AD 2015-11-07

final rule
Data completeness: 70%

Airworthiness Directives; Agusta S.p.A. Helicopters

AD Number
2015-11-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2015-1936
FR Citation
80 FR 32451

Applicability

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

Unsafe Condition

A crack in the tail rotor (T/R) drive shaft flanged adapter, which could result in failure of the T/R drive shaft and reduced control of the helicopter.

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

Required Actions

Inspect the tail rotor (T/R) drive shaft flanged adapter (part numbers 412-040-622-101 and 412-040-623-101) for cracks. Remove the adapter from service if a crack is found. Visually inspect the adapter before installation.

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

Compliance Time

Before further flight if a crack is found.

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 serial numbers 25801 through 25900, and Model AB412 EP helicopters with serial numbers 25901 and larger.

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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