AD 95-15-07
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
Cracked or significantly deteriorated Structural Significant Items (SSI) could lead to loss of structural integrity of the airplane as it approaches or exceeds the manufacturer's original fatigue design life goal.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the FAA-approved maintenance inspection program to include inspections, repairs, and replacements as per Tables 1, 2, and 3 of Alert Service Bulletin 51-A-PM5830, Issue 4 (excluding MPG 52-10-6R and 53-10-29R). Perform inspections of SSI's at intervals not exceeding specified landings, and repair or replace cracked parts before further flight.
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Compliance Time
Within 6 months after the effective date of this AD (August 30, 1995) for paragraph (b), and within one year after November 3, 1988, or prior to the accumulation of the number of landings listed in the service bulletin, whichever is later, for paragraphs (c) and (d).
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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