achievable in a timely manner, if at all.

  14. Boeing F3B-1

    NASA Technical Reports Server (NTRS)

    1930-01-01

    Boeing F3B-1: While most Boeing F3B-1s served aboard the U. S. Navy aircraft carriers Lexington and Saratoga, this example flew in NACA hands at the Langley Memorial Aeronautical Laboratory in the late 1920's. Also known as the Boeing Model 77, the aircraft was powered by a Pratt & Whitney Wasp radial engine.

  15. Boeing to Rank Colleges by Measuring Graduates' Job Success

    ERIC Educational Resources Information Center

    Basken, Paul

    2008-01-01

    Boeing Company, the Chicago-based aerospace giant, has spent the past year matching internal data from employee evaluations with information about the colleges its engineers attended. It has used that analysis to create a ranking system, which it plans to unveil in the coming month, that will show which colleges have produced the workers it…

  16. COIL technology development at Boeing

    NASA Astrophysics Data System (ADS)

    Hurlock, Steve C.

    2002-05-01

    The historical COIL contributions at the McDonnell Douglas Research Laboratory, the Rocketdyne Division of Rockwell International and Boeing's Laser and Electro-Optic Systems organization are briefly described. The latter organization now contains the capabilities of the two heritage organizations. Boeing's new high pressure sealed COIL is also described.

  17. Will Boeing Change Health Care?

    PubMed

    Stempniak, Marty

    2015-12-01

    Big employers like Boeing and Intel are directly contracting with hospitals in an effort to control health care prices. Some hospital CEOs see direct contracting as the future, while others wonder how they can participate.

  18. Boeing flight deck design philosophy

    NASA Technical Reports Server (NTRS)

    Stoll, Harty

    1990-01-01

    Information relative to Boeing flight deck design philosophy is given in viewgraph form. Flight deck design rules, design considerations, functions allocated to the crew, redundancy and automation concerns, and examples of accident data that were reviewed are listed.

  19. Water Injection Feasibility for Boeing 747 Aircraft

    NASA Technical Reports Server (NTRS)

    Daggett, David L.

    2005-01-01

    Can water injection be offered at a reasonable cost to large airplane operators to reduce takeoff NO( sub x) emissions? This study suggests it may be possible. This report is a contract deliverable to NASA Glenn Research Center from the prime contractor, The Boeing Commercial Airplane Company of Seattle, WA. This study was supported by a separate contract to the Pratt & Whitney Engine Company of Hartford, CT (contract number NNC04QB58P). Aviation continues to grow and with it, environmental pressures are increasing for airports that service commercial airplanes. The feasibility and performance of an emissions-reducing technology, water injection, was studied for a large commercial airplane (e.g., Boeing 747 with PW4062 engine). The primary use of the water-injection system would be to lower NOx emissions while an important secondary benefit might be to improve engine turbine life. A tradeoff exists between engine fuel efficiency and NOx emissions. As engines improve fuel efficiency, by increasing the overall pressure ratio of the engine s compressor, the resulting increased gas temperature usually results in higher NOx emissions. Low-NO(sub x) combustors have been developed for new airplanes to control the increases in NO(sub x) emissions associated with higher efficiency, higher pressure ratio engines. However, achieving a significant reduction of NO(sub x) emissions at airports has been challenging. Using water injection during takeoff has the potential to cut engine NO(sub x) emissions some 80 percent. This may eliminate operating limitations for airplanes flying into airports with emission constraints. This study suggests an important finding of being able to offer large commercial airplane owners an emission-reduction technology that may also save on operating costs.

  20. Barotrauma in Boeing 737 cabin crew.

    PubMed

    Kortschot, H W; Oosterveld, W J

    1993-01-01

    Several aircrew members of a Boeing 737 aircraft were referred to our department because they suffered from a barotrauma. The fast rate of pressure change during the descent of a Boeing 737 aircraft, as compared to the Boeing 747, DC-10 and Airbus 310 aircrafts, is most likely the cause of the development of the barotraumata.

  1. Boeing F4B-4

    NASA Technical Reports Server (NTRS)

    1932-01-01

    The Boeing F4B-4 was seen to differ from earlier F4Bs in having a vertical fin with slightly more area. The Boeing model 235 was not fitted with a NACA cowling, but rather the less efficient 'Townend' ring around the Pratt & Whitney Wasp radials cylinders. This aircraft was much used by both the Navy and the Army Air Corps in the late 1920's and early 1930's. The Army variation was known as the P-12E. The engine cowling was a British development known as the 'Townend' ring. It differed from the NACA cowling and was less effective in reducing the drag.

  2. Status of the Boeing Dish Engine Critical Component Project

    SciTech Connect

    Brau, H.W.; Diver, R.B.; Nelving, H.; Stone, K.W.

    1999-01-08

    The Boeing Company's Dish Engine Critical Component (DECC) project started in April of 1998. It is a continuation of a solar energy program started by McDonnell Douglas (now Boeing) and United Stirling of Sweden in the mid 1980s. The overall objectives, schedule, and status of this project are presented in this paper. The hardware test configuration, hardware background, operation, and test plans are also discussed. A summary is given of the test data, which includes the daily power performance, generated energy, working-gas usage, mirror reflectivity, solar insolation, on-sun track time, generating time, and system availability. The system performance based upon the present test data is compared to test data from the 1984/88 McDonnell Douglas/United Stirling AB/Southem California Edison test program. The test data shows that the present power, energy, and mirror performance is comparable to when the hardware was first manufactured 14 years ago.

  3. Status of the Boeing Dish Engine Critical Component project

    SciTech Connect

    Stone, K.W.; Nelving, H.; Braun, H.W.; Clark, T.B.; Diver, R.B.

    1999-07-01

    The Boeing Company's Dish Engine Critical Component (DECC) project started in April of 1998. It is a continuation of a solar energy program started by McDonnel Douglas (now Boeing) and United Stirling of Sweden in the mid 1980s. The overall objectives, schedule, and status of this project are presented in this paper. The hardware test configuration, hardware background, operation, and test plans are also discussed. A summary is given of the test data, which includes the daily power performance, generated energy, working-gas usage, mirror reflectivity, solar insolation, on-sun track time. Generating time, and system availability. The system performance based upon the present test data is compared to test data from the 1984/88 McDonnel Douglas/United Stirling AB/Southern California Edison test program. The test data shows that the present power, energy, and mirror performance is comparable to when the hardware was first manufactured 14 years ago.

  4. Boeing--A Case Study Example of Enterprise Project Management from a Learning Organization Perspective.

    ERIC Educational Resources Information Center

    Szymczak, Conrad C.; Walker, Derek H. T.

    2003-01-01

    The evolution of the Boeing Company illustrates how to achieve an enterprise project management culture through organizational learning. Project management can be a survival technique for adapting to change as well as a proactive mechanism. An organizational culture that supports commitment and enthusiasm and a knowledge management infrastructure…

  5. 78 FR 72567 - Airworthiness Directives; General Electric Company Turbofan Engines

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-03

    ... Company Turbofan Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are adopting a new airworthiness directive (AD) for certain General Electric Company (GE) GE90... Proposed AD The Boeing Company and FedEx Express agreed with the AD as proposed. Request To Change...

  6. 78 FR 76731 - Special Conditions: Boeing Model 777-200, -300, and -300ER Series Airplanes; Rechargeable Lithium...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-19

    ...These special conditions are issued for the Boeing Model 777- 200, -300, and -300ER series airplanes. These airplanes as modified by the ARINC Aerospace Company will have a novel or unusual design feature, specifically the installation of rechargeable lithium ion batteries and battery system that will be used on an International Communications Group (ICG) ePhone cordless cabin handset. The......

  7. 77 FR 47267 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-08

    ... Model 747-200B series airplanes having a stretched upper deck. The existing AD currently requires...-300, 747-400, and 747-400D series airplanes; and Model 747-200B series airplanes having a stretched..., and 747-400D series airplanes; and Model 747-200B series airplanes having a stretched upper...

  8. 77 FR 40481 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-10

    ..., 747-200B, 747- 200C, 747-200F, 747-400F, 747SR, and 747SP series airplanes, without a stretched upper deck or stretched upper deck modification. That AD currently requires repetitive inspections for...

  9. 77 FR 5195 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-02

    ... series airplanes; and Model 747-200B series airplanes having a stretched upper deck. The original NPRM...; and Model 747-200B series airplanes having a stretched upper deck. The original NPRM was published in... series airplanes; and Model 747-200B series airplanes having a stretched upper deck; certificated in...

  10. 77 FR 34879 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-12

    ... fairing of the left engine strut at the clamp support location under the aft fairing compartment, inside... of the left engine strut at the clamp support location under the aft fairing compartment, inside the... requires replacing the drain tube assemblies and support clamps on the aft fairing of the engine...

  11. 78 FR 21279 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-10

    ... locations, inspecting application of stencils and index markers of impact resistant access doors, corrective... near ignition sources (engine, hot brakes), consequently leading to a fuel-fed fire. DATES: We must... object penetration of the wing tank, which could lead to a fuel leak near ignition sources (engine,...

  12. 78 FR 42415 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-16

    ... determine that impact-resistant access doors are installed in the correct locations, inspecting application... penetration of the wing tank, which could lead to a fuel leak near ignition sources (engine, hot brakes...-resistant access doors are installed in the correct ] locations, inspecting application of stencils...

  13. 77 FR 70357 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-11-26

    ... by a report of a broken drain tube assembly on the left engine strut at the clamp support location... support clamps on the aft fairing of the engine struts. This new AD requires replacing the drain tube assembly of the left and right engine strut aft fairings with a new one, which includes an integral...

  14. 78 FR 70196 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-11-25

    ... determine that impact-resistant access doors are installed in the correct locations, and to replace any door..., which could cause a fuel leak near an ignition source (e.g., hot brakes or engine exhaust nozzle... the correct locations, and to replace any door with an impact-resistant access door if necessary....

  15. 78 FR 58970 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-25

    ... flight deck display units resulting in blanking, blurring, or loss of color on the display. This proposed... airplanes reported flight deck display unit malfunctions including blanking, blurring, or loss of color... units resulting in blanking, blurring, or loss of color on the display. We are issuing this AD...

  16. 76 FR 62667 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-10-11

    ... airplanes. This proposed AD was prompted by reports of water leaking into electrical and electronic... sealing and taping the floor panels. We are proposing this AD to correct the unsafe condition on these... substantive verbal contact we receive about this proposed AD. Discussion We have received reports of...

  17. 77 FR 53155 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-31

    ... firing cable and safety pin, and modifying the slide valise. That NPRM was prompted by reports of escape... regulator, modifying the slide valise, and installing a new firing cable and safety pin. Actions Since... valve regulator P/N 4A3865-2, -3, or -4, as applicable; installing a new firing cable and safety...

  18. 77 FR 10406 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-22

    ... deactivation pin. This proposed AD would add a dye penetrant inspection for cracking of the rivet holes of the... a dye penetrant inspection for cracking of the rivet holes of the bushing plate; repair or... Alert Service Bulletin 767-78A0089, Revision 5, dated June 9, 2009, do a dye penetrant inspection...

  19. 78 FR 71989 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-02

    ...-8F series airplanes. This AD requires repetitive ultrasonic or dye penetrant inspections for cracking.... (2) Dye penetrant inspection for cracking of the bolts and barrel nuts. Whenever a dye penetrant... this AD. (2) For airplanes on which a dye penetrant inspection was done, do the required actions at...

  20. 77 FR 41895 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-17

    ... requires a dye penetrant inspection for cracking of the rivet holes of the bushing plate and repair or..., improved components. That NPRM also proposed to require a dye penetrant inspection for cracking of the..., dated June 9, 2009, do a dye penetrant inspection for cracking of the rivet holes and replace any...

  1. 77 FR 16147 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-20

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION... Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final... the flightcrew's ability to perform critical takeoff communication and result in an aborted takeoff...

  2. 77 FR 73908 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-12-12

    ... displays for airplane attitude, altitude, or airspeed, and consequently reduce the ability of the... airplane attitude, altitude, or airspeed, and consequently reduce the ability of the flightcrew to...

  3. 78 FR 42895 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-18

    ... intended to support the airplane reaching its limit of validity (LOV) of the engineering data that support.../media/Advisory_Circular/120-104.pdf ), several programs have been developed to support initiatives that... initiatives is the requirement to establish a LOV of the engineering data that support the...

  4. 76 FR 72863 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-11-28

    ... (for Model 707 airplanes, and Model 720 and 720B series airplanes). Determine Material of the... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM...-100 long body, -200, -100B long body, and -100B short body series airplanes; Model 707-300,...

  5. 78 FR 72836 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-04

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM... airplanes. This proposed AD was prompted by multiple reports of cracking in the overwing frames. This... adjacent structure and consequent loss of structural integrity of the airplane. DATES: We must...

  6. 78 FR 55662 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-11

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM...-10, DC-9-30, and DC-9-40 series airplanes. This proposed AD was prompted by an evaluation by the... integrity of the airplane. DATES: We must receive comments on this proposed AD by October 28,...

  7. 77 FR 50411 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-21

    ... Material Specification (BMS) 8-39 urethane foam, and a report from the airplane manufacturer that airplanes... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM... 747SP series airplanes; Model 767-200, -300, -300F, and -400ER series airplanes; and Model...

  8. 78 FR 26720 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-08

    ... airplanes. The existing AD requires, for certain airplanes, an inspection to determine the material of an..., dated December 22, 2010, but airplane groups were changed based on the material composition of the.... The proposed AD would add, for certain airplanes, an inspection to determine material type of...

  9. 77 FR 63714 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-17

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are adopting a... airplanes. This AD was prompted by a report of elevator vibration and bearing swage failures. This AD requires, for certain airplanes, repetitive inspections for any discrepancies (such as a gap or a...

  10. 78 FR 78703 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-27

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are adopting a... series airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating... bulkhead, which could result in reduced structural integrity of the airplane. DATES: This AD is...

  11. 78 FR 28128 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-14

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are adopting a... airplanes. This AD was prompted by reports of two in-service occurrences on Model 737-400 airplanes of total..., inability to restart the engines, and consequent forced landing of the airplane. DATES: This AD is...

