AD 82-01-02 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes |
Unsafe Condition
Cracking of passenger and service door inner operating handles and endfittings could result in possible failures.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect handle tube, reinforcing liners, and endfitting for cracks following specified procedures. Replace or repair components with cracks exceeding specified lengths; repeat inspections at intervals not to exceed 1800 or 300 hours time in service depending on findings. Incorporate Modification PM5703 to no longer require compliance.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 600 hours time in service after March 19, 1984, or prior to 10,000 hours time in service since modification, whichever is later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
British Aerospace Model BAC 1-11 200 and 400 Series airplanes not incorporating Modification PM 5703.
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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