AD 95-19-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | BAe 146-100A | Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A Airplanes |
| aircraft | BAE Systems (Operations) Limited | BAe 146-200A | Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A Airplanes |
| aircraft | BAE Systems (Operations) Limited | BAe 146-300A | Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A Airplanes |
Unsafe Condition
Fatigue cracking in the web and inboard flange of fuselage frame 29.
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Required Actions
Perform detailed visual inspections (or surface eddy current inspections if polymer coating prevents visual access) for cracking of frame 29 between stringers 12 and 18 on left and right fuselage sides, following Avro SB 53-130. Repeat inspections at intervals not exceeding 6,000 landings (4,000 for specified BAe 146-300A serials). Repair any cracking prior to further flight using an approved method.
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Compliance Time
Within 6 months after October 20, 1995, or prior to accumulating 30,000 (BAe 146-100A), 24,000 (BAe 146-200A and most BAe 146-300A), or 13,000 landings (specific BAe 146-300A serials), whichever occurs later. Repeat inspections at intervals not exceeding specified landing limits.
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Affected Aircraft
British Aerospace Model BAe 146-100A, -200A, and -300A airplanes, including serial numbers E3207, E3212, E3214, E3216, E3218, E3219, and E3222 for the -300A variant.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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