  12. 77 FR 46343 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-03

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM...-400D, 747-400F, 747SR, and 747SP series airplanes; and certain Model 757-200, -200PF, and -300 series airplanes. The existing AD currently requires replacing the control switches of the forward, aft, and...

  13. 78 FR 73744 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-09

    ... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Supplemental notice of proposed... series airplanes. The SNPRM proposed to require inspecting for a serial number that starts with the... action revises the SNPRM by revising the applicable thresholds from flight cycles on the airplane...

  14. 77 FR 54848 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-06

    ... electrical systems, as well as flight control and avionics equipment. In addition to electromagnetic coupling, since the tail strobe light is located in a flammable leakage zone, electrical current on the...

  15. 77 FR 58330 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-20

    ... elevator tab control mechanism, which could result in severe elevator and tab vibration. Consequent... elevator vibration. That AD also was prompted by reports of gaps in elevator tab control mechanisms and... mechanism, which could result in elevator and tab vibration. Consequent structural failure of the...

  16. 77 FR 65613 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-30

    ... report of an abnormal airframe vibration in the aft fuselage during flight. We are issuing this AD to prevent excessive freeplay in the rudder control surface, which could cause rudder vibration, and result...: Discussion We have received a report of an abnormal airframe vibration in the aft fuselage during flight....

  17. 77 FR 45513 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-01

    ... proposed AD was prompted by a report of elevator vibration and bearing swage failures. This proposed AD... vibration. Consequent structural failure of the elevator or horizontal stabilizer could result in loss of... proposed AD. Discussion We received a report of elevator vibration and bearing swage failures on Model...

  18. 78 FR 21569 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-11

    ... stiffness, that could lead to elevator vibration and possible interference with the tab control rod and..., could adversely affect elevator structural stiffness, which could result in elevator vibration and..., which could adversely affect elevator structural stiffness, that could lead to elevator vibration...

  19. 78 FR 43770 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-22

    ... vibration and possible interference with the tab control rod. These conditions could result in flutter and... adversely affect elevator structural stiffness, which could lead to elevator vibration and...

  20. 78 FR 58487 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-24

    ... system installations. The phase 3 DUs provide primary flight information including airspeed, altitude..., Aerospace Engineer, Systems and Equipment Branch, ANM-130S, Seattle Aircraft Certification Office, FAA, 1601.... Discussion This proposed AD resulted from instrumented testing on Model 737 series airplanes that...

  1. 77 FR 52201 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-29

    ... installing Aero-Engine database (AEDB) software in the airplane information management system (AIMS) hardware... 3110-BCG-00R-06, media set part number 243W0033-7, in the airplane information management system... Management, P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; phone: 206-544-5000, extension 1;...

  2. 77 FR 49708 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-17

    ... with Figure 24, Steel Part Surface Inspection (Impedance Plane Display), Subject 51-00-00, Structural... Inspection (Impedance Plane Display), Subject 51-00-00, Structural--General, of Part 6, Eddy Current, of...

  3. 77 FR 65506 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-29

    ... service history, which included numerous reports of fatigue cracking on certain strut and wing structure... engines. (d) Subject Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America... during the initial design. Subsequent analysis and service history, which includes numerous reports...

  4. 77 FR 23166 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-18

    ... regulations, the service history of airplanes subject to those regulations, and existing maintenance practices... System Component (JASC)/Air Transport Association (ATA) of America Code 28, Fuel. (e) Unsafe...

  5. 77 FR 13043 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-05

    ... drip shield, including an inspection for cracking and holes in the MEC drip shield, and corrective... the forward drain tubes. We are proposing this supplemental NPRM to prevent water penetration into the... the top surface of the MEC drip shield, including an inspection for cracking and holes in the MEC...

  6. 78 FR 40060 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-03

    ... currently requires repetitive inspections to detect cracks of the outer V-blades of the thrust reverser, and... repetitive inspections. Since we issued that AD, we have received reports of cracked outer V-blade fittings... action is done, repetitive inspections for cracking in the outer V-blade fittings of the hinge beam...

  7. 77 FR 51720 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-27

    ... ignition source, which in combination with flammable fuel vapors could result in a fuel tank explosion, and..., which in combination with flammable fuel vapors, could result in a fuel tank explosion, and consequent... could result in a fuel tank explosion, and consequent loss of the airplane. (f) Compliance Comply...

  8. 77 FR 47329 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-08

    ... explosion and consequent loss of the airplane. Since we issued that AD, we have received new data indicating... tanks, which, in combination with flammable fuel vapors, could result in a fuel tank explosion...

  9. 78 FR 14644 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-07

    ... fuel vapors, could result in a center wing fuel tank explosion, and consequent loss of the airplane... fuel tank explosion, and consequent loss of the airplane,'' to clarify the area that might be... to a fire in the area and potentially result in a center wing tank explosion. Therefore, we agree...

  10. 77 FR 51722 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-27

    ... that AD to prevent electrical energy from lightning, hot shorts, or fault current from entering the... that AD to prevent electrical energy from lightning, hot shorts, or fault current from entering...

  11. 77 FR 41931 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-17

    ... keyways of the number 2 windows on the flight deck; re-clocking the connector keyways to 12 o'clock, if... Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE... Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and...

  12. 77 FR 18137 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-27

    ...), latch pin migration, and broken latch pin fittings. This proposed AD would require various repetitive... cargo door latch mechanism and/or the lower sill structure. The migration of two or more latch pins and... determine if the bolt is broken; and checking the latch pin for migration and, if necessary, a...

  13. 78 FR 4047 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-18

    ... broken and damaged latch pin retention bolts and subsequent migration of the latch pins of the main deck... retention bolts and the subsequent migration of the latch pins rather than by the broken latch pin fittings... prompted by reports of broken and damaged latch pin retention bolts and subsequent migration of the...

  14. 78 FR 9346 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-02-08

    ... $10,285. correctly assembled. per hour = $85. Option to rework/replace Between 3 and 24 $286 per latch... done. (g) Replacement or Rework of Escape Slide Latch Assembly Within 48 months after the...

  15. 78 FR 58982 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-25

    ... inspecting to determine the part number of the attach pins of the horizontal stabilizer rear spar, and replacing certain attach pins. Since we issued AD 2013-07-07, we received inquiries from affected operators regarding the parts installation limitation and prohibition, and re-installation of certain attach pins...

  16. 78 FR 11972 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-02-21

    ... under the number 3 very high frequency (VHF) antenna on the lower external surface of the airplane at... corrosion under the number 3 VHF antenna, and corrective actions if necessary; and, for certain airplanes... structure under the number 3 VHF antenna, which could result in separation of the antenna from the...

  17. 77 FR 13187 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-06

    ... external doublers and antennas, and at locations where external decals had been cut. We are issuing this AD... doublers and antennas, and at locations where external decals had been cut. We are issuing this AD...

  18. 77 FR 15640 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-16

    ... frequency (VHF) antenna, and corrective actions if necessary; and, for certain airplanes, replacing bonded... cracks in the skin and surrounding structure under the number 3 VHF antenna on the lower external surface... number 3 VHF antenna, which could result in separation of the antenna from the airplane, and...

  19. 78 FR 59293 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-26

    ... satellite communication (SATCOM) antenna adapter. This proposed AD would require repetitive inspections of... SATCOM antenna adapter. During a maintenance planning data inspection, one operator reported a 16-inch crack under the 3-bay SATCOM antenna adapter plate in the crown skin of the fuselage on an airplane...

  20. 77 FR 70355 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-11-26

    ... arcing and consequent fire in section 48 (a flammable fluid leakage zone) or heat damage to the APU power... zone) or heat damage to the auxiliary power unit (APU) power feeder cable, insulation blankets, or..., ``If visual indications of heat damage are found, do steps 6.c through 6.f.'' However, if no...

  1. 78 FR 26233 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-06

    ... View B: These illustrations show the top fastener to be removed in the center of three fasteners in...) fasteners that do not require removal for this action. View B also incorrectly shows the location of the top... Retainer Support on the Left (Right) Thrust Reverser Half,'' have View B showing the top fastener in...

  2. 78 FR 21571 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-11

    ... AD would also require installing a fiberglass reinforcement overcoat to the top surface of the aft...- NM-005-AD. (a) Comments Due Date We must receive comments by May 28, 2013. (b) Affected ADs None. (c... found. (2) Install a fiberglass reinforcement overcoat to the top surface of the aft MEC drip...

  3. 77 FR 2666 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-19

    ... a general visual inspection of the housing ] assembly of the packboard release mechanism to... visual inspection of the housing assembly of the door- mounted slide/raft packboard release mechanism to... Attention Service Bulletin 777-25-0507, dated June 30, 2011: Do a general visual inspection of the...

  4. 77 FR 21426 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-10

    .... This AD requires repetitive general visual inspections for broken or missing latch pins of the lower..., 2011 (76 FR 54405). That NPRM proposed to require repetitive general visual inspections for broken or... visual inspections of the entire door. The inspections required by this final rule include...

  5. 78 FR 79289 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-30

    ... shield gutter; and doing a one-time general visual inspection for disbonded seams, and repair if...; cleaning the aft MEC drip shield gutter; and doing a one-time general visual inspection for disbonded seams... aft MEC drip shield gutter, and do a general visual inspection for disbonded seams; repair...

  6. 78 FR 65171 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-31

    ... conversion. This AD requires doing a general visual inspection of the station 1920 splice clip for correct... visual inspection of the station 1920 splice clip for correct fastener installation, and related..., 2012: Do a general visual inspection for correct installation of the station 1920 splice clip common...

  7. 78 FR 60673 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-02

    ... the control column shaker during takeoff. This AD requires performing a general visual inspection to... performing a general visual inspection to determine if a certain angle of attack (AOA) sensor with a paddle... done. (g) Inspection Within 36 months after the effective date of this AD: Do a general...

  8. 77 FR 71731 - Airworthiness Directives; The Boeing Company

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-12-04

    ... found in the strut forward dry bay. This proposed AD would require repetitive general visual inspections... repetitive general visual inspections for hydraulic fluid contamination of the strut forward dry bay, and... Cost on U.S. operators Repetitive general visual 5 work-hours x $85 per hour $0 $425 per inspection...

  9. 78 FR 19093 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-29

    ... slide/raft packboard release mechanisms. This AD requires doing a general visual inspection of the... to require doing a general visual inspection of the housing assembly of the packboard release..., January 19, 2012), which defined a general visual inspection, to new paragraph (i) in the regulatory...

  10. 78 FR 63855 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-25

    ... stabilizer rear spar and the elevator front spar and between certain stabilizer stations for defects and... cause wear of adjacent parts and increased freeplay of the elevator surfaces. Freeplay that exceeds... check of the ram air turbine system. When investigating the cause of the noise, the operator found...

  11. 78 FR 11569 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-02-19

    ... track of slats 1 and 10; a detailed inspection of all slat track housings for foreign object debris (FOD... puncture in the slat track housing and lead to a fuel leak and potential fire. DATES: This AD is effective... potential fire. (f) Compliance Comply with this AD within the compliance times specified, unless...

  12. 78 FR 49910 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-16

    ... an inspection of the slat can interior for foreign object debris (FOD), and removal of any FOD found... assemblies, which could puncture the slat track housing and result in a fuel leak and consequent fire. DATES... the slat can interior for foreign object debris (FOD), and removal of any FOD found; modification...

  13. 78 FR 15332 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-11

    ... inspection of the slat can interior for foreign object debris (FOD), and removal of any FOD found... track housing and result in a fuel leak and consequent fire. DATES: We must receive comments on this... could puncture the slat track housing and result in a fuel leak and consequent fire. Actions...

  14. 77 FR 32433 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-01

    ... and 10; a detailed inspection of all slat track housings for foreign object debris (FOD) and visible... the slat track housing and lead to a fuel leak and potential fire. Since these actions impose an... prevent a potential fire. To delay this action would be inappropriate, since we have determined that...

  15. 78 FR 49903 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-16

    ... Federal Regulations is sold by the Superintendent of Documents. #0;Prices of new books are listed in the... cracking on the door on the other side of the airplane. Southwest added that, for a door that has no... surface high frequency eddy current (HFEC) inspection for cracking of the left- and right-side inboard...

  16. 78 FR 60679 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-02

    ... prompted by multiple reports of cracks of overwing frames. This AD requires repetitive inspections for cracking of the overwing frames, and corrective actions if necessary. We are issuing this AD to detect and correct such cracking that could sever a frame, which may increase the loading of adjacent frames,...

  17. 77 FR 57541 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-18

    ...-600 series airplanes. This proposed AD was prompted by reports of early fatigue cracks at chem- mill areas on the crown skin panels. This proposed AD would require repetitive inspections for cracking of... this AD to detect and correct fatigue cracking of the skin panel at the specified chem- ] mill...

  18. 77 FR 65805 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-31

    ... prompted by reports of cracks of the wing rear spar lower cap at the outboard flap, inboard drive hinge at... cracking on the aft side of the left and right wing rear spar lower caps at station Xrs=164.000, further ETHF inspections if cracks are found, and repair if necessary; and repetitive post-repair...

  19. 78 FR 49906 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-16

    ... by a report of cracking in the left-side chord of the fin closure rib on the vertical stabilizer... cracking and corrosion, and related investigative and corrective actions if necessary. We are issuing this AD to detect and correct cracking and corrosion in the left- and right-side chords of the fin...

  20. 77 FR 27142 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-05-09

    ... airplanes. This proposed AD was prompted by multiple reports of cracks of overwing frames. This proposed AD would require repetitive inspections for cracking of the overwing frames, and related investigative and corrective actions if necessary. We are proposing this AD to detect and correct such cracking that...

  1. 78 FR 24338 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-25

    ... airplanes. This AD was prompted by reports of early fatigue cracks at chem-mill areas on the crown skin panels. This AD requires repetitive inspections for cracking of the fuselage skin along chem-mill steps... detect and correct fatigue cracking of the skin panel at the specified chem-mill step locations,...

  2. 77 FR 24355 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-24

    ..., and 777F series airplanes. This AD was prompted by reports of cracks found in the Web pockets of the... frequency eddy current inspections for cracks of the WCS spanwise beams, and repair if necessary. We are issuing this AD to detect and correct cracking in the WCS spanwise beams, which could result in...

