AD 66-16-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 Series Airplanes |
Unsafe Condition
Chafing of the fuselage frame forward flange by the aft end of the headliner P/N AB77 A1605.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Rework the headliner P/N AB77 A1605, inspect the flange of fuselage frame P/N AB29 A501, and rework as necessary in accordance with BAC One-Eleven Alert Service Bulletin 53-A-PM 2107 or later ARB-approved issue.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before the accumulation of 3,000 hours' time in service for airplanes with less than 2,900 hours' time in service on the effective date of this AD and within the next 100 hours' time in service after the effective date of this AD for airplanes with 2,900 or more hours' time in service on the effective date of this AD unless already accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 Series Airplanes.
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.