AD 95-24-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | British Aerospace Regional Aircraft | Jetstream 3201 | Airworthiness Directives; Jetstream Aircraft Limited Model 3201 Airplanes |
Unsafe Condition
Cracking at the main landing gear (MLG) bay forward lower edge wing skin structure during fatigue testing could cause failure of the wing structure and loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the MLG bay forward lower edge wing skin structure adjacent to the main spar for cracks in accordance with Jetstream SB 57-A-JA920540. Replace existing doublers with joggled doublers of improved design if cracks are found, or within 9,000 hours time-in-service. Re-inspect at intervals not exceeding 600 hours TIS if no cracks are found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Required as indicated in the body of this AD, unless already accomplished. The initial inspection must be done upon accumulating 4,000 hours time-in-service (TIS) or within the next 200 hours TIS after the effective date of this AD, whichever occurs later. The doubler replacement under paragraph (b) must be done upon accumulating 9,000 hours TIS or within the next 200 hours TIS after the effective date of this AD, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Jetstream Aircraft Limited Model 3201 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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