AD 79-02-04

final rule
Data completeness: 70%

Airworthiness Directives; Costruzioni Aeronautiche Model A109 and A109A Helicopters

AD Number
79-02-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Agusta S.p.A. A109 Airworthiness Directives; Costruzioni Aeronautiche Model A109 and A109A Helicopters
aircraft Agusta S.p.A. A109A Airworthiness Directives; Costruzioni Aeronautiche Model A109 and A109A Helicopters

Unsafe Condition

Cracks in the tail rotor drive shaft hanger bearing support bracket, P/N 109-0370-02-1, could lead to tail rotor failure.

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

Required Actions

Within 10 hours time in service after the effective date, inspect the bracket daily for cracks per Agusta Bollettino Tecnico No. 109-2. Replace cracked brackets with same P/N or new P/N 109-0370-12-1 before further flight. By 100 hours time in service, replace all P/N 109-0370-02-1 brackets with P/N 109-0370-12-1 to discontinue daily inspections.

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

Compliance Time

within the next 10 hours time in service after the effective date of this AD, and thereafter following the last flight of each day in which the helicopter is operated

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

Affected Aircraft

Costruzioni Aeronautiche Giovanni Agusta Model A109 and A109A helicopters, serial numbers 7109 and below, with tail rotor drive shaft hanger bearing bracket P/N 109-0370-02-1

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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