AD 93-01-11

Historical

Airworthiness directive · Wing Structural Integrity · BAE Systems BAe 146-100A, BAe 146-200A and BAe 146-300A

Effective
March 2, 1993
Superseded by
AD2010-09-11
Models
BAe 146-100A, BAe 146-200A, BAe 146-300A
Data sheet
TCDSA49EU
Registered aircraft
8 matched by model
Product
Aircraft · Large airplane
Amendment
39-8465
Docket
92-NM-56-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 August 7, 2025.

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The airworthiness directive

93-01-11 BRITISH AEROSPACE: Amendment 39-8465. Docket 92-NM-56-AD. Applicability: All Model BAe 146-100A, -200A, and -300A series airplanes, certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent reduced structural integrity of the wings, accomplish the following:

(a) Prior to the accumulation of 24,000 landings, or within 60 days after the effective date of this AD, whichever occurs later: Perform an X-ray inspection to detect fatigue cracks in the left and right wing upper skins, joint straps, and stringers in the vicinity of rib "O," in accordance with British Aerospace Inspection Service Bulletin 57-41, dated July 26, 1991.

(1) If cracks are found, prior to further flight, repair in accordance with a method approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. Thereafter, repeat the inspection required by paragraph (a) of this AD at intervals not to exceed9,000 landings, in accordance with the service bulletin.

(2) If no cracks are found, repeat the inspection required by paragraph (a) of this AD at intervals not to exceed 9,000 landings, in accordance with the service bulletin.

(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113.

(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 inspections shall be done in accordance with British Aerospace Inspection Service Bulletin 57-41, dated July 26, 1991. 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 British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, DC 20041-0414. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(e) This amendment becomes effective on March 2, 1993.

Affected TCDS · 1

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

Registered aircraft · 8

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
  • British Aerospace8 aircraft
By year built
19851989
Registered aircraft by year built: 6 aircraft
19851
19861
19871
19881
19892

2 with no year recorded

By model

Aircraft