AD 94-08-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | ATP | Airworthiness Directives; Jetstream Model ATP Airplanes |
Unsafe Condition
Loose fasteners on the wing top surface stringer joint bolts at Rib 0 could lead to reduced structural integrity of the wing top surface stringer joints and subsequently the wing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a detailed visual inspection and appropriate torque loading check of the fasteners in the stringer joint brackets (part number JD534J0015) at the wing top surface stringer joints for stringers 1 through 19 at Rib 0, in accordance with specified service bulletins. Correct discrepancies prior to further flight as required.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 10,000 total hours time-in-service, or within the next 600 hours time-in-service 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 Model ATP airplanes; serial numbers 2001 through 2053 inclusive, and 2055; 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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.