  3. 78 FR 14469 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-06

    ... inspections to find cracking of the web, strap, inner chords, inner chord angle of the forward edge frame of... necessary; and repetitive inspections for cracking of repairs. Since we issued that AD, we have received multiple reports of cracking outside of the previous fuselage inspection areas and a report of a crack...

  4. 77 FR 36222 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-18

    ... of an inboard main landing gear (MLG) door assembly departure due to premature fatigue cracking in... cracking of the inboard MLG door hinge fittings; and modification of cracked fittings, which would terminate the repetitive inspections. We are proposing this AD to detect and correct fatigue cracking in...

  5. 77 FR 2664 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-19

    ... airplanes. This proposed AD was prompted by reports of cracks found on the center section ribs of the horizontal stabilizers. This proposed AD would require repetitive inspections for cracking of the aft face of... crack measurement, repairs, and installation of a new center section rib if necessary. We are...

  6. 78 FR 76047 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-16

    ..., and 747SR series airplanes. This AD was prompted by reports of cracks of both lower chords and web on certain outboard struts. This AD requires repetitive inspections for cracking of the lower spar chords and web, web lower spar chord modification, which includes inspections for cracking of the lower...

  7. 77 FR 36143 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-18

    ... prompted by reports of cracks found on the center section ribs of the horizontal stabilizers. This AD requires repetitive inspections for cracking of the aft face of the left and right rib hinge bearing lugs of the center ] section of the horizontal stabilizer; and crack measurement, repairs,...

  8. 77 FR 57536 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-18

    ...-700 and -700C series airplanes. This proposed AD was prompted by reports of early fatigue cracks at... cracking of the fuselage skin at certain locations at chem-mill areas, and repair if necessary. We are proposing this AD to detect and correct fatigue cracking of the skin panel at the specified chem-mill...

  9. 78 FR 25369 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-01

    ... airplanes. This AD was prompted by reports of early fatigue cracks at chem-mill areas on the crown skin panels. This AD requires repetitive inspections for cracking of the fuselage skin at certain locations at chem-mill areas, and repair if necessary. We are issuing this AD to detect and correct fatigue...

  10. 78 FR 25372 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-01

    ... AD was prompted by reports of early fatigue cracks at chem-mill areas on the crown skin panels. This AD requires repetitive inspections for cracking of the fuselage skin along chem-mill steps at certain... correct fatigue cracking of the skin panel at the specified chem-mill step locations, which could...

  11. 77 FR 28240 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-05-14

    ... airplanes. This AD was ] prompted by reports of multiple site damage cracks in the radial web lap and tear... repetitive inspections for cracking of the aft pressure bulkhead at STA 1582, repair or replacement of any cracked bulkhead, and eventual replacement of the aft pressure bulkhead at STA 1582 with a new...

  12. 77 FR 69744 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-11-21

    ... airplanes. This AD was prompted by reports of cracks in the inner chords at both left-side and right-side... transition radius for cracks, and related investigative and corrective actions if necessary. We are issuing this AD to prevent large cracks in the frames and adjacent structure that can adversely affect...

  13. 78 FR 43763 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-22

    ... airplanes. This AD was prompted by reports of cracking in the outboard flange of the longeron extension... of the longeron extension fittings for cracking, and corrective actions if necessary. We are issuing this AD to detect and correct cracks in the longeron extension fittings, which can become large...

  14. 78 FR 60807 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-02

    ... cracking found in the skin at the lower aft corner of the forward entry doorway on airplanes that do not have an airstair door cutout. This proposed AD would require repetitive inspections for cracking in the... repair if necessary. We are proposing this AD to detect and correct cracking in the lower corners of...

  15. 77 FR 46932 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-07

    ... by reports of cracks of the underwing longeron fittings in the wing center section. This AD requires repetitive inspections of the underwing longeron fitting for cracking, and related investigative and corrective actions if necessary. We are issuing this AD to detect and correct such cracking, which...

  16. 78 FR 23465 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-19

    ... AD was prompted by reports of early fatigue cracks at chem-mill areas on the crown skin panels. This AD requires repetitive inspections for cracking of the fuselage skin at certain locations at chem-mill areas, and repair if necessary. We are issuing this AD to detect and correct fatigue cracking...

  17. 77 FR 65642 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-30

    ... the fuel cross-feel valve is powered by the battery direct current (DC) bus. AAL added that the wing... identification statement to alert maintenance personnel of the importance of regulatory compliance, as well...

  18. 77 FR 56170 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-12

    ... protective surface coating to attach pins of the horizontal stabilizer rear spar. This proposed AD would... receive about this proposed AD. Discussion We received reports of pins with an unapproved surface coating... and corrosion protective surface coating was used by a supplier. The pins were installed on...

  19. 78 FR 21276 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-10

    ... nuts might have been over-torqued. Over-torqued nuts are at risk of fracture. Fractured nuts could... fractures could lead to additional nut or bolt fractures within that support rib, and these additional fractures could cause the joint to be compromised. We are proposing this AD to detect and correct...

  20. 78 FR 65166 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-31

    ... Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Nathan Weigand, Aerospace..., describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail... information about this AD, contact Nathan Weigand, Aerospace Engineer, Airframe Branch, ANM-120S, FAA,...

  1. 78 FR 37497 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-06-21

    ... existing AD, which requires an inspection to determine if certain motor operated valve (MOV) actuators for... CONTACT: Rebel Nichols, Aerospace Engineer, Propulsion Branch, ANM-140S, FAA, Seattle Aircraft... electrical current to flow through certain MOV actuators into the fuel tank. The new MOV actuators...

  2. 78 FR 56182 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-12

    ... the potential for an electrical current to flow through certain motor-operated shutoff valve actuators... if certain motor-operated shutoff valve actuators for the fuel tanks are installed, and related... Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Rebel Nichols,...

  3. 76 FR 59590 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-09-27

    ... repetitive inspections for cracking of the aft pressure bulkhead at station (STA) 1582, repair or replacement of any cracked bulkhead, and eventual replacement of the aft pressure bulkhead at STA 1582 with a new... and tear strap splices of the aft pressure bulkhead at STA 1582 due to fatigue. We are proposing...

  4. 77 FR 70362 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-11-26

    ..., along the bend radius of the chord on several airplanes. This AD requires a general visual inspection to... main entry door number 1 upper main sill outer chord, along the bend radius of the chord, which could..., along the bend radius of the chord on several airplanes. We are issuing this AD to detect and...

  5. 78 FR 43766 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-22

    ... cracking of the rear spar upper chord radius; for certain other airplanes, repetitive inspections for..., repetitive inspections for cracking of the rear spar upper chord radius; for certain other airplanes... horizontal flange. (3) Do a detailed or HFEC inspection for cracking in the rear spar upper chord radius....

  6. 77 FR 50407 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-21

    ... modification of the outboard radius of the lower corners of the door frame and reinforcement of the cross beam... inspections. Since we issued that AD, we have received additional reports of fatigue cracking in the radius of... radius of the lower corners of the door frame and reinforcement of the cross beam of the forward...

  7. 76 FR 81879 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-29

    ... radius of the chord on several airplanes. This action revises the original NPRM by reducing certain... number 1 upper main sill outer chord, along the bend radius of the chord, which could result in loss of... chord, along the bend radius of the chord on several airplanes. We are issuing this AD to detect...

  8. 77 FR 69747 - Airworthiness Directives; The Boeing Company Model Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-11-21

    ... adds inspections for cracks in the BS 727 frame outboard chords and the radius of the auxiliary chord... outboard chord at BS 727 and in the radius of the auxiliary chord on airplanes that were not affected by... radius of the auxiliary chord, for certain airplanes. That NPRM also proposed to remove the...

  9. 77 FR 48423 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-14

    ... AD was prompted by reports of chem-mill step cracking on the aft lower lobe fuselage skins. This AD requires inspections of the fuselage skin at the chem- mill steps, and repair if necessary. We are issuing this AD to detect and correct cracking on the aft lower lobe fuselage skins, which could result...

  10. 77 FR 57529 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-18

    ... for cracking of the fuselage skin along chem- mill steps at certain crown skin and shear wrinkle areas... to non-chem-mill areas at antenna and door bearstrap installations, and shear wrinkle areas at.... (h) Inspections of Shear Wrinkle Areas For Groups 2, 5, and 6 airplanes as identified in...

  11. 77 FR 57539 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-18

    ... inspections for cracking of the fuselage skin along chem-mill steps at certain crown skin and shear wrinkle... adjacent to non-chem-mill areas at antenna and door bearstrap installations, and shear wrinkle areas at...-1312, Revision 1, dated March 14, 2012. (h) Inspections of Shear Wrinkle Areas For Group 1 airplanes...

  12. 77 FR 54856 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-06

    ... structural re-evaluation by the manufacturer, which identified elements within the wing trailing edge flap... correct fatigue cracking of the wing trailing edge structure, which could result in compromised structural... elements within the wing trailing edge flap area, which qualified as SSI. An SSI is defined as a...

  13. 77 FR 45515 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-01

    ... detect and correct such cracking, which could result in the wing structure not supporting the limit load condition, which could lead to loss of the structural integrity of the wing. DATES: We must receive comments... fastener of the wing bulkhead clip attachment to the stringer. If undetected, a crack in the stringer...

  14. 77 FR 54854 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-06

    ... to diode fire card 285U0072-1 in the M826 automatic fire overheat logic test system cardfile... 21, 2008), we received reports of continued water damage to diode fire card 285U0072-1 in the M826... reports of continued water damage to diode fire card 285U0072-1 in the M826 automatic fire overheat...

  15. 77 FR 11416 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-27

    ... from the manufacturer that center overhead stowage (COS) boxes could fall from their supports under.... This proposed AD would require modifying COS boxes by installing new brackets, stiffeners, and hardware as needed. We are proposing this AD to prevent detachment of COS boxes at forward load levels...

  16. 76 FR 77157 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-12

    .... Additionally, this proposed AD would require installing Aero-Engine database (AEDB) software in the airplane..., environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing... actions required by paragraph (g) of this AD, install Aero-Engine database software, software part...

  17. 78 FR 45054 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-26

    ... locator transmitter (ELT), and corrective action if necessary. This AD was prompted by a report of a fire involving a Honeywell fixed ELT. We are issuing this AD to prevent a fire in the aft crown of the airplane, or to detect and correct discrepancies within the ELT that could cause such a fire. DATES: This AD...

  18. 77 FR 45518 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-01

    ... occurred at the end fastener of the wing bulkhead clip attachment to the stringer. If undetected, a crack... cracking, which could result in the wing structure not supporting the limit load condition, which could lead to loss of structural integrity of the wing. DATES: We must receive comments on this proposed...

  19. 77 FR 54798 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-06

    ... operators to use the AMM, the NPRM (76 FR 62667, October 11, 2011) would put the UPS mechanics in an untenable situation. Mechanics following AMM procedures in the nose area of these two airplanes...

  20. 78 FR 48835 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-12

    ... requires repetitive detailed inspections for cracking of the aft tension tie channels from body station (BS... proposed AD. Discussion On August 2, 2007, we issued AD 2007-16-19, Amendment 39-15158 (72 FR 45151, August... body station (BS) 1120 to BS 1220 and from BS 880 to BS 1100, and corrective actions if necessary....

  1. 78 FR 57049 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-17

    ... Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 57, Wings. (e) Unsafe... and corrective actions if necessary, and if necessary, a detailed inspection to determine the nut type..., Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, Washington 98057-3356; phone:...

  2. 78 FR 23694 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-22

    ... airplanes. This proposed AD was prompted by a report of a broken forward support fitting at the inboard... fitting assemblies of the inboard track of the left and right inboard flaps for cracking, and corrective... fitting assembly, which could result in loss of inboard flap control and subsequent loss of...

  3. 78 FR 14731 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-07

    ... outboard flange of the longeron extension fittings, which attach to the wing-to- body fairing support frame. This proposed AD would require repetitive inspections of the longeron extension fittings for cracking... longeron extension fittings, which can become large and adversely affect the structural integrity of...

  4. 78 FR 58962 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-25

    ... ignition source (e.g., hot brakes or engine exhaust nozzle), consequently leading to a fuel-fed fire. DATES... brakes or engine exhaust nozzle), consequently leading to a fuel-fed fire. (f) Compliance Comply with... 747-28-2315, dated January 11, 2012. (1) Do either a general visual inspection or ultrasonic...

  5. 78 FR 48826 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-12

    ... could cause a fuel leak near an ignition source (e.g., hot brakes or engine exhaust nozzle... a fuel leak near an ignition source (e.g., hot brakes or engine nozzle), consequently leading to a... (e.g., hot brakes or engine nozzle), consequently leading to a fuel-fed fire. (f) Compliance...

  6. 78 FR 49237 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-13

    ... could cause a fuel leak near an ignition source (e.g., hot brakes or engine exhaust nozzle..., which could cause a fuel leak near an ignition source (e.g., hot brakes or engine exhaust nozzle... engine exhaust nozzle), consequently leading to a fuel-fed fire. (f) Compliance Comply with this...

  7. 77 FR 37831 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-25

    ... report summarizing each substantive verbal contact we receive about this proposed AD. Discussion We... statement would serve as direct communication to maintenance personnel that there is an AD associated with... Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate...

  8. 78 FR 42720 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-17

    ... airplane reaching its limit of validity (LOV) of the engineering data that support the established... personal information you provide. We will also post a report summarizing each substantive verbal contact we... element of those initiatives is the requirement to establish a limit of validity (LOV) of the...

  9. 78 FR 27010 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-09

    ... adds airplanes to the applicability. This AD was prompted by reports that the work sequence and..., ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil.... (e) Unsafe Condition This AD was prompted by reports that the work sequence and procedures...

  10. 77 FR 37332 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-21

    ... repetitive ultrasonic inspections for cracking of the bulkhead, and repair if necessary; and an option for... extend the repetitive intervals by also doing repetitive ultrasonic inspections for cracking of the... airplanes, add an option to extend the repetitive intervals by also doing repetitive ultrasonic...

