AD 88-06-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | HS 748 Series 2A | Airworthiness Directives; BRITISH AEROSPACE Model H.S. 748 Series Airplanes |
| aircraft | BAE Systems (Operations) Limited | HS 748 Series 2B | Airworthiness Directives; BRITISH AEROSPACE Model H.S. 748 Series Airplanes |
Unsafe Condition
Cracks in the inboard main pivot bracket assemblies of the main landing gear could lead to collapse of the main landing gear.
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Required Actions
Inspect inboard main pivot bracket assemblies in accordance with British Aerospace H.S. 748 Service Bulletin 57/59, Revision No. 1, dated April 1984. Repair corrosion, loose bolts, and/or cracks as specified in the service bulletin. For corrosion exceeding 0.060-inch depth, use an FAA-approved repair method.
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Compliance Time
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.
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Affected Aircraft
BAE Systems (Operations) Limited Model HS 748 Series 2A and HS 748 Series 2B airplanes with Modification 6175 accomplished (post Mod 6175).
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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