AD 88-06-01

Airworthiness directive · Main Landing Gear · BAE Systems HS 748 Series 2A and HS 748 Series 2B

Effective
April 18, 1988
Models
HS 748 Series 2A, HS 748 Series 2B
Data sheet
TCDSA24EU
Registered aircraft
2 matched by model
Product
Aircraft · Large airplane
Amendment
39-5870

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

88-06-01 BRITISH AEROSPACE: Amendment 39-5870. Applies to all Model H.S. 748 series airplanes, on which Modification 6175 has been accomplished (post Mod 6175), certificated in any category. Compliance required as indicated, unless previously accomplished.

To detect cracks and prevent collapse of the main landing gear, accomplish the following:

A. Prior to accumulating 25,000 landings or within the next 750 flight hours after the effective date of this AD, whichever occurs later, and thereafter at intervals not to exceed 1,500 landings, perform an inspection of inboard main pivot bracket assemblies in accordance with paragraph 2A of the British Aerospace H.S. 748 Service Bulletin 57/59, Revision No. 1, dated April 1984. Any assembly found to exhibit corrosion, loose bolts, and/or cracks must be repaired in accordance with paragraph 2D of the above mentioned service bulletin. If corrosion to a depth greater than 0.060-inch is found, repair in accordance with a method approved by the FAA.

B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety and which has the concurrence of an FAA Principal Maintenance Inspector, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to British Aerospace, Librarian for Service Bulletins, P.O. Box 17414 Dulles International Airport, Washington, D.C. 20041. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective April 18, 1988.

Affected TCDS · 1

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

Registered aircraft · 2

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 Aerospace2 aircraft

By model

Aircraft