AD 98-13-31
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Saab AB, Saab Aerosystems | SAAB 2000 | Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes |
Unsafe Condition
Failure of the fitting lugs due to vibration caused by loose bushings in the aileron actuation fittings, which could result in reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the bushing installations of the left-hand and right-hand aileron actuation fittings within 100 flight hours after the effective date. Repeat inspections at intervals not exceeding 300 flight hours (or 600 flight hours if the optional temporary preventive action is taken) until the installation of staked bushings is completed. Install new staked bushings within 3,000 flight hours after the effective date to terminate inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 100 flight hours after the effective date of this AD for the initial inspection, and within 3,000 flight hours after the effective date for the installation of staked bushings.
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Affected Aircraft
Saab Model SAAB 2000 series airplanes having serial numbers -002 through -023 inclusive.
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
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