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Airworthiness Directive

AD 2004-23-16 69 FR 67807 Active

Federal Aviation Administration · 14 CFR part 39

Requires a one- time eddy-current inspection of the propeller hub for cracks, and if necessary, replacing the propeller assembly.

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FR document
04-25543
Amendment
39-13871
Published
2004-11-22
Effective
2004-12-07
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/2004-23-16 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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AD

2004-23-16

FR doc 04-25543 · 69 FR 67807

AD 2004-23-16Published 2004-11-22Effective 2004-12-07

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires a one- time eddy-current inspection of the propeller hub for cracks, and if necessary, replacing the propeller assembly.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for McCauley Propeller Systems propeller assemblies, part numbers (P/Ns) B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0, installed on BAE Systems (Operations) Limited Jetstream Model 4100 series airplanes. This AD requires a one- time eddy-current inspection of the propeller hub for cracks, and if necessary, replacing the propeller assembly. This AD results from three reports of cracked hubs. We are issuing this AD to detect cracked hubs, which could cause failure of the propeller hub and loss of control of the airplane.

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All British Aerospace Jetstream 41 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index