AD 92-17-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; British Aerospace Model BAC 1-11-200 and -400 Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; British Aerospace Model BAC 1-11-200 and -400 Airplanes |
Unsafe Condition
Reduced structural integrity of the fuselage pressure vessel due to cracks in the top and bottom corners of the passenger and service door apertures.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform close visual, dye penetrant, or eddy current inspections to detect cracks in door apertures and repair any found cracks and associated damage per British Aerospace Alert Service Bulletin 53-A-PM5989. Compliance intervals vary based on inspection method and modification PM51 installation status.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the specified landing accumulation or within a certain number of landings after the AD's effective date (September 29, 1992), whichever occurs later.
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Affected Aircraft
British Aerospace Model BAC 1-11-200 and -400 airplanes, certificated in any category.
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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