AD 67-30-02
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 damage of the lower sidestay pin retaining bolt, P/N AC43-267.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the main landing gear lower sidestay retaining bolts (P/N AC43-267) for cracks using magnetic particle procedure or FAA-approved equivalent, following BAC 1-11 Alert Service Bulletin 32-A-PM 2898 or equivalent. Replace defective bolts with serviceable P/N AC43-267 or new P/N AC43-399 before further flight. Replace AC43-267 bolts with AC43-399 or inspected AC43-267 before 15,000 landings.
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Compliance Time
Within the next 200 landings after the effective date (December 4, 1967) or before 5,000 landings, whichever occurs later, and thereafter at intervals not exceeding 5,000 landings. For replacement before 15,000 landings.
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Affected Aircraft
BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes incorporating Modification PM 1558 part (c).
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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