  11. 77 FR 16188 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-20

    ... (HFEC) and ultrasonic (UT) inspections for cracking of the termination fitting at certain bolt locations...) High Frequency Eddy Current and Ultrasonic Inspections of Termination Fitting and Repair For any..., do HFEC and ultrasonic inspections for cracking of the forward and aft sides of the...

  12. 77 FR 33619 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-07

    ... -400ER series airplanes. That AD currently requires replacing the separation link assembly on the applicable entry and service doors with an improved separation link assembly, and doing related investigative... replacing the separation link assembly on the applicable entry and service doors with an improved...

  13. 77 FR 58334 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-20

    ... separation between the wire bundle and the hydraulic tubing in the main landing gear (MLG) wheel well. This... applicable. We are proposing this AD to detect and correct possible damage caused by insufficient separation... condition was caused by inadequate separation between the wire bundle and the hydraulic line....

  14. 78 FR 59798 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-30

    ... was arcing to hydraulic tubing and caused by insufficient separation between the wire bundle and the... possible damage caused by insufficient separation between the wire bundles and hydraulic ] tubing to... installation based on whether there is sufficient separation between the wire bundle and hydraulic...

  15. 77 FR 6692 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-09

    ... information identified in this proposed AD, contact Goodrich Corporation, Sensors and Integrated Systems, 100... Corporation, Sensors and Integrated Systems, 100 Panton Road, Vergennes, Vermont 05491; phone: 802-877-4580... airplane. (d) Subject Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of...

  16. 78 FR 66859 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-11-07

    ... airplanes. This proposed AD was prompted by reports of bearing damage at certain trailing edge (TE) flap support rib assemblies. This proposed AD would require inspecting certain TE flap support rib assemblies... TE flap support bearings, which can result in damage to the TE rotary actuators and consequent...

  17. 78 FR 70214 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-11-25

    ... issuing this AD to detect and correct fatigue cracks in the fuselage skin that can propagate and grow, and... the economic burden on any operator or increase the scope of this AD. Costs of Compliance We estimate... economic impact, positive or negative, on a substantial number of small entities under the criteria of...

  18. 78 FR 60676 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-02

    ... reports of worn or incorrectly assembled latches on main deck escape slides installed on airplane doors... (78 FR 9346). The NPRM proposed to require determining if the latches on main deck escape slides... after the effective date of this AD: Determine if the latches in the main deck escape slide/rafts...

  19. 78 FR 22435 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-16

    ... become large and cause the floor beams to become severed and result in rapid decompression or reduced... structural design details, or globally. Global fatigue damage is general degradation of large areas of... occurs in a large structural element such as a single rivet line of a lap splice joining two large...

  20. 77 FR 29212 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-05-17

    ... retention bolts, replacement of existing titanium bolts with new Inconel bolts, and related investigative... fractured or missing latch pin retention bolts, replacement of existing titanium bolts with new Inconel... Inspections Replacing latch pin retention bolts made of titanium with new Inconel bolts, in accordance...

  1. 77 FR 6522 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-08

    ... inspections for fractured or missing latch pin retention bolts, replacement of existing titanium bolts with... titanium with new Inconel bolts; replacing the latch pin fitting assembly; repairing the lower sill of the... necessary. Replacing latch pin retention bolts made of titanium with new Inconel bolts, if...

  2. 78 FR 35749 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-06-14

    ... strut forward dry bay, which could result in hydrogen embrittlement of the titanium forward engine mount... hydrogen embrittlement of the titanium forward engine mount bulkhead fittings, and consequent inability...

  3. 77 FR 63266 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-16

    ..., reinforcement straps were not bonded to the center overhead stowage bins in the passenger compartment. For certain airplanes, this proposed AD would require performing an inspection of reinforcement straps to ensure they are correctly bonded to the center overhead stowage bins, and bonding the...

  4. 78 FR 25377 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-01

    ... and -900ER series airplanes. This AD was prompted by a report of leaking fuel from the wing leading... drain path in the wing leading edge area, forward of the wing front spar, and doing all applicable... wing leading edge, and draining inboard and onto the engine exhaust nozzle, which could result in...

  5. 77 FR 64696 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-23

    ... flammable fluid leaks from the wing leading edge area onto the engine exhaust area. This AD requires modification of the fluid drain path in the leading edge area of the wing. We are issuing this AD to prevent... modifying the fluid drain path in the leading edge area of the wing. Comments We gave the public...

  6. 77 FR 24835 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-26

    ... prompted by reports of cracking in the upper wing skin at the fastener holes common to the pitch load fittings of the inboard and outboard front spar, which could result in the loss of the strut-to-wing upper... requires repetitive inspections to detect fatigue cracking in the wing skin, and corrective actions...

  7. 77 FR 43178 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-24

    ... eddy current high frequency (ETHF) inspections for cracking on the aft side of the left and right wing.... That NPRM was prompted by reports of cracks of the wing rear spar lower cap at the outboard flap... wing skin or other structure, and consequent loss of the structural integrity of the wing. Since...

  8. 77 FR 15638 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-16

    ... airplanes. That NPRM proposed to require modifying the fluid drain path in the wing leading edge area, forward of the wing front spar, and doing all applicable related investigative and corrective actions. That NPRM was prompted by a report of leaking fuel from the wing leading edge area at the inboard...

  9. 76 FR 78574 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-19

    ... underwing longeron fittings in the wing center section which could result in loss of the primary load path between the fuselage and the wing box, and consequent catastrophic damage to the wing box and failure of the wing. This proposed AD would require repetitive high frequency eddy current (HFEC) inspections...

  10. 78 FR 1772 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-09

    ... actions specified in the existing AD. We are proposing this AD to detect and correct fatigue cracking... if necessary. That AD resulted from several reports of fatigue cracking at that location. We issued that AD to detect and correct such fatigue cracking, which could result in rapid decompression of...

  11. 78 FR 70211 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-11-25

    ... location for fatigue cracking to initiate at a relatively low number of flight cycles. The airplane event..., provides corrosion protection at the fastener locations and that application of the chemical conversion... of compliance (AMOC) to apply alternative corrosion protection coatings under the provisions...

  12. 78 FR 25662 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-02

    ... and right side chords of the fin closure rib for cracking and corrosion, and related investigative and corrective actions if necessary. We are proposing this AD to detect and correct cracking and corrosion in the... corrosion caused by the material properties of 2024-T351 extrusion from which the closure rib chord is...

  13. 77 FR 60891 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-05

    ...) beam outboard end fittings for corrosion, and rework if necessary; and ultrasonic inspections for... beams for cracks and corrosion, and corrective actions if necessary. This AD was prompted by new reports of corrosion damage to the end fittings of the WLG support beams, and one report of...

  14. 77 FR 24831 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-26

    ... corrosion on ATSDs. This AD requires revising the maintenance program to incorporate certain limitations. We are issuing this AD to detect and correct corrosion on ATSDs, which could result in the loss of high...) Unsafe Condition This AD was prompted by multiple reports of corrosion on ATSDs. We are issuing this...

  15. 78 FR 15658 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-12

    ... airplanes. This proposed AD was prompted by reports of spanwise cracks and corrosion in the wing center box... other airplanes, repetitive inspections for damage, cracking, and corrosion of the pressure seal; and repair if necessary. We are proposing this AD to detect and correct cracking and corrosion of the...

  16. 78 FR 63903 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-25

    ... corrosion on bonding jumpers installed on the flight control surfaces. This proposed AD would require repetitive bonding jumper inspections for corrosion, sealant disbond, and insufficient sealant coverage, and... for corrosion damage of the bonding brackets, and corrective actions if necessary, which...

  17. 77 FR 12170 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-29

    ... corrosion and cracking in this area, and corrective actions if necessary. We are issuing this AD to detect and correct such corrosion and cracking, which, if not corrected, could grow and result in structural... proposed to require repetitive inspections for corrosion and cracking in the front spar lower chord at...

  18. 77 FR 50414 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-21

    ... structure, which could result in uncontrolled decompression of the airplane. DATES: We must receive comments...-inch crack common to the fuselage skin was hidden under the drain mast. The crack was likely caused by... hidden by the drain mast. This condition, if not corrected, could result in uncontrolled decompression...

  19. 77 FR 65501 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-29

    ... Teflon sleeving on the wiring, and doing associated actions; and doing repetitive inspections to detect... override pumps with new wiring, installing Teflon sleeving on the wiring, and doing associated actions; and... override pumps, install Teflon sleeving over ] the wiring, and do all associated actions, per...

  20. 78 FR 57053 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-17

    ... chords, inner chord angle of the forward edge frame of the number 5 main entry door cutouts; the frame... issuing this AD to detect and correct such cracks, which could cause damage to the adjacent body structure... chords, inner chord angle of the forward edge frame of the number 5 main entry door cutouts; the...

  1. 78 FR 26286 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-06

    ... the loading of adjacent frames, and result in damage to the adjacent structure and consequent loss of... repetitive inspections for cracking of the overwing frames, and corrective actions if necessary. That NPRM was prompted by multiple reports of cracks of overwing frames. This action revises that NPRM...

  2. 77 FR 731 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-06

    ... (HSTA). This AD requires repetitive inspections, lubrications, and repetitive overhauls of the ball nut..., lubrications, and repetitive repairs/overhauls of the ball nut and ballscrew and attachment (Gimbal) fittings...,940 per inspection cycle. Lubrications 1 or 3 85 None $85 or $255, per 1,641 Between...

  3. 78 FR 24673 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-26

    ... unsafe condition for in-service airplanes. For all future delivered airplanes, the replacement batteries... airplanes. That AD currently requires modification of the battery system, or other actions. This AD requires installing main and auxiliary power unit (APU) battery enclosures and environmental control system...

  4. 78 FR 60670 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-02

    ... cracking at the aft upper corner of the main entry door (MED) 5 cutout. This AD requires inspecting for the... of the door cutout, inspecting for any cracking of the fuselage skin assembly and bear strap in the aft upper corner area of the door cutout, and repairing or modifying the fuselage skin assembly...

  5. 78 FR 16198 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-14

    ... channel. The existing AD resulted from fuel system reviews conducted by the manufacturer. Since we issued that AD, we have identified additional center upper auxiliary fuel tank locations where inspections and... extruded channel. That AD resulted from fuel system reviews conducted by the manufacturer. We issued...

  6. 76 FR 77367 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-13

    ... location were manufactured improperly using anodized aluminum. This AD requires replacing the anodized rub... aluminum. We are issuing this AD to prevent inadequate electrical bonding between the rub strips and...

  7. 77 FR 46943 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-07

    ... installing aluminum gutter reinforcing brackets to the forward and aft drip shield gutters of the MEC; and... original NPRM (75 FR 27966, May 19, 2010) proposed to require installing aluminum gutter reinforcing... safety risk of cracked MEC drip shields by installing aluminum reinforcing brackets (i.e., an...

  8. 78 FR 46540 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-01

    ... methods: ] Federal eRulemaking Portal: Go to http://www.regulations.gov . Follow the instructions for... require operators to repair those conditions in accordance with a method approved by the FAA. Costs of.... product operators Inspection for correct fastener 2 work-hours x $85 per hour = $0 $170 $510...

  9. 78 FR 53078 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-28

    ... methods: Federal eRulemaking Portal: Go to http://www.regulations.gov . Follow the instructions for... with a method that we approve; or Using data that meet the certification basis of the airplane, and...: Estimated Costs Cost on U.S. Action Labor cost Parts cost Cost per product operators Inspections 27...

  10. 78 FR 39633 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-02

    ... requirements of paragraphs (g), (h), (i), (j), (k), and (l) of this AD. (2) Replacing a type A wedge with a...) paragraph (k). paragraph (g) paragraph (l). paragraph (h) paragraph (m). paragraph (i) paragraph (n... paragraph (k) of this AD. (2) For the purposes of this AD, a detailed inspection is: ``An...

  11. 76 FR 71472 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-11-18

    ... seal contacts the 12-o'clock engine strut, and for correct stiffness and vent holes, and doing... edge of the thrust reverser, where the fire seal contacts the 12-o'clock engine strut. The damage has... remained in service for an extended time, damage also could result to the 12-o'clock strut structure...

  12. 78 FR 28764 - Airworthiness Directives; The Boeing Company

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-16

    ... and a bonding jumper, doing certain bonding resistance measurements, and changing the GFI relay..., and do certain $2,635. bonding resistance measurements, and change the GFI relay position, depending... bonding resistance measurements, in accordance with Part 1 of the Accomplishment Instructions of...

  13. 77 FR 31167 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-05-25

    ... pivot pins having improved corrosion resistance, doing repetitive inspections after installing the pivot... with new or reworked pivot pins having improved corrosion resistance, doing repetitive...

  14. 77 FR 59728 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-01

    ... straps, doing a bonding-resistance check and an inspection to determine correct installation of certain... necessary, measuring the electrical resistance of the bonding straps, verifying that brackets have an...-resistance check and an inspection to determine correct installation of certain bonding straps,...

  15. 78 FR 78701 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-27

    ... bonding resistance measurements, and changing the GFI relay position. This AD also requires revising the..., installing ground studs and a bonding jumper, doing certain bonding resistance measurements, and changing the... panel, the required bonding resistance measurements cannot be obtained. In addition, ANA requested...

  16. 77 FR 18719 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-28

    ... requires, for certain airplanes, repositioning or replacing two bonding straps, doing a bonding- resistance... electrical resistance of the bonding straps, verifying that brackets have an acceptable fillet seal, and...-resistance check and an inspection to determine correct installation of certain bonding straps,...

  17. 77 FR 20505 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-05

    ... ground fault interrupter (GFI) feature. This AD also requires an electrical bonding resistance... bonding resistance measurement for certain GFI relays to verify that certain bonding requirements are met.... Inspection of screw 1 work-hour x $85 $0 $85 $59,160. installation and bonding per hour = $85....

  18. 77 FR 24357 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-24

    ..., and measuring the resistance of the modified installation to verify resistance is within specified..., installing new bonding jumpers, and measuring the resistance of the modified installation to verify resistance is within specified limits. Comments We gave the public the opportunity to participate...

  19. 78 FR 17290 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-21

    ... measuring the electrical resistance of the bond from the adapter plate to the airplane structure, and doing... actuator if necessary; and measuring the electrical resistance of the bond from the adapter plate to the... resistance of the bond. If an operator encountered unscheduled removal of P/N MA20A1001-1, that part...

