AD 2004-25-20
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Saab | SAAB 2000 | Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes |
Unsafe Condition
Fatigue cracking of the drag and shear angles that attach the nacelle to the wing, which could result in reduced structural integrity of the nacelle attachment to the wing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for cracking of the drag and shear angles that attach the nacelle to the wing. Perform repetitive inspections as specified. Modify the drag and shear angles as required to end repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the specified intervals as outlined in the AD, with initial inspections due at 14,500 and 11,000 flight cycles, respectively.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Saab Model SAAB 2000 series airplanes, as specified in the AD, with the drag and shear angles in question.
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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