AD 92-10-08

Airworthiness directive · Thrust Reverser · Boeing 757-200 Series, 757-200CB Series and 757-200PF Series

Effective
June 8, 1992
Models
757-200 Series, 757-200CB Series, 757-200PF Series
Data sheet
TCDSA2NM
Registered aircraft
245 matched by model
Product
Aircraft · Large airplane
Amendment
39-8242
Docket
92-NM-77-AD

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

92-10-08 BOEING: Amendment 39-8242. Docket No. 92-NM-77-AD.

Applicability: Boeing Model 757-200 series airplanes equipped with Rolls-Royce RB211-535 series engines; as listed in Boeing Alert Service Bulletin 757-78A0030, dated January 31, 1992; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent in-flight deployment of both thrust reverser sleeves on one engine, which could result in reduced controllability of the airplane, accomplish the following:

(a) Within 90 days after the effective date of this AD, replace the restrictor union with a standard union, on each engine strut, in the return port of the thrust reverser directional control valve; and perform a functional test of the thrust reverser system; in accordance with Boeing Alert Service Bulletin 757-78A0030, dated January 31, 1992.

(b) An alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. The request shall be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO.

(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) The replacement and functional test shall be done in accordance with Boeing Alert Service Bulletin 757-78A0030, dated January 31, 1992. 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 Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124-2207. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the FederalRegister, 1100 L Street NW., Room 8401, Washington, DC.

(e) This amendment becomes effective on June 8, 1992.

Affected TCDS · 1

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

Registered aircraft · 245

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
  • Boeing245 aircraft
By year built
19822002
Registered aircraft by year built: 231 aircraft
19823
19831
19852
19866
19871
19882
19897
199018
199122
199221
199317
199419
19957
199616
199715
199820
199918
200017
200115
20024

14 with no year recorded

By model

Aircraft

See all 245 aircraft