AD 95-19-12
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
Cracking in panel number 1 at rib 6 and panel number 2 at rib 10 of the lower skin of the wing, and in the rebate radius of panel number 2 at the joint between panels 1 and 2 of the lower skin of the wing, and in the top and bottom flanges of fixed ribs 6, 10, and 14 of the leading edge of the wing due to fatigue-related stress.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform close visual and dye penetrant inspections for cracks in wing panels and ribs as specified. Repeat inspections at intervals not to exceed 8,000 landings if no cracks found. Repair or replace cracked parts prior to further flight per service bulletin. Alternative methods may be approved by the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 12,000 total landings or within 1,500 landings after the effective date of this AD, whichever occurs later for panels 1 and 2 at ribs 6 and 10. For rebate radius and fixed ribs 6, 10, and 14, prior to 30,000 total landings or within 1,500 landings after the AD's effective date, whichever is later.
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, all serial numbers.
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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