AD 2005-17-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Saab | SAAB 2000 | Airworthiness Directives; Saab Model SAAB 2000 Airplanes |
Unsafe Condition
Cracking of certain fastener holes in the lower spar cap of the rear spar and in the lower skin at the front spar, which could result in fuel leakage and reduced structural integrity of the wing structure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for cracking of fastener holes in the lower spar cap of the rear spar and in the lower skin at the front spar, using Saab Service Bulletin 2000-57-038, Revision 01. Modify the fastener holes of the front and rear spars and the rear spar web, also using the same service bulletin. Repair any detected cracking or damage before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 20,000 total flight cycles
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Affected Aircraft
Saab Model SAAB 2000 airplanes, serial numbers 004 through 063 inclusive, 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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