  20. 76 FR 74012 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-11-30

    ... space utilization (OSU) option, was found to be under-strength when subjected to a 9.0 g forward load... Avenue SW., Renton, Washington. For information on the availability of this material at the FAA, call... the OSU option, was found to be under-strength when subjected to a 9.0 g forward load. This...

  1. 78 FR 3363 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-16

    ...-mechanical brake flex shaft (short flexshaft) of the thrust reverser actuation system (TRAS). This proposed... the electro-mechanical brake and center drive unit (CDU) cone brake to verify the holding torque, and... describes a functional test of the electro-mechanical brake and CDU cone brake to verify the holding...

  2. 77 FR 60889 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-05

    ... required by paragraph (h)(2) of this AD is done. (ii) Inspection Option 2: Do a one-time external low-frequency eddy current (LFEC) inspection for cracks of the STA 908 upper butt strap. (iii) Inspection...

  3. 76 FR 81890 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-29

    ... the following repetitive inspections, depending on configuration: High frequency eddy current (HFEC) and low frequency eddy current (LFEC) inspections for cracking of the skin and bear strap at the... inspection for cracking along the edge of the skin and bear strap. (3) Do a low frequency eddy current...

  4. 77 FR 32918 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-04

    ... repetitive inspections (detailed, external low frequency eddy current (LFEC), or internal LFEC) for cracks... Option 2: Do a one-time external low-frequency eddy current (LFEC) inspection for cracks of the STA 908... doubler, and lower butt strap; an open-hole high frequency eddy current (HFEC) inspection for cracks...

  5. 77 FR 49396 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-16

    ... option for installing a redesigned aft hinge fitting with the trim already done, instead of trimming an... installing a redesigned aft hinge fitting with the trim already done, instead of trimming an existing or new... action in the existing AD) for installing a redesigned aft hinge fitting designed with the trim...

  6. 78 FR 23468 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-19

    ... (j)(2) of this AD regarding the language in the service information. In addition, we added a..., and (4) Will not have a significant economic impact, positive or negative, on a substantial number...

  7. 77 FR 31758 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-05-30

    ... output from a radio altimeter channel and correct improper autothrottle system response to that erroneous... erroneous output from a single radio altimeter channel, which resulted in premature autothrottle retard... from a radio altimeter channel, which could result in premature autothrottle landing flare retard...

  8. 78 FR 39193 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-01

    ..., 2012, which describes reduced repetitive intervals for the non- destructive test (NDT) ultrasonic... ultrasonic inspection of the spindle has been done and the spindle has been confirmed not to be severed. We...)(3) to prohibit the application of any plating to the carriage using any high velocity oxygen...

  9. 77 FR 40832 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-11

    ... the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Ana Martinez Hueto, Aerospace... this AD, Ana Martinez Hueto, Aerospace Engineer, Cabin Safety and Environmental Systems Branch,...

  10. 77 FR 20511 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-05

    ..., measuring the electrical conductivity on the aluminum upper compression pads 2 and 3 as applicable... Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket... the Docket Office (phone: 800-647-5527) is Document Management Facility, U.S. Department...

  11. 78 FR 17285 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-21

    ... of stiff operation of the elevator pitch control system and jammed elevator controls. This AD... issuing this AD to prevent moisture from collecting and freezing on the elevator control system components... airborne warning and control system (AWACS) airplanes; and line numbers 972 through 974. However,...

  12. 76 FR 77371 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-13

    ... ensure that a fuel filter impending bypass condition due to gross fuel contamination is detected in a... prevents the display of an advisory message to the flightcrew of a left engine fuel filter contamination... malfunction event due to fuel contamination. We are issuing this AD to correct the unsafe condition on...

  13. 78 FR 72791 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-04

    ... inspections of the in-tank fuel boost pump wiring, installation of sleeving over the in-tank fuel boost pump... also requires replacement of the wire bundles for the wing and center fuel boost pumps, installation of... cracking, and repair if necessary. This new AD also requires revising the maintenance program...

  14. 78 FR 14934 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-08

    ... of the wiring and surrounding Teflon sleeves of the fuel tank boost pumps and override/jettison pumps... maintenance program to incorporate changes to the airworthiness limitations section. We are proposing this second SNPRM to detect and correct chafing of the fuel pump wire insulation and consequent exposure...

  15. 77 FR 61731 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-11

    ... repetitive inspections of the in-tank fuel boost pump wiring to detect chafing of the wire insulation... installation of sleeving over the in- tank fuel boost pump wires. The existing AD also requires repetitive... AD would require replacement of the wire bundles for the wing and center fuel boost pumps with...

  16. 78 FR 45898 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-30

    ... supplemental notice of proposed rulemaking (SNPRM) proposed to require revising the maintenance program to incorporate a revision to the Airworthiness Limitations Section of the maintenance planning data (MPD... total loss of boost pump pressure of the fuel feed system, followed by loss of fuel system suction...

  17. 77 FR 54793 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-06

    ... maintenance action after landing to safely restart the pump. We have not changed the final rule regarding this... latched off until the fault is cleared through maintenance action and verified that the pump and the... detect a pump running in an empty fuel tank. We are issuing this AD to reduce the potential of...

  18. 78 FR 49217 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-13

    .... That NPRM proposed to retain repetitive inspections of the in-tank fuel boost pump wiring, installation of sleeving over the in-tank fuel boost pump wires, repetitive inspections of a certain electrical... for the wing and center fuel boost pumps, installation of convoluted liners, and related...

  19. 78 FR 14722 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-07

    ... total loss of boost pump pressure of the fuel feed system, followed by loss of fuel system suction feed... revise the maintenance program to incorporate a revision to the Airworthiness Limitations Section of the maintenance planning data (MPD) document. We are proposing this supplemental NPRM to detect and...

  20. 77 FR 2442 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-18

    ... maintenance program to incorporate Airworthiness Limitations (AWLs) No. 28-AWL-27 and No. 28-AWL-28. This AD... requires an alternative functional test for the left and right override/jettison pumps. We are issuing this... dry operation of the main tank boost pumps and center auxiliary tank override and jettison pumps....

  1. 78 FR 39571 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-02

    ... loss of boost pump pressure of the fuel feed system, followed by loss of fuel system suction feed... capability of the fuel system, which, in the event of total loss of the fuel boost pumps, could result in... identifications, and the second error is an airplane maintenance manual (AMM) procedure referred to in the...

  2. 78 FR 46532 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-01

    ... loss of boost pump pressure of the fuel feed system, followed by loss of fuel system suction feed... revise the maintenance program to incorporate a revision to the Airworthiness Limitations Section of the maintenance planning data (MPD) document, and to remove airplanes from the applicability. We are...

  3. 78 FR 63431 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-24

    ... would require repetitive inspections for cracking of the aft support fitting for the main landing gear... the main ] landing gear (MLG) beam, and the rear spar upper chord and rear spar web. We are...

  4. 77 FR 37781 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-25

    ... the main landing gear to extend without restriction and attempt to lock into position under high... assemblies, which could result in landing gear collapse during touchdown, rollout, or taxi. DATES: This AD is... (ATA) of America Code 32: Main landing gear. (e) Unsafe Condition This AD was prompted by reports...

  5. 76 FR 82210 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-30

    ... retract actuator fuse pin can cause the main landing gear (MLG) to extend without restriction and attempt... prevent structural damage to the side and drag brace lock assemblies, which could result in landing gear... fractured retract actuator fuse pin can cause the main landing gear (MLG) to extend without restriction...

  6. 77 FR 32889 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-04

    ... trunnion lower housing of the main landing gear (MLG), which could result in an incorrect MLG emergency... pins could also result in a possible landing gear collapse causing a runway excursion during take-off... gear (MLG), which could result in an incorrect MLG emergency landing break-away sequence. We...

  7. 77 FR 6685 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-09

    ... requires an inspection to detect cracks and fractures of the outboard hinge fitting assemblies on the... fractures found before the currently-required inspection cycle compliance times on certain airplanes. This... detect cracks and fractures of the outboard hinge fitting assemblies on the trailing edge of the...

  8. 77 FR 61550 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-10

    ... fracture and failure of the skin panels of the fuselage, and consequent rapid decompression of the airplane... fracture and failure of the skin panels of the fuselage, and consequent rapid decompression of the...

  9. 78 FR 68345 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-11-14

    ... report of the fracture of an inboard actuator attach fitting of the outboard flap. An inspection of the...@faa.gov . SUPPLEMENTARY INFORMATION: Discussion We received a report a report of the fracture of a No. 7 inboard actuator attach fitting of the outboard flap. It was determined that the fracture...

  10. 78 FR 49229 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-13

    ... corrosion cracking of the forward trunnion pins, which could result in fracture of the pins and consequent... prevent stress corrosion cracking of the forward trunnion pins, which could result in fracture of the pins... AD to prevent stress corrosion cracking of the forward trunnion pins, which could result in...

  11. 77 FR 24643 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-25

    ... airplanes. This proposed AD was prompted by a report of in-flight fracture of the right windshield (window 1... the fracture of the inner pane of the first officer's windshield (right window 1). This windshield fracture resulted in total loss of the first officer's outside visibility and small shards of...

  12. 78 FR 61164 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-03

    ... lugs, and inner cylinder lugs, which could result in fracture of the pivot joint components and... fracture of the pivot joint components and consequent MLG collapse. (f) Compliance Comply with this...

  13. 77 FR 2669 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-19

    ... detect and correct fatigue cracking of the fuselage skin, which could cause the fuselage skin to fracture..., which could cause the fuselage skin to fracture and fail, and result in rapid decompression of the... and correct fatigue cracking of the fuselage skin, which could cause the fuselage skin to fracture...

  14. 77 FR 60285 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-03

    ... (pivot joint), which could result in fracture of the MLG pivot joint components and consequent collapse... axle and shock strut inner cylinder lugs (pivot joint), which could result in fracture of the MLG...

  15. 77 FR 36134 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-18

    ... fracture and failure of the fuselage skin panels, and consequent rapid decompression of the airplane. DATES... fuselage skin panels at the chem-mill steps, which could result in sudden fracture and failure of...

  16. 78 FR 9 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-02

    ... skin to fracture and fail, and result in rapid decompression of the airplane. DATES: This AD is... and correct fatigue cracking of the fuselage skin, which could cause the fuselage skin to fracture...

  17. 77 FR 39153 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-02

    ..., which could result in a fracture; fracture of both the inboard and outboard carriage spindles, at the..., could result in fracture of the spindle. One fractured carriage spindle on a flap can be compensated for with pilot inputs to the aileron or rudder (increasing pilot workload). However, fracture of both...

  18. 76 FR 72853 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-11-28

    ... result in sudden fracture and failure of the fuselage skin panels, and consequent rapid decompression of... fracture and failure of the fuselage skin panels, and consequent rapid decompression of the airplane...-mill steps, which could result in sudden fracture and failure of the fuselage skin panels,...

  19. 77 FR 73897 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-12-12

    ... report of in-flight fracture of the right windshield (window 1) on the flight deck and multiple reports... fracture of the right windshield (window 1) on the flight deck and multiple reports of electrical arcs...

  20. 77 FR 25647 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-05-01

    ... fracture of the MLG pivot joint components and consequent collapse of the MLG. DATES: We must receive... strut inner cylinder lugs (pivot joint) could result in fracture of the MLG pivot joint components and... result in fracture of the MLG pivot joint components and consequent collapse of the MLG. (f)...

  1. 78 FR 27315 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-10

    ... pedal assemblies. We are proposing this AD to prevent fracture of the rudder pedal pushrod connecting..., could result in a fracture of the rudder pedal pushrod connecting bolts during pedal use, which could... pedal pushrod connecting bolts in the rudder pedal assembly. We are issuing this AD to prevent...

  2. 78 FR 60660 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-02

    ... fatigue cracking of the skin panels, which could result in sudden fracture and failure of the skin panels... fracture and failure of the skin panels of the fuselage, and consequent rapid decompression of the...

  3. 77 FR 34881 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-12

    ... this AD to prevent complete fracture of the crown frame assembly, and consequent damage to the skin and... drawings. This condition, if not corrected, could result in complete fracture of the crown frame assembly... left buttock line (LBL) 15.0, station (STA) 320. We are proposing this AD to prevent complete...

  4. 78 FR 17294 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-21

    ... -300ER series airplanes. This AD was prompted by reports of in-service events related to electrical power system malfunctions resulting in damage to electrical load management system (ELMS) P200 and P300 power..., Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207;...

  5. 77 FR 47563 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-09

    ..., and corrective action if necessary; replacing the aft air-intake duct assembly with a new or modified... cable aft pressure seals and corrective action if necessary; replacing the aft air-intake duct assembly with a new or modified aft air-intake duct assembly and installing a dripshield; and installing...

  6. 77 FR 42964 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-23

    ... Airworthiness by ] incorporating new limitations for fuel tank systems to satisfy Special Federal Aviation... incorporating new limitations for fuel tank systems to satisfy Special Federal Aviation Regulation No. 88..., ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of...

  7. 78 FR 66254 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-11-05

    .... Inspection (new action) 259 work-hours x 0 $22,015 per $1,849,260 per $85 per hour = inspection cycle..., 2013. (b) Affected ADs This AD supersedes AD 2009-10-06, Amendment 39-15901 (74 FR 22424, May 13,...

  8. 76 FR 82207 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-30

    ... the flightcrew due to hypoxia (lack of oxygen in the body), and consequent loss of control of the... not aware of cabin depressurization. The flightcrew also were not aware that passenger oxygen masks... flightcrew due to hypoxia (lack of oxygen in the body), and consequent loss of control of the...

  9. 77 FR 60296 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-03

    ... lack of oxygen in the body), and consequent loss of control of the airplane. DATES: This AD is... incapacitation of the flightcrew due to hypoxia (a lack of oxygen in the body), and consequent loss of control of... oxygen in the body), and consequent loss of control of the airplane. (f) Compliance Comply with this...

