AD 2014-23-02

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Agusta S.p.A. Helicopters (Type Certificate Currently Held by AgustaWestland S.p.A.) (Agusta)

AD Number
2014-23-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0472
FR Citation
79 FR 69039

Applicability

TypeManufacturerModelDetails
aircraft Agusta S.p.A. Airworthiness Directives; Agusta S.p.A. Helicopters (Type Certificate Currently Held by AgustaWestland S.p.A.) (Agusta)

Unsafe Condition

A crack in a Gleason crown, which could cause damage to or loss of the main rotor drive and subsequent loss of control of the helicopter.

Required Actions

Perform repetitive magnetic particle inspections of the Gleason crown for a crack. If there is a crack, replace the Gleason crown assembly before further flight.

Compliance Time

Within 200 hours TIS for main transmissions with 2,400 or more hours.

Affected Aircraft

Agusta Model A109E, A109K2, A119, and AW119 MKII helicopters with a main transmission, part number (P/N) 109-0400-03-103, 109-0400-05-103, or 109-0400-03-109, with a Gleason crown, P/N 109-0403-07-103, installed.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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