AD Amdt-39-11474

final rule
Data completeness: 70%

Airworthiness Directives; Agusta S.p.A. Model AB412 Helicopters

AD Number
Amdt-39-11474
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-SW-63-AD
FR Citation
64 FR 71012

Applicability

TypeManufacturerModelDetails
aircraft Agusta S.p.A. Model AB412 Airworthiness Directives; Agusta S.p.A. Model AB412 Helicopters

Unsafe Condition

Fatigue failure of the main rotor yoke (yoke) due to insufficient thickness and margin of safety, which could lead to loss of a main rotor blade and subsequent loss of control of the helicopter.

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

Required Actions

Remove and replace each main rotor yoke, part number (P/N) 412-010-101-123 or -127, with an airworthy yoke, P/N 412-010-101-129, before further flight.

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

Compliance Time

Before further flight

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

Affected Aircraft

Agusta S.p.A. Model AB412 helicopters with main rotor yoke, part number (P/N) 412-010-101-123 or -127, installed, certificated in any category.

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

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