AD 90-05-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 208 | Airworthiness Directives; CESSNA Model 208, 208A, and 208B Airplanes |
| aircraft | Cessna Aircraft Company | 208A | Airworthiness Directives; CESSNA Model 208, 208A, and 208B Airplanes |
| aircraft | Cessna Aircraft Company | 208B | Airworthiness Directives; CESSNA Model 208, 208A, and 208B Airplanes |
Unsafe Condition
Failure of the Part Number 2622083-18 bellcrank assembly and resulting unexpected retraction of the flaps.
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Required Actions
Visually inspect the P/N 2622083-18 bellcrank assembly for cracks, deformation, and incomplete welds in accordance with Cessna Service Bulletin CAB89-34. Replace the bellcrank with an airworthy part if cracks, deformation, or incomplete welds are found before further flight or within the next 50 hours time-in-service. Inspect replacement parts before installation.
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Compliance Time
within the next 50 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished
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Affected Aircraft
Cessna Model 208 (Serial Numbers 20800001 thru 20800173), 208A (same serial range as Model 208), and 208B (Serial Numbers 208B0001 through 208B0202) airplanes certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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