AD 2010-23-06

final rule
Data completeness: 70%

Airworthiness Directives; McCauley Propeller Systems Five-Blade Propeller Assemblies

AD Number
2010-23-06
Status
final_rule
Effective Date
Product Category
propeller
Docket
Docket No. FAA-2005-22690
FR Citation
75 FR 67613

Unsafe Condition

A cracked propeller hub could cause failure of the propeller hub, blade separation, and loss of control of the airplane.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Remove the propeller hub from service if it exceeds 6,000 hours time-since-new (TSN) on the effective date, within 250 hours time-in-service after the effective date. Remove the hub if it has fewer than 6,000 hours TSN, not later than 6,000 hours TSN. Do not install any hub removed under this AD into any propeller assembly.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 250 hours time-in-service after the effective date for hubs exceeding 6,000 hours TSN on the effective date; not later than 6,000 hours TSN for hubs with fewer than 6,000 hours TSN.

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.

View Official Source ↗