AD 83-15-08 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
Structural failure of the fuselage due to cracks and loose rivets in fuselage skin lap joints.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform initial and repetitive visual and eddy current inspections of fuselage skin lap joints for cracks and loose rivets at intervals specified in Table I of this AD, following British Aerospace Alert Service Bulletin 53-A-PM5726, Issue 3. Repair identified cracks or loose rivets prior to further flight as per specified repair methods or approved alternatives.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Required as indicated unless previously accomplished.
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, 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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