AD 2007-15-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; British Aerospace Regional Aircraft Jetstream HP.137 Jetstream Mk.1, Jetstream Series 200, Jetstream Series 3101, and Jetstream Model 3201 Airplanes |
Unsafe Condition
Failed bolts fitted to frame 199 wing spigot post assembly could compromise the structural integrity of the wing to fuselage attachment, leading to loss of the aircraft.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect and torque check the bolts at frame 199 initially within 90 days or 100 hours TIS after August 22, 2007, and repetitively every 4,000 hours TIS. Correct any discrepancies before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Initially within 90 days or 100 hours TIS after August 22, 2007, whichever occurs first.
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Affected Aircraft
Jetstream HP.137 Jetstream Mk.1, Jetstream Series 200, Jetstream Series 3101, and Jetstream Model 3201 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 6, 2026
Rights: U.S. Government Public Domain
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