AD 96-11-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Saab AB, Saab Aerosystems | SAAB 2000 | Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes |
Unsafe Condition
Fatigue cracking of the lower rib of the rudder could result in failure of the primary structure of the rudder.
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Required Actions
Perform an initial visual inspection within 20 days after the effective date. Repeat inspections at intervals not exceeding 400 hours time-in-service if no cracking is found. Repair or modify per specified service bulletins if cracking is detected beyond limits.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 20 days after the effective date of this AD. Repeat inspections at intervals not to exceed 400 hours time-in-service.
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Affected Aircraft
Model SAAB 2000 series airplanes with serial numbers 004 through 039, inclusive.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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