AD 89-16-08

Airworthiness directive · Manifold · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more

Effective
August 31, 1989
Models
CF6-80A, CF6-80A1, CF6-80A2, CF6-80A3
Data sheet
TCDSE13NE
Registered aircraft
251 matched by model
Product
Engine
Amendment
39-6259

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

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The airworthiness directive

89-16-08 GENERAL ELECTRIC COMPANY: Amendment 39-6259.

Applicability: General Electric Company (GE) CF6-80A/A1/A2/A3 turbofan engines.

Compliance: Required as indicated, unless already accomplished.

To provide increased fire protection in the event of a fire escaping from the LPT recoup manifold which could lead to fuel leakage and possible engine fire, accomplish the following prior to August 31, 1989:

(a) Install on CF6-80A/A2 engines, two zirconia-coated fire shields, Part Numbers (P/N) 1306M85G01 and 1306M86G01, in accordance with GE CF6-80A series Alert Service Bulletin (ASB) A72-512, Revision 1, dated May 24, 1988.

(b) Install on CF6-80A1/A3 engines, fire shield, P/N 1306M84P02, in accordance with GE CF6-80A series ASB A72-510, Revision 2, dated November 14, 1988.

(c) Aircraft may be ferried in accordance with the provisions of FAR 21.197 and 21.199 to a base where the AD can be accomplished.

(d) Upon submission of substantiating data by anowner or operator through an FAA Airworthiness Inspector, an alternative method of compliance with the requirements of this AD or adjustments to the compliance time specified in this AD, may be approved by the Manager, Engine Certification Office, ANE-140, Engine and Propeller Directorate, Aircraft Certification Service, 12 New England Executive Park, Burlington, Massachusetts 01803.

The installation of the required fire shields shall be done in accordance with the procedures given in GE CF6-80A series ASB A72-512, Revision 1, dated May 24, 1988 (CF6-80A/80A2 engines) or ASB A72-510, Revision 2, dated November 14, 1988, (CF6-80A1/A3 engines). This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from General Electric Aircraft Engines, CF6 Distribution Clerk, Room 132, 111 Merchant Street, Cincinnati, Ohio 45246. Copies may be inspected at the Regional Rules Docket, Office of the Assistant Chief Counsel, Federal Aviation Administration, New England Region, 12 New England Executive Park, Room 311, Burlington, Massachusetts 01803, or at the office of the Federal Register, 1100 L Street, Room 8301, Washington, DC 20591.

This amendment (39-6259, AD 89-16-08) becomes effective on August 31, 1989.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 251

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Boeing171 aircraft
  • Mcdonnell Douglas45 aircraft
  • Airbus Industrie35 aircraft
By year built
19822020
Registered aircraft by year built: 243 aircraft
19821
19836
19849
19853
19881
19891
19906
199111
199220
199314
19949
199519
199620
199711
199821
199922
200028
200118
200217
20031
20051
20072
20202

8 with no year recorded

By model

Aircraft

See all 251 aircraft