AD 2008-08-01
Unsafe Condition
Cracks in the propeller blades could cause failure and separation, leading to loss of control. Blunt leading edges due to erosion can degrade single engine climb performance and increase the risk of terrain collision.
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Required Actions
Initial inspections include fluorescent penetrant inspections (FPI) and eddy current inspections (ECI) for cracks. Repetitive inspections are added, and a life limit is mandated for the blades. Blades with cracks or blunt leading edges must be removed from service.
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Compliance Time
Extended compliance times and intervals are specified, but exact details are not provided in the summary.
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Affected Aircraft
McCauley Propeller Systems propeller models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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