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2010-09-22
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Airworthiness Directives; Boeing Model 767 Airplanes
Rules and Regulations
D09002ee1bde1e2f2
D09002ee1bde1e3be
United States
Department of Transportation
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org
United States Government Agency or Subagency
United States
Federal Aviation Administration
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United States Government Agency or Subagency
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 767 airplanes. This AD requires performing a test of the bonding resistance between the engine fuel feed tube fitting and the front spar, applying sealant on a hex nut inside the dry bay, and performing any applicable corrective actions. This AD results from a report that the engine fuel feed tubes were found not electrically bonded to the front spar. We are issuing this AD to prevent an ignition source from entering the fuel tank during a lightning strike event, which could cause a fuel tank explosion.
71 FR 19104
https://www.govinfo.gov/app/details/FR-2006-04-13/06-3478
06-3478
fr13ap06-3
RIN 2120-AA64
4910-13-P
Docket No. FAA-2004-19680
Directorate Identifier 2003-NM-215-AD
Amendment 39-14558
AD 2006-08-04
https://www.govinfo.gov/app/details/FR-2006-04-13/06-3478
https://www.govinfo.gov/content/pkg/FR-2006-04-13/html/06-3478.htm
https://www.govinfo.gov/content/pkg/FR-2006-04-13/pdf/06-3478.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
4 p.
19104
19107
71 FR 19104
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Boeing Model 767 Airplanes; Federal Register Vol. 71, Issue
RULE
06-3478
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2006-05-18
Docket No. FAA-2004-19680
Directorate Identifier 2003-NM-215-AD
Amendment 39-14558
AD 2006-08-04
4910-13-P
06-3478
Final rule.
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 767 airplanes. This AD requires performing a test of the bonding resistance between the engine fuel feed tube fitting and the front spar, applying sealant on a hex nut inside the dry bay, and performing any applicable corrective actions. This AD results from a report that the engine fuel feed tubes were found not electrically bonded to the front spar. We are issuing this AD to prevent an ignition source from entering the fuel tank during a lightning strike event, which could cause a fuel tank explosion.
This AD becomes effective May 18, 2006.
John Vann, Aerospace Engineer, Propulsion Branch, ANM-140S, Seattle Aircraft Certification Office, FAA, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6513; fax (425) 917-6590.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Boeing,
http://dms.dot.gov
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
Federal Register
Vol. 71, no. 71
Office of the Federal Register, National Archives and Records Administration
2006-04-13
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339 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2006-04-13
P0b002ee18094cf26
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr13ap06
https://www.govinfo.gov/app/details/FR-2006-04-13
https://www.govinfo.gov/content/pkg/FR-2006-04-13/pdf/FR-2006-04-13.pdf
https://www.govinfo.gov/content/pkg/FR-2006-04-13/xml/FR-2006-04-13.xml
fdlp
19097
19425
DGPO
2010-09-22
2023-05-03
FR-2006-04-13
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FR
FR-2006-04-13
71
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