AD 67-27-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes |
Unsafe Condition
Fatigue failures of the flap carriage links P/N AB09 A943 and post modification PM 2245 flap carriage links P/N AB09 A3657.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace carriage links P/N AB09 A943 with new links of the same part number or with P/N AB09 A3657 within specified landing intervals. For P/N AB09 A3657 links, replace with same part number or P/N AB09 A943 within specified landing intervals.
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Compliance Time
Within the next 500 landings after January 15, 1967, or before the accumulation of the number of landings specified in Column 2 or 3 for respective flap numbers and series, whichever occurs later, and thereafter at intervals not exceeding specified landings.
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Affected Aircraft
BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series airplanes equipped with flap carriage links P/N AB09 A943 or AB09 A3657.
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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