AD 99-16-02
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
Fatigue cracking of the airplane fuselage, which could result in reduced structural integrity of the airplane.
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Required Actions
Perform inspections for cracking of the fuselage in accordance with specified service bulletins. Reduce aircraft maximum cabin pressure differential to 7.5 psi by system modification if required. Repeat inspections at intervals shown in Table AA of the referenced service bulletin.
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Compliance Time
Within 15 months after September 28, 1989, or at or prior to specific landing accumulation thresholds, whichever is later.
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Affected Aircraft
British Aerospace Model BAC 1-11 200 and 400 series airplanes with Modifications PM2840, PM3187, or PM4886 (excluding those with PM5282).
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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