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2010-09-23
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Airworthiness Directives; Boeing Model 727 Series Airplanes
Rules and Regulations
D09002ee1bde9d476
D09002ee1bde9d51c
United States
Department of Transportation
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United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 727 series airplanes, that requires an inspection of the bolts used to attach the forward cone bolt to the engine flange to determine if the attachment bolts are either H-11 steel bolts or cadmium-plated bolts. This action also requires replacement of either H-11 steel bolts or cadmium-plated bolts with new corrosion-resistant steel bolts. This action is necessary to prevent undetected cracking of the H-11 bolts or excessive wear of the cadmium- plated bolts, which would compromise the primary load path of the engine support and could result in separation of the engine from the airplane. This action is intended to address the identified unsafe condition.
69 FR 26015
https://www.govinfo.gov/app/details/FR-2004-05-11/04-10374
04-10374
fr11my04-12
RIN 2120-AA64
4910-13-P
Docket No. 2002-NM-273-AD
Amendment 39-13627
AD 2004-09-36
https://www.govinfo.gov/app/details/FR-2004-05-11/04-10374
https://www.govinfo.gov/content/pkg/FR-2004-05-11/html/04-10374.htm
https://www.govinfo.gov/content/pkg/FR-2004-05-11/pdf/04-10374.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
26015
26017
69 FR 26015
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Boeing Model 727 Series Airplanes; Federal Register Vol. 69, Issue
RULE
04-10374
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2004-06-15
Docket No. 2002-NM-273-AD
Amendment 39-13627
AD 2004-09-36
4910-13-P
04-10374
Final rule.
This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 727 series airplanes, that requires an inspection of the bolts used to attach the forward cone bolt to the engine flange to determine if the attachment bolts are either H-11 steel bolts or cadmium-plated bolts. This action also requires replacement of either H-11 steel bolts or cadmium-plated bolts with new corrosion-resistant steel bolts. This action is necessary to prevent undetected cracking of the H-11 bolts or excessive wear of the cadmium- plated bolts, which would compromise the primary load path of the engine support and could result in separation of the engine from the airplane. This action is intended to address the identified unsafe condition.
Effective June 15, 2004.
Daniel F. Kutz, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6456; fax (425) 917-6590.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Boeing,
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
Federal Register
Vol. 69, no. 91
Office of the Federal Register, National Archives and Records Administration
2004-05-11
continuing
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311 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2004-05-11
P0b002ee180973832
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr11my04
https://www.govinfo.gov/app/details/FR-2004-05-11
https://www.govinfo.gov/content/pkg/FR-2004-05-11/pdf/FR-2004-05-11.pdf
https://www.govinfo.gov/content/pkg/FR-2004-05-11/xml/FR-2004-05-11.xml
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2010-09-23
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FR-2004-05-11
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FR
FR-2004-05-11
69
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