  10. 77 FR 55159 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-07

    ... airplanes. That NPRM proposed to require an inspection for affected serial numbers of the crew oxygen mask stowage box units; and replacement of the crew oxygen mask stowage box unit with a new crew oxygen mask stowage unit, if necessary. That NPRM was prompted by reports indicating that certain crew oxygen...

  11. 77 FR 6518 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-08

    ... deck. This proposed AD would require replacing the low-pressure oxygen hoses with non-conductive low-pressure oxygen hoses in the flight compartment. We are proposing this AD to prevent electrical current from passing through the low- pressure oxygen hose internal anti-collapse spring, which can cause...

  12. 78 FR 23110 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-18

    ..., -300ER, and 777F series airplanes. This AD was prompted by a report that during a test of the oxygen system, an operator found that the passenger oxygen masks did not properly flow oxygen, and that a loud... inspection of certain areas of the airplane oxygen system to ensure clamshell couplers are installed...

  13. 77 FR 41045 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-12

    ... low-pressure oxygen hoses with non-conductive low-pressure oxygen hoses in the flight compartment. We are issuing this AD to prevent electrical current from passing through the low-pressure oxygen hose internal anti-collapse spring, which can cause the low-pressure oxygen hose to melt or burn, and...

  14. 78 FR 63130 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-23

    ... the low-pressure oxygen hoses with non-conductive low-pressure oxygen hoses in the stowage box and... internal, anti-collapse spring of the low-pressure oxygen hose, which can cause the low- pressure oxygen hose to melt or burn and lead to an oxygen-fed fire on the flight deck. DATES: We must receive...

  15. 77 FR 55768 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-11

    ... prompted by a report that during a test of the oxygen system, an operator found that the passenger oxygen masks did not properly flow oxygen, and that a loud noise occurred in the overhead area, which was... airplane oxygen system to ensure clamshell couplers are installed and fully latched, and corrective...

  16. 78 FR 49978 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-16

    ... currently requires repetitive inspections for cracking and corrosion of the aft pressure bulkhead, and... actions if necessary. This proposed AD would also limit corrosion and cracking repairs of the aft pressure... proposing this AD to detect and correct corrosion or cracking of the aft pressure bulkhead, which...

  17. 78 FR 42900 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-18

    ... well pressure floor and a preventive modification or permanent repair, as applicable. We are proposing this AD to prevent cracking in the main wheel well pressure floor, which could result in reduced... the ends of the pressure floor reinforcing beads at stations 930 and 940 in the main wheel well....

  18. 77 FR 5386 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-03

    .... FOR FURTHER INFORMATION CONTACT: Nenita Odesa, Aerospace Engineer, Airframe Branch, ANM-120L, FAA, Los...: (562) 627-5234; fax: (562) 627-5210; email: nenita.odesa@faa.gov . ] SUPPLEMENTARY INFORMATION...: Nenita Odesa, Aerospace Engineer, Airframe Branch, ANM-120L, FAA, Los Angeles ACO, 3960...

  19. 77 FR 40828 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-11

    ... available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Nenita Odesa, Aerospace... Boulevard, Lakewood, CA 90712-4137; phone: (562) 627-5234; fax: (562) 627-5210; email: nenita.odesa@faa.gov... Information (1) For more information about this AD, contact Nenita Odesa, Aerospace Engineer, Airframe...

  20. 78 FR 61161 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-03

    ...-140, 1200 New Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Nenita Odesa....odesa@faa.gov . SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM..., contact Nenita Odesa, Aerospace Engineer, Airframe Branch, ANM-120L, FAA, Los Angeles...

  1. 78 FR 4051 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-18

    ... requires replacing the control switches of the forward, aft, and nose cargo doors of Model 747 airplanes; and requires replacing the control switches of cargo doors 1 and 2 of Model 757 series airplanes. This... continue to require replacing the control switches of the forward, aft, and nose cargo doors of Model...

  2. 77 FR 58325 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-20

    ... switch if necessary. We are proposing this AD to prevent power from being supplied to passenger seats when the entertainment control switch is in the OFF position, which could cause an electrical shock... terminator. The airplane manufacturer found that the entertainment control switch has no effect on...

  3. 78 FR 4055 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-18

    ... doing certain wiring changes of the entertainment control switch. We are issuing this AD to prevent power from being supplied to passenger seats when the entertainment control switch is in the OFF... of the entertainment control switch if necessary. Comments We gave the public the opportunity...

  4. 78 FR 42727 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-07-17

    ... systems and other non-essential electrical systems through a switch in the flight compartment in the event... that, in order to minimize the risk of smoke or flames in the passenger cabin, a switch is needed in... systems and other non-essential electrical systems through a switch in the flight compartment in the...

  5. 78 FR 54387 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-04

    ... loads. DATES: This AD is effective October 9, 2013. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of October 9, 2013. ADDRESSES: For... Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD...

  6. 78 FR 25898 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-03

    ... address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service... Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket... September 9, 2010, have a unique configuration at the S-6 lap splice in Section 41. This configuration...

  7. 77 FR 46340 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-03

    ... incorrect torque values. This proposed AD would require, for previously modified airplanes, repetitive..., with corrected torque values, would terminate the requirements of the AD. This proposed AD would also..., Washington. For information on the availability of this material at the FAA, call 425-227-1221. Examining...

  8. 78 FR 18922 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-28

    ... the availability of this material at the FAA, call 425-227-1221. Examining the AD Docket You may... Labor cost Parts cost Cost per product operators Inspection/Torque/Measurement... 3 work-hours x $85 $0... Torque, Latch Pin Measurement, Bolt Replacement, and Rigging At the applicable times specified in table...

  9. 77 FR 7518 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-13

    ... seals of the blocker doors on the thrust reverser torque boxes are not fireproof. This AD requires a one... reverser torque boxes on the engines, and replacing affected aero/fire seals with new, improved aero/fire... availability of this material at the FAA, call 425-227-1221. Examining the AD Docket You may examine the...

  10. 77 FR 21422 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-10

    ... NPRM (76 FR 19278, April 7, 2011) to add a system in the airplane to sound an alarm in the air traffic... experience with GKN windows, the interlayer has not exhibited cracking at the hot and cold...

  11. 78 FR 73739 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-09

    ... CONTACT: Roger Durbin, Airframe Branch, ANM- 120L, FAA, Los Angeles Aircraft Certification Office (ACO...; email: roger.durbin@faa.gov . SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any... more information about this AD, contact Roger Durbin, Airframe Branch, ANM-120L, FAA, Los...

  12. 77 FR 65803 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-31

    ... Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Roger Durbin, Airframe Branch..., California 90712-4137; phone: (562) 627- 5233; fax: (562) 627-5210; email: roger.durbin@faa.gov... AD. (k) Related Information For more information about this AD, contact Roger Durbin, Airframe...

  13. 77 FR 65611 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-30

    .... FOR FURTHER INFORMATION CONTACT: Roger Durbin, Airframe Branch, ANM- 120L, FAA, Los Angeles Aircraft...; fax: (562) 627-5210; email: roger.durbin@faa.gov . SUPPLEMENTARY INFORMATION: Discussion We issued a... about this AD, contact Roger Durbin, Airframe Branch, ANM-120L, FAA, Los Angeles Aircraft...

  14. 77 FR 55773 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-11

    ... receipt. FOR FURTHER INFORMATION CONTACT: Roger Durbin, Aerospace Engineer, Airframe Branch, ANM-120L, FAA...: (562) 627-5233; fax: (562) 627-5210; email: roger.durbin@faa.gov . SUPPLEMENTARY INFORMATION: Comments... this AD. (m) Related Information (1) For more information about this AD, contact Roger...

  15. Remarks on CFD validation: A Boeing Commercial Airplane Company perspective

    NASA Technical Reports Server (NTRS)

    Rubbert, Paul E.

    1987-01-01

    Requirements and meaning of validation of computational fluid dynamics codes are discussed. Topics covered include: validating a code, validating a user, and calibrating a code. All results are presented in viewgraph format.

  16. 78 FR 65193 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-31

    .... FOR FURTHER INFORMATION CONTACT: Suzanne Lucier, Aerospace Engineer, Propulsion Branch, ANM-140S, FAA... more information about this AD, contact Suzanne Lucier, Aerospace Engineer, Propulsion Branch,...

  17. 77 FR 16143 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-20

    ...., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Tung Tran, Aerospace Engineer, Propulsion Branch, ANM..., Aerospace Engineer, Propulsion Branch, ANM-140S, Seattle Aircraft Certification Office (ACO), FAA, 1601...

  18. 78 FR 73457 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-06

    ... limit of validity (LOV) of the engineering data that support the structural maintenance program under 14... mandated programs intended to support the airplane reaching its limit of validity (LOV) of the engineering data that support the established structural maintenance program. For certain airplanes, this...

  19. 77 FR 64242 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-19

    ... of cracking of the forward bulkhead web, web stiffeners, attachment angles, and thermal anti-ice (TAI... report of extensive cracking in the forward bulkhead inner and outer cap angles, stiffeners, and the... the forward bulkhead web, web stiffeners, attachment angles, and thermal anti- ice (TAI) spray...

  20. 78 FR 24037 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-24

    ... adding design features to detect electrical faults and to detect a pump running in an empty fuel tank. We... faults, to detect a pump running in an empty fuel tank, and to ensure that a fuel pump's operation is not...), and agreed that the proposed actions will enhance safety. Request To Delay AD Pending Release...

  1. 77 FR 64704 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-23

    ... of two in-service occurrences on Model 737-400 airplanes of total loss of boost pump pressure of the... fuel system, which, in the event of total loss of the fuel boost pumps, could result in dual engine... that air safety and the public interest require adopting the AD as proposed. Costs of Compliance...

  2. 76 FR 70377 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-11-14

    .... This proposed AD would require adding design features to detect electrical faults, to detect a pump running in an empty fuel tank, and to ensure that a fuel pump's operation is not affected by certain... proposed AD. Discussion The FAA has examined the underlying safety issues involved in fuel tank...

  3. 78 FR 10499 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-02-14

    ... airplanes. That AD currently requires replacing wiring for the fuel boost pumps and override pumps with new... are issuing this AD to detect and correct damaged wiring for the fuel boost pumps and override pumps... continue to require replacing wiring for the fuel boost pumps and override pumps with new...

  4. 77 FR 40307 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-09

    ... June 6, 2008 (73 FR 32248). That NPRM proposed to require performing repetitive operational tests of....'' Lufthansa stated that it is performing the operational test at a 1-D interval that corresponds to up to 33... Actions Within 30,000 flight hours after the effective date of this AD: Perform an operational test of...

  5. 77 FR 41041 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-12

    .... GKN pointed out that the primary cause of arcing that leads to high temperatures is the melting of the... caused by a loose terminal exceeds the rated melting point of the solder, resulting in high voltage...: Ice and rain protection. (e) Unsafe Condition This AD was prompted by several reports of...

  6. 77 FR 72200 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-12-05

    ... couplings. This AD also requires inspecting the assembly of the engine fuel feed manifold rigid and full... on hot engine parts that could lead to a fire. DATES: This AD is effective December 5, 2012. The... in fuel leaks, which could lead to fuel exhaustion, engine power loss or shutdown, or leaks on...

  7. 77 FR 50577 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-22

    ... horizontal stabilizer ballscrew assembly; repetitive lubrication of the horizontal stabilizer trim control... load paths for the ballscrew in the horizontal stabilizer, which could lead to loss of control of the... horizontal stabilizer ballscrew assembly; repetitive lubrication of the horizontal stabilizer trim...

  8. 78 FR 75512 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-12-12

    ... clamps that are not fully cushioned could allow electrical power wiring to come in contact with the exposed metal of the improper clamp, causing a short circuit and subsequent electrical arcing. This..., causing a short circuit and subsequent electrical arcing. We are proposing this AD to prevent...

  9. 77 FR 33129 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-05

    ... Airlines for America (A4A), and James Hurd on behalf of the Families of TWA Flight 800, to extend the comment period. A4A requested a 60-day extension because of the extensive scope and significant potential... results of prototype efforts. A4A stated that this extension would provide operators additional time...

  10. 77 FR 11789 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-28

    ...-icing system for the angle of attack sensor, the total air temperature, and the pitot probes. We are proposing this AD to prevent ice from forming on air data system sensors and consequent loss of or... receive about this proposed AD. Discussion The air data sensor heating system, when ON, heats the...

  11. 77 FR 61548 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-10

    ... require performing a general visual inspection to determine if a certain angle of attack (AOA) sensor with a paddle type vane is installed, and, for affected sensors, performing an operational test of the stall warning system, and replacing the AOA sensor with a new sensor if necessary. We are proposing...

  12. 77 FR 12506 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-03-01

    ... (FQIS) wiring or fuel tank systems to prevent development of an ignition source inside the center fuel tank. We are proposing this AD to prevent ignition sources inside the center fuel tank, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of...

  13. 78 FR 64164 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-28

    ... AD requires, as applicable, repetitive high frequency eddy current (HFEC) and low frequency eddy... this AD within the compliance times specified, unless already done. (g) High Frequency Eddy Current (HFEC) and Low Frequency Eddy Current (LFEC) Inspections At the compliance time specified in paragraph...

  14. 77 FR 43547 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-25

    .... This proposed AD would require repetitive detailed and high frequency eddy current inspections for... service information describes procedures for repetitive detailed and high frequency eddy current (HFEC...: Do detailed and high frequency eddy current (HFEC) inspections of the skin for cracking in the...

  15. 78 FR 15281 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-11

    ... repetitive high frequency eddy current (HFEC) inspections for cracking of the left and right rib hinge..., August 26, 2011) proposed to require repetitive high frequency eddy current (HFEC) inspections for... high frequency eddy current (HFEC) inspection for cracking of the left and right rib hinge bearing...

  16. 78 FR 4042 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-18

    ... cracking of the bulkhead, and repair if necessary; and provides an option for a high frequency eddy current... add an option for a high frequency eddy current inspection for cracking of the critical fastener holes...-16-13, Amendment 39-15152 (72 FR 44753, August 9, 2007)), do a high frequency eddy current...

  17. 76 FR 58098 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-09-20

    ... frequency eddy current or repetitive low frequency eddy current inspections for cracks on the area around... current or repetitive low frequency eddy current inspections for cracks on the area around certain... occurs later, do a high frequency eddy current (HFEC) or low frequency eddy current (LFEC) inspection...

