AD 91-08-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | BAe 146-200A | Airworthiness Directives; British Aerospace Model BAe 146-200A Series Airplanes |
Unsafe Condition
Reduced structural integrity of the fuselage pressure vessel due to rivet abrasion damage, loose or missing rivets, skin cracks, and reduced skin thickness from polishing operations.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform detailed visual and ultrasonic inspections of fuselage skins and rivets within 30 days of AD effective date. Repeat inspections at intervals not exceeding 1,500 flights or 2,000 landings as specified. Repair cracks, replace loose/missing rivets, apply protective treatment to curved-edge rivets, and report findings to British Aerospace.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 30 days after the effective date of this AD for initial inspections; repeat inspections at intervals not to exceed 1,500 flights or 2,000 landings as specified. Repairs must be done prior to further flight unless otherwise stated.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
British Aerospace Model BAe 146-200A series airplanes with serial numbers E2022 through E2025, E2028, E2030, E2031, E2034, E2036, and E2039 through E2048.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.