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Airworthiness Directives; General Electric Company (GE) CF6-80C2 Series Turbofan Engines
Rules and Regulations
D09002ee1be03477c
D09002ee1be0359ae
United States
Department of Transportation
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United States Government Agency or Subagency
This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CF6-80C2 series turbofan engines. This action supersedes priority letter AD 96-09-01 that currently requires borescope inspections of the rear right hand mount link to determine if the serial number matches those listed in applicable service bulletins as improperly manufactured, and replacement, if necessary, with a serviceable part. This action references a newly revised service bulletin and bases the compliance time on the effective date of this superseding AD for engines installed on McDonnell Douglas MD-11 series aircraft. This amendment is prompted by the availability of the newly revised service bulletin. The actions specified by this AD are intended to prevent rear right hand mount link failure, which could result in engine separation from the aircraft.
61 FR 41951
https://www.govinfo.gov/app/details/FR-1996-08-13/96-20397
96-20397
fr13au96-3
RIN 2120-AA64
4910-13-U
Docket No. 96-ANE-16
Amendment 39-9707, AD 96-16-07
https://www.govinfo.gov/app/details/FR-1996-08-13/96-20397
https://www.govinfo.gov/content/pkg/FR-1996-08-13/html/96-20397.htm
https://www.govinfo.gov/content/pkg/FR-1996-08-13/pdf/96-20397.pdf
3 p.
41951
41953
61 FR 41951
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; General Electric Company (GE) CF6-80C2 Series Turbofan Engines; Federal Register Vol. 61, Issue
RULE
96-20397
DEPARTMENT OF TRANSPORTATION
1996-08-28
Docket No. 96-ANE-16
Amendment 39-9707, AD 96-16-07
4910-13-U
96-20397
Final rule; request for comments.
This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CF6-80C2 series turbofan engines. This action supersedes priority letter AD 96-09-01 that currently requires borescope inspections of the rear right hand mount link to determine if the serial number matches those listed in applicable service bulletins as improperly manufactured, and replacement, if necessary, with a serviceable part. This action references a newly revised service bulletin and bases the compliance time on the effective date of this superseding AD for engines installed on McDonnell Douglas MD-11 series aircraft. This amendment is prompted by the availability of the newly revised service bulletin. The actions specified by this AD are intended to prevent rear right hand mount link failure, which could result in engine separation from the aircraft.
Effective August 28, 1996.
Richard Woldan, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (617) 238-7136, fax (617) 238-7199.
Federal Register
Vol. 61, no. 157
Office of the Federal Register, National Archives and Records Administration
1996-08-13
continuing
daily
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196 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-1996-08-13
P0b002ee180a26256
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr13au96
https://www.govinfo.gov/app/details/FR-1996-08-13
https://www.govinfo.gov/content/pkg/FR-1996-08-13/pdf/FR-1996-08-13.pdf
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2010-09-24
2023-05-06
FR-1996-08-13
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FR
FR-1996-08-13
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