  18. 78 FR 59801 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-09-30

    ... detailed and high frequency eddy current inspections for cracking of the skin around the eight fasteners...). The NPRM proposed to require repetitive detailed and high frequency eddy current (HFEC) inspections... detailed and high frequency eddy current (HFEC) inspections of the skin for cracking in the area around...

  19. 77 FR 66757 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-11-07

    ... requires a one-time mid-frequency eddy current (MFEC) inspection, a low frequency eddy current (LFEC... AD would instead require repetitive external eddy current inspections for cracking of certain fuselage crown lap joints and corrective actions; internal eddy current and detailed inspections...

  20. 78 FR 21854 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-12

    ... applicable, repetitive high frequency eddy current (HFEC) and low frequency eddy current (LFEC) inspections... already done. (g) High Frequency Eddy Current (HFEC) and Low Frequency Eddy Current (LFEC) Inspection...

  1. 78 FR 27001 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-09

    ..., -400, and - 500 series airplanes. That AD currently requires a one-time mid- frequency eddy current (MFEC) inspection, a low-frequency eddy current (LFEC) inspection, and a detailed inspection for damage... external eddy current inspections for cracking of certain fuselage crown lap joints, and corrective...

  2. 78 FR 60804 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-02

    ... fatigue cracking of the aft frame and frame support structure of the forward galley door, which could... frame and frame support structure of the forward galley door. Actions Since AD 2005-07-12, Amendment 39... are issuing this AD to detect and correct fatigue cracking of the aft frame and frame...

  3. 78 FR 31867 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-28

    ... affect the structural integrity of the bulkhead and the horizontal stabilizer support structure and... affect the structural integrity of the bulkhead and the horizontal stabilizer support structure and... fitting, frame supports, forward and aft inner chords, and floor support; doing an inspection for...

  4. 77 FR 37793 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-25

    ... ceiling support structure of Section 41, in airplanes incorporating the overhead space utilization (OSU... ceiling support structure. We are issuing this AD to prevent the forward lowered ceiling panels and support structure from becoming dislodged during a 9.0 g forward load and consequent injury to...

  5. 77 FR 71485 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-12-03

    ... and internal support structure, which could result in uncontrolled decompression of the airplane... issuing this AD to detect and correct cracking in the fuselage skin and internal support structure,...

  6. 78 FR 63135 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-23

    ... General Electric Model CF6- 80C2 engines. The NPRM proposed to require modifying a relay installation and... Federal Register on May 18, 2005 (70 FR 28489). The NPRM proposed to require modifying a...

  7. 77 FR 9518 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-17

    ... airplanes. This AD was prompted by reports of loss of avionics cooling due to an unserviceable relay... requires doing certain wiring changes, installing a new relay and necessary wiring in the CACTCS, and... to require doing certain wiring changes, installing a new relay and necessary wiring in the...

  8. 78 FR 22802 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-04-17

    ... proposed AD would require replacing certain relays and relay sockets, and doing wiring changes. For certain airplanes, this proposed AD would also require installing new relay panels, and removing and installing.... (1) For Model 747-200B, 747-200F, 747-300, and 747SP series airplanes: Replace relays and...

  9. 78 FR 25905 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-03

    ... (ACO), 3960 Paramount Boulevard, Lakewood, California 90712- 4137; phone: (562) 627-5239; fax: (562... provide. We will also post a report summarizing each substantive verbal contact we receive about this... engineering data that support the structural maintenance program. Operators affected by the WFD rule may...

  10. 78 FR 46538 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-01

    ... airplanes. This proposed AD was prompted by reports indicating that a standard fuel tank access door was... locations, and to replace any door with an impact-resistant access door if necessary. This proposed AD also... 5 p.m., Monday through Friday, except Federal holidays. For service information identified in...

  11. 77 FR 76230 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-12-27

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: We are adopting a..., and -900ER series airplanes. This AD was prompted by reports of escape slides failing to deploy...

  12. 77 FR 22686 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-04-17

    ... From the Federal Register Online via the Government Publishing Office DEPARTMENT OF TRANSPORTATION... Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM...-500 series airplanes. This proposed AD was prompted by reports of chem-mill step cracking on the...

  13. 78 FR 47233 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-05

    .../9bf85b85ea3e295d8625735600721055/$FILE/ST02887AT.pdf. Investigation of the cause of the cracks revealed that lack of dimensional controls on the radome manufacturing drawings can result in the introduction of preload stress on the radome during its assembly with the skirt fairing. Preload stress combined with flight or handling...

  14. 77 FR 29857 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-05-21

    ... at stringers S-6L and S-6R, which could result in sudden loss of cabin pressurization and the... and the external reinforcement doubler installation (which does not cut the lap). We partially agree... not have a significant economic impact, positive or negative, on a substantial number of...

  15. 78 FR 61173 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-10-03

    ... update inspection requirements to detect fatigue cracking of principal ] structural elements (PSEs). We are issuing this AD to detect and correct fatigue cracking of various principal structural elements... to require revising the maintenance program to update inspection requirements to detect...

  16. 78 FR 49913 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-08-16

    ... is subject to widespread fatigue damage. This AD requires repetitive high frequency eddy current... are issuing this AD to detect and correct fatigue cracking at the frame-to-floor beam attachment, on... widespread fatigue damage. We are issuing this AD to detect and correct fatigue cracking at the...

  17. 77 FR 57990 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-19

    ... AD was prompted by several reports of fatigue cracking at that location. We are issuing this AD to detect and correct such fatigue cracking, which could result in rapid decompression of the fuselage...) Unsafe Condition This AD was prompted by several reports of fatigue cracks in the aft pressure...

  18. 77 FR 58791 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-24

    ... require revising the maintenance program to update inspection requirements to ] detect fatigue cracking of principal structural elements (PSEs). We are proposing this AD to detect and correct fatigue cracking of... additional analyses of fatigue cracking of PSEs on certain Model 737 airplanes, which included: Crack...

  19. 77 FR 42962 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-23

    ... airplanes. This AD was prompted by reports of fatigue cracks in the lap joints, which initiated at scribe... repair if necessary. We are issuing ] this AD to detect and correct such fatigue cracking, which could... reports of fatigue cracks in the lap joints, which initiated at scribe lines that were made...

  20. 77 FR 10403 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-02-22

    ... of certain doors and flaps was done based on their fatigue-critical nature. This proposed AD would... applicability. We are proposing this AD to detect and correct fatigue cracking of the principal structural... to the airworthiness limitation instructions (ALI). We issued that AD to ensure that fatigue...

  1. 77 FR 37770 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-06-25

    ... airplanes. This AD was prompted by reports of fatigue cracking on the lower main sill inner chord of the..., and repair if necessary. We are issuing this AD to detect and correct fatigue cracking on the lower... prompted by reports of fatigue cracking on the lower main sill inner chord of the hatch opening of...

  2. 77 FR 3187 - Airworthiness Directives; the Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-23

    ... certain Model 767-200 and -300 series airplanes. This proposed AD was prompted by reports of fatigue... proposing this AD to detect and correct fatigue cracking on the lower main sill inner chord of the hatch... proposed AD. Discussion We received reports of fatigue cracking on the lower main sill inner chord of...

  3. 78 FR 14719 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-07

    ... skin just above certain lap splice locations is subject to widespread fatigue damage (WFD). This... locations, and repair if necessary. We are proposing this AD to detect and correct fatigue cracking of the... substantive verbal contact we receive about this proposed AD. Discussion Structural fatigue damage...

  4. 76 FR 82111 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-12-30

    ... fire in the fan compartment to spread beyond the firewall and reach the flammable fluid leakage zones... compartment to spread beyond the firewall and reach the flammable fluid leakage zones, resulting in...

  5. Advanced composite stabilizer for Boeing 737 aircraft

    NASA Technical Reports Server (NTRS)

    1978-01-01

    Activities related to development of an advanced composites stabilizer for the Boeing 737 commercial transport are reported. Activities include discussion of criteria and objectives, design loads, the fatigue spectrum definition to be used for all spectrum fatigue testing, fatigue analysis, manufacturing producibility studies, the ancillary test program, quality assurance, and manufacturing development.

  6. Boeing's High Voltage Solar Tile Test Results

    NASA Technical Reports Server (NTRS)

    Reed, Brian J.; Harden, David E.; Ferguson, Dale C.; Snyder, David B.

    2002-01-01

    Real concerns of spacecraft charging and experience with solar array augmented electrostatic discharge arcs on spacecraft have minimized the use of high voltages on large solar arrays despite numerous vehicle system mass and efficiency advantages. Boeing's solar tile (patent pending) allows high voltage to be generated at the array without the mass and efficiency losses of electronic conversion. Direct drive electric propulsion and higher power payloads (lower spacecraft weight) will benefit from this design. As future power demand grows, spacecraft designers must use higher voltage to minimize transmission loss and power cable mass for very large area arrays. This paper will describe the design and discuss the successful test of Boeing's 500-Volt Solar Tile in NASA Glenn's Tenney chamber in the Space Plasma Interaction Facility. The work was sponsored by NASA's Space Solar Power Exploratory Research and Technology (SERT) Program and will result in updated high voltage solar array design guidelines being published.

  7. Boeing XF2B-1 (F2B-1)

    NASA Technical Reports Server (NTRS)

    1931-01-01

    Boeing XF2B-1 (F2B-1): Serving as the prototype for the F2B-1 shipboard fighter, the XF2B-1 differed visually in having a pointed spinner and an unbalanced rudder. Like many aircraft of its day, the Boeing model 69 was powered by a Pratt & Whitney Wasp radial engine.

  8. Company profile: tengion.

    PubMed

    Bertram, Timothy

    2009-05-01

    Founded in 2005, Tengion is a clinical-stage organ regeneration company with products in urologic, vascular and renal regeneration based on its proprietary Autologous Organ Regeneration Platform. Tengion uses biocompatible materials and a patient's own (autologous) cells to assemble neo-organs or neo-tissues that are designed to catalyze the body's innate ability to regenerate. Tengion is a fully-integrated organization, with scalable US and European manufacturing and distribution capabilities, experienced research, development, clinical and commercial teams, and significant intellectual property. The company's corporate headquarters and commercial manufacturing facility are in East Norriton, PA, USA, and its research offices, a development laboratory and a pilot manufacturing facility are located in Winston-Salem, NC, USA. Tengion's product candidates may ultimately address the most critical problems facing organ and tissue failure patients, enabling people to lead healthier lives without donor transplants or the side effects of related therapies.

  9. Final Technical Report. Project Boeing SGS

    SciTech Connect

    Bell, Thomas E.

    2014-12-31

    Boeing and its partner, PJM Interconnection, teamed to bring advanced “defense-grade” technologies for cyber security to the US regional power grid through demonstration in PJM’s energy management environment. Under this cooperative project with the Department of Energy, Boeing and PJM have developed and demonstrated a host of technologies specifically tailored to the needs of PJM and the electric sector as a whole. The team has demonstrated to the energy industry a combination of processes, techniques and technologies that have been successfully implemented in the commercial, defense, and intelligence communities to identify, mitigate and continuously monitor the cyber security of critical systems. Guided by the results of a Cyber Security Risk-Based Assessment completed in Phase I, the Boeing-PJM team has completed multiple iterations through the Phase II Development and Phase III Deployment phases. Multiple cyber security solutions have been completed across a variety of controls including: Application Security, Enhanced Malware Detection, Security Incident and Event Management (SIEM) Optimization, Continuous Vulnerability Monitoring, SCADA Monitoring/Intrusion Detection, Operational Resiliency, Cyber Range simulations and hands on cyber security personnel training. All of the developed and demonstrated solutions are suitable for replication across the electric sector and/or the energy sector as a whole. Benefits identified include; Improved malware and intrusion detection capability on critical SCADA networks including behavioral-based alerts resulting in improved zero-day threat protection; Improved Security Incident and Event Management system resulting in better threat visibility, thus increasing the likelihood of detecting a serious event; Improved malware detection and zero-day threat response capability; Improved ability to systematically evaluate and secure in house and vendor sourced software applications; Improved ability to continuously monitor

  10. Technology Approach: DoD Versus Boeing (A Comparative Study)

    DTIC Science & Technology

    2016-01-01

    they may have affected development time for the C-17 and the Boeing 777. Boeing’s focus on cost, schedule, performance, and market competition is...serve its customers and protect its market share against competition for 50 years into the future. Boeing was also committed to changing and improving...Boeing’s focus during the design and acquisition process was on cost, schedule, performance, and market competition. DoD’s focus during the design and

  11. Boeing prepares AOA sensor for flight test on 767

    NASA Astrophysics Data System (ADS)

    Smith, Bruce A.

    1988-11-01

    The Airborne Optical Adjunct sensor, developed to evaluate the ability of aircraft-mounted longwave infrared systems to supplement ground-based radar in defense against ballistic missiles, is being tested at Boeing Aerospace prior to installation in the Boeing 767 aircraft for flight tests to evaluate the sensor's ability to track and detect missiles. The major objectives of the test program are summarized, and final computer changes are reviewed. The sensing operations involved in the tests are described.

  12. Advanced composite elevator for Boeing 727 aircraft

    NASA Technical Reports Server (NTRS)

    1979-01-01

    Detail design activities are reported for a program to develop an advanced composites elevator for the Boeing 727 commercial transport. Design activities include discussion of the full scale ground test and flight test activities, the ancillary test programs, sustaining efforts, weight status, and the production status. Prior to flight testing of the advanced composites elevator, ground, flight flutter, and stability and control test plans were reviewed and approved by the FAA. Both the ground test and the flight test were conducted according to the approved plan, and were witnessed by the FAA. Three and one half shipsets have now been fabricated without any significant difficulty being encountered. Two elevator system shipsets were weighed, and results validated the 26% predicted weight reduction. The program is on schedule.

  13. Flight test evaluation of drag effects on surface coatings on the NASA Boeing 737 TCV airplane

    NASA Technical Reports Server (NTRS)

    George-Falvy, D.; Sikavi, D. A.

