AD 90-26-01

Historical

Airworthiness directive · Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more

Effective
December 20, 1990
Superseded by
AD2014-21-01
Models
CF6-80C2A1, CF6-80C2A2, CF6-80C2A3, CF6-80C2A5, CF6-80C2B1, CF6-80C2B1F and 8 more
Data sheet
TCDSE13NE
Registered aircraft
592 matched by model
Product
Engine
Amendment
39-6810
Docket
89-ANE-03

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 August 7, 2025.

On this page

The airworthiness directive

90-26-01 GENERAL ELECTRIC COMPANY: Amendment 39-6810. Docket No. 89-ANE- 03.

Applicability: General Electric Company (GE) CF6-80C2 series turbofan engines installed on, but not limited to, Airbus A300 and A310 and Boeing 747 and 767 series aircraft.

Compliance: Required within 30 calendar days after the effective date of this AD, unless already accomplished.

To prevent engine fire and potentially significant aircraft damage, accomplish the following:

(a) Replace fuel manifold systems, Part Numbers (P/N) 1303M31G04 and 1303M32G04, with fuel manifold systems, P/N 1303M31G06 and 1303M32G06, or with P/N 1303M31G07 and P/N 1303M32G07 in accordance with the Accomplishment Instructions of GE CF6-80C2 Series Service Bulletin 73-053, Revision 3, dated April 3, 1990.

(b) 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.

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

The installation of the improved fuel manifold systems shall be accomplished in accordance with the following GE document:

Document Number Page Numbers Issue/Rev. Date SB 73-053 4-14, 18-25, 27, 29-42 Revision 2 08/23/89

1-3, 15-17, 26,28, 43-45 Revision 3 04/03/90

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, FAA, New England Region, 12 New England Executive Park, Room 311, Burlington, Massachusetts 01803, or at the Office of the Federal Register, 1100 L Street, NW, Room 8301, Washington, DC 20591.

Airworthiness Directive 90-26-01 supersedes AD 89-03-52, Amendment 39-6199.

This amendment (39-6810, AD 90-26-01) becomes effective on December 20, 1990.

Affected TCDS · 1

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

Registered aircraft · 592

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
  • Boeing489 aircraft
  • Mcdonnell Douglas65 aircraft
  • Airbus Industrie38 aircraft
By year built
19822026
Registered aircraft by year built: 578 aircraft
19821
19832
19842
19852
19871
19883
19895
199010
199120
199234
199325
199423
199526
199628
199718
199826
199925
200032
200124
200222
20032
20042
20053
20064
20075
20086
20093
20109
20116
201213
201311
20145
201516
201613
20179
201817
201919
202020
202118
202216
202317
202410
202515
202610

14 with no year recorded

By model

Aircraft

See all 592 aircraft