AD 47-43-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 120 | Airworthiness Directives; CESSNA Model 120 and 140 Airplanes |
| aircraft | Cessna Aircraft Company | 140 | Airworthiness Directives; CESSNA Model 120 and 140 Airplanes |
Unsafe Condition
Cracks at the fillet joining the cylindrical outer surface of the propeller blade retainer ferrule with the retaining face of the flange.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect the propeller blade retainer ferrule for cracks at the specified location. Disassemble and reassemble following the propeller manufacturer's instructions. Replace both blades with R003-225 blades if cracks are found.
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Compliance Time
prior to January 1, 1948, and thereafter upon completion of each 25 hours of operation
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Affected Aircraft
Cessna Model 120 and 140 aircraft equipped with Beech R003 propeller having R003-201 blades and Continental C-85 series engine.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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