AD 2000-15-10
Unsafe Condition
Crack on the camber side of the blade surface, which could cause failure of the propeller blade and result in loss of control of the airplane.
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Required Actions
Perform one-time and repetitive eddy current inspections or dye penetrant inspections of the camber side of the propeller blade, in accordance with McCauley Propeller Systems Alert Service Bulletin (ASB) 234. Inspections must be conducted by qualified personnel with a 'Level II' rating.
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Compliance Time
Within 200 flight hours after the effective date of this AD or within 30 days after the effective date, whichever occurs first, and thereafter every 600 flight hours after the last inspection.
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Affected Aircraft
McCauley Propeller Systems 4HFR34C653/L106FA-0 model propellers installed on Jetstream Series 3200 airplanes, and those installed on Ayres S2R-G5 and S2R-G10 airplanes if the propeller was previously installed on Jetstream Series 3200 airplanes or if the installation history is unknown.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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