AD 95-16-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | British Aerospace Regional Aircraft | H.P. 137 Jetstream Mk. 1 | Airworthiness Directives; Jetstream Aircraft Limited HP137 Mk1 and Jetstream Series 200 Airplanes |
| aircraft | British Aerospace Regional Aircraft | Jetstream Series 200 | Airworthiness Directives; Jetstream Aircraft Limited HP137 Mk1 and Jetstream Series 200 Airplanes |
Unsafe Condition
Cracks or loose or damaged rivets in the wing lower skin panels could result in structural damage to the point of failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the wing lower skin between WS 60 and WS 115 for loose or damaged rivets or cracks, replace loose or damaged rivets, repair cracked panels, reinforce the wing lower skin at landing gear bay cutouts (WS 115) per SB 57-JM5221, and reinforce undercarriage bay cutouts between WS 60 and WS 90 per Part 2 of Modification 5146 Ref 7/5146.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 100 hours time-in-service (TIS) after the effective date (September 26, 1995) or upon accumulation of 6,500 hours TIS, whichever occurs later, and thereafter at intervals not to exceed 100 hours TIS until modifications are incorporated. Modifications must be done by 10,000 hours TIS or within the next 100 hours TIS after the effective date, whichever is later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Jetstream Aircraft Limited HP137 Mk1 and Jetstream Series 200 airplanes (all serial numbers), certificated in any category.
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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