AD 2004-23-16
Unsafe Condition
Cracked hubs in McCauley Propeller Systems propeller assemblies, which could cause failure of the propeller hub and loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a one-time eddy-current inspection of the propeller hub for cracks using McCauley Alert Service Bulletin ASB247A, Revision A. Replace the propeller assembly if cracks are found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 200 hours TSLI or 30 days after the effective date for propeller assemblies with more than 8,000 hours TIS; within 400 hours TSLI or 60 days after the effective date for propeller assemblies with 8,000 or fewer hours TIS.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McCauley Propeller Systems propeller assemblies, part numbers B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0, installed on BAE Systems (Operations) Limited Jetstream Model 4100 series airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.