    1981-01-01

    A flight test program was conducted in which the effects of various surface coatings on aerodynamic drag were investigated; results of this program are described in this report. The tests were conducted at NASA-Langley Research Center on the terminal configured vehicle (TCV) Boeing 737 research airplane. The Boeing Company, as contractor with NASA under the Energy Efficient Transport (EET) program, planned and evaluated the experiment. The NASA-TCV Program Office coordinated the experiment and performed the flight tests. The principal objective of the test was to evaluate the drag reduction potential of an elastomeric polyurethane surface coating, CAAPCO B-274, which also has been considered for application on transport airplanes to protect leading edges from erosion. The smooth surface achievable with this type of coating held some promise of reducing the skin friction drag as compared to conventional production type aircraft surfaces, which are usually anodized bare metal or coated with corrosion protective paint. Requirements for high precision measurements were the principal considerations in the experiment.

  14. Boeing Crew Exploration Vehicle Environmental Control and Life Support System Architecture Overview

    NASA Technical Reports Server (NTRS)

    Saiidi, Mo; Lewis, John F.

    2007-01-01

    The Boeing Company under the teaming agreement with the Northrop Grumman Systems Corporation and in compliance with the NASA Phase 1 contract, had the responsibilities for the CEV architecture development of the Environmental control and life support (ECLS) system under the NASA Phase 1 contract. The ECLS system was comprised of the various subsystems which provided for a shirt-sleeve habitable environment for crew to live and work in the crew module of the CEV. This architecture met the NASA requirements to ferry cargo and crew to ISS, and Lunar sortie missions, with extensibility to long duration missions to Moon and MARS. This paper provides a summary overview of the CEV ECLS subsystems which was proposed in compliance with the contract activities.

  15. Flight test of ARINC 741 configuration low gain SATCOM system on Boeing 747-400 aircraft

    NASA Technical Reports Server (NTRS)

    Murphy, Timothy A.; Stapleton, Brian P.

    1990-01-01

    The Boeing company conducted a flight test of a SATCOM system similar to the ARINC 741 configuration on a production model 747-400. A flight plan was specifically designed to test the system over a wide variety of satellite elevations and aircraft attitudes as well as over land and sea. Interface bit errors, signal quality and aircraft position and navigational inputs were all recorded as a function of time. Special aircraft maneuvers were performed to demonstrate the potential for shadowing by aircraft structures. Both a compass rose test and the flight test indicated that shadowing from the tail is insignificant for the 747-400. However, satellite elevation angles below the aircraft horizon during banking maneuvers were shown to have a significant deleterious effect on SATCOM communications.

  16. Smart Companies.

    ERIC Educational Resources Information Center

    Galagan, Patricia A.

    1997-01-01

    Capturing and leveraging knowledge is an important new management trend that is as yet undefined. Some companies are accounting for their intellectual capital and applying it to the company balance sheets. (JOW)

  17. 78 FR 14400 - Southern USA Resources, Inc., Order of Suspension of Trading

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-05

    ... COMMISSION Southern USA Resources, Inc., Order of Suspension of Trading March 1, 2013. It appears to the... securities of Southern USA Resources, Inc. (``Southern USA'') because of questions regarding the accuracy of... company's outstanding shares. Southern USA's securities are quoted on the OTC Link, operated by...

  18. Model BOE Block Program for Rural Schools. Final Report.

    ERIC Educational Resources Information Center

    Spooner, Kendrick L.

    A one-year evaluation was conducted of the Exemplary Business and Office Education (BOE) Program as implemented in seven rural Colorado schools. The individualized program featured a two-period block core curriculum with three or more optional areas of study. Evaluation objectives were to describe the exemplary projects in light of the…

  19. VIEW OF BOEING 737200 FUSELAGE FROM TOP LEVEL OF TAIL ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    VIEW OF BOEING 737-200 FUSELAGE FROM TOP LEVEL OF TAIL DOCK AND. A NEW SAFETY CABLE FROM THE TAIL DOCK WILL ALLOW INSPECTORS TO WALK UP AND DOWN THE FUSELAGE TO CHECK FOR CRACKS OR MISSING FASTENERS. - Greater Buffalo International Airport, Maintenance Hangar, Buffalo, Erie County, NY

  20. RIGHT ENGINE MAINTENANCE ON BOEING 737200. THE COWLING OF THE ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    RIGHT ENGINE MAINTENANCE ON BOEING 737-200. THE COWLING OF THE RIGHT ENGINE IS OPEN, AND THE CREW IS WORKING ON THE JACK SCREWS THAT REGULATE THE FLAPS. MECHANICS WILL CHANGE ALL FUEL AND OIL FILTERS AS WELL AS CHECKING CHIP DETECTORS FOR METAL PARTICLES THAT INDICATE BEARING FAILURE. - Greater Buffalo International Airport, Maintenance Hangar, Buffalo, Erie County, NY

  1. Feasibility study of the Boeing Small Research Module (BSRM) concept

    NASA Technical Reports Server (NTRS)

    1975-01-01

    The design, capabilities, and subsystem options are described for the Boeing Small Research Module (BSRM). Specific scientific missions are defined and the BSRM capability to support these missions is discussed. Launch vehicle integration requirements and spacecraft operational features are also presented.

  2. Chromate-free Exterior Painting for Boeing Commercial Aircraft

    DTIC Science & Technology

    2009-09-01

    vinegar odor pH 4 after mixed Apply with no rinse ASETSDefense2009_JHO.ppt | 8 Engineering, Operations & Technology | Boeing Research...Conventional Boegel EP-II/AC-131-CB Health & Safety Contains Hexavalent chromium pH = 2.1 No Hexavalent chromium pH = 4 Environmental Impact Volume of

  3. Technology Approach: DoD versus Boeing (A Comparative Study)

    DTIC Science & Technology

    1995-01-01

    John Newhouse points out in his book, The Sporty Game, “...there is more technology in the wing than in any other part of an airframe...production...Defense. Nelson, E. (1994, May). Boeing Gets Air- lines on Board. Business Marketing. Newhouse, J. (1982). The Sporty Game. New York: Alfred A. Knopf

  4. Feasibility study of the Boeing Small Research Module (BSRM) concept

    NASA Technical Reports Server (NTRS)

    1975-01-01

    The design, capabilities, and subsystem options for the Boeing Small Research Module (BSRM) are described. Specific scientific missions are defined based on NASA-Ames Research Center requirements and the BSRM capability to support these missions is discussed. Launch vehicle integration requirements and spacecraft operational features are also presented.

  5. Nde Challenges with Future Commercial Aircraft-A Boeing Perspective

    NASA Astrophysics Data System (ADS)

    Kollgaard, J. R.; LaRiviere, S. G.

    2008-02-01

    Commercial aircraft have undergone revolutionary changes in design, configuration and materials. This produces new challenges to the NDE community ranging from process controls of raw materials, to testing and fabrication of structural components, to service damage assessments. As we drive NDE up the value stream, it will become imperative to understand variousprocess parameters and their relationship to product quality. NDE may play a key role in characterizing and controlling those parameters. In production, inspection has become a critical aspect in the processing of large, unitized structures. Penetrant, radiographic, and magnetic particle techniques are less applicable while ultrasonics has taken on a critical role, earlier in the build process. NDE data are acquired over large areas at rates far faster than before, creating challenges in the time required to analyze and document the data. Qualified inspectors, equipment, and techniques are essential. In the field, eddy current and shear wave ultrasonic methods, long a mainstay of aircraft maintenance, are beginning to yield to ultrasonic techniques involving C-scans and linear arrays. The building of new-generation airplanes has revealed shortcomings in existing NDE technology and in some cases enhanced the case for non-traditional methods. This paper will review Boeing's experience with NDE of advanced structures, in particular those present on the Boeing 787, and summarize the Boeing outlook for future NDE needs.

  6. Impact evaluation of lighting retrofit projects at Boeing Commercial Airplane Group under The Energy $avings Plan

    SciTech Connect

    Sullivan, G.P.; Oens, M.A.; Spanner, G.E.

    1994-01-01

    This impact evaluation of two lighting retrofit projects that were recently installed at Boeing Commercial Airplane Group (Boeing) was conducted for the Bonneville Power Administration (Bonneville) as part of an evaluation of its Energy $avings Plan (E$P) Program. The first project was a light-fixture and lighting control retrofit, consisting of five individual measures installed in Building 40-05. The second project was a retrofit of all parking lot lighting on the site. The objective of this impact evaluation was to assess how much electrical energy is being saved at Boeing as a result of the E$P projects and to determine how much the savings cost Bonneville and the region. The impact of the project was evaluated with a combination of engineering analysis, financial analysis, interviews, and submittal reviews (Boeing`s proposals and completion reports).

  7. 76 FR 35336 - Airworthiness Directives; The Boeing Company Model 767 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-06-17

    ... by (1) reports of fuel leaks from certain drain locations of the slat track housing near the engine... results from (1) reports of fuel leaks from certain drain locations of the slat track housing near the engine exhaust nozzle, which could result in a fire when the airplane is stationary, or taxiing at...

  8. 75 FR 61999 - Airworthiness Directives; The Boeing Company Model 767 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-10-07

    ... reports of fuel leaks from certain drain locations of the slat track housing near the engine exhaust... airplanes. This proposed AD results from reports of fuel leaks from certain drain locations of the slat track housing near the engine exhaust nozzles of the wings, which could result in a fire when...

  9. Health hazard evaluation report No. HETA 82-272-1276, Boeing Vertol Company, Philadelphia, Pennsylvania

    SciTech Connect

    Chrostek, W.; Liss, G.M.; Moss, G.

    1983-03-01

    To evaluate employee health complaints, including anxiety, nausea, eye strain, and headache thought possibly related to working under high pressure sodium vapor (HPSV) lamps and working with storage boxes dipped in sulfur, air samples were collected in May and July 1982 for exposures to sulfates, sulfites, and sulfur dioxide. A calibrated photometer was used to measure illumination in units of lux. Self-administered questionnaires were completed. To further assess possible color distortion, investigators administered the Farnsworth-Munsell 100-Hue Test to 15 employees in Building 3-25. Environmental sampling found non-detectable levels of sulfite. The illumination levels in some parts of the building were far less than optimal. Although no serious adverse health effects were noted, symptoms related to the eyes and minor abnormalities of color discrimination, possibly related to HPSV lamps and exposure to sulfur containers, were detected. Recommendations to improve the lighting situation are presented.

  10. 76 FR 41659 - Airworthiness Directives; The Boeing Company Model 747 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-07-15

    ... nor increase the scope of the AD. Costs of Compliance We estimate that this AD affects 215 airplanes of U.S. registry. The new requirements of this AD add no additional economic burden. The current costs for this AD are repeated below for the convenience of affected operators. The actions that...

  11. 75 FR 77793 - Airworthiness Directives; The Boeing Company Model 747 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-12-14

    .... The new requirements of this proposed AD add no additional economic burden. The current costs for this...) paragraph (l). paragraph (g) paragraph (m). Costs of Compliance There are about 772 airplanes of the... labor rate of $85 per work-hour. Based on these figures, the estimated cost of the currently...

  12. 75 FR 77790 - Airworthiness Directives; The Boeing Company Model 767 Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-12-14

    ... current costs for this proposed AD are repeated below for the convenience of affected operators. The...) paragraph (i). paragraph (d) paragraph (j). paragraph (e) paragraph (k). Costs of Compliance There are about... pumps), at an average labor rate of $85 per work-hour. Required parts cost about $336 per...

  13. 76 FR 69685 - Airworthiness Directives; The Boeing Company Model 767-200 and -300 Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-11-09

    ... information describes procedures for repetitive detailed inspections or surface high frequency eddy current... Airplanes Organization Designation Authorization (ODA) whom we have authorized to make those findings. Costs... estimate the following costs to comply with this proposed AD: Estimated Costs Cost on U.S. Action...

  14. 76 FR 44458 - Airworthiness Directives; The Boeing Company Model 747 Airplanes and Model 767 Airplanes Equipped...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-07-26

    ... multiple dual engine flameout events and one total power loss event, in ice-crystal icing conditions. We... the capability to detect ice-crystal icing. Therefore, the anti-ice systems would not be activated...-ice activation in ice-crystal icing conditions. We have made no change to the final rule in...

  15. 75 FR 46868 - Airworthiness Directives; The Boeing Company Model 747 Airplanes and Model 767 Airplanes Equipped...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-08-04

    ..., in ice-crystal icing conditions. This action revises the original NPRM by revising the text of the... flightcrews to the accretion of ice crystals on internal engine surfaces, so that flightcrews can take the... engine needs to be modified to mitigate the risk of flameouts caused by ice crystal accretion....

  16. 75 FR 53843 - Airworthiness Directives; The Boeing Company Model 737-100 and -200 Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-09-02

    ... to be approved, the repair must meet the certification basis of the airplane. Material Incorporated... Model 737-100 and - 200 Series Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION... -200 series airplanes. This AD requires repetitive inspections for cracking and damaged fasteners...

  17. 76 FR 15814 - Airworthiness Directives; The Boeing Company Model 747 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-03-22

    ... to prevent electrical current from flowing through an MOV actuator into a fuel tank, which could... Administration is issuing this AD to prevent electrical current from flowing through a motor operated valve (MOV... measuring the electrical bond resistance between the motor operated valve (MOV) actuators and...

  18. 75 FR 27969 - Airworthiness Directives; The Boeing Company Model 737-100 and -200 Series Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-05-19

    ... cracking and damaged fasteners of certain fuselage frames and stub beams, and corrective actions if... the inboard chord fastener hole of the frame at body station 639, stringer S-16, and corrective... inspections for the repaired or modified frame only. For airplanes on which the modification or repair is...

  19. 75 FR 43097 - Airworthiness Directives; The Boeing Company Model 757 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-07-23

    ... ignition source, in the event of a fault current or lightning strike, which could result in a fuel tank... the event of a fault current, which could result in a fuel tank explosion and consequent loss of the... source, in the event of a fault current or lightning strike, which could result in a fuel tank...

  20. 75 FR 3660 - Airworthiness Directives; The Boeing Company Model 757 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-01-22

    ... airplanes. This proposed AD would require repetitive inspections for corrosion and cracking in the front... Model 757 Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed... side link support fitting at WS 292. We are proposing this AD to detect and correct such corrosion...