AD 89-03-11
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
Cracks in the rear pintle support beam could lead to a hazardous landing condition.
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Required Actions
Perform eddy current or dye penetrant inspections for cracks in the rear pintle support beam according to British Aerospace Alert Service Bulletin 57-A-PM5896. Repeat inspections at intervals not exceeding 3,200 landings. If cracks are found, repair or replace the part prior to further flight depending on crack length and modification status. Inspect toggle links' special bolt assembly for damage and replace if necessary.
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Compliance Time
Compliance required as indicated: inspections must be done at or prior to specified landings or within specified periods after certain dates, with repeat intervals not exceeding 3,200 landings. Specific compliance times vary by model and modification status.
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Affected Aircraft
British Aerospace Model BAC 1-11 200 and 400 series airplanes, all serial numbers, with specific modifications (PM3070, PM5928) or part numbers (EDO3-1001/2, ENO3-1259/60).
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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