AD 2013-21-01

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France (Eurocopter) Helicopters

AD Number
2013-21-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2013-0878
FR Citation
78 FR 63853

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter France (Eurocopter) Airworthiness Directives; Eurocopter France (Eurocopter) Helicopters

Unsafe Condition

A crack in the yoke of the tail rotor pitch horn assembly, which may lead to failure of the pitch horn, loss of the anti-torque function, 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

Visually inspect each pitch horn for a crack in the specified areas. If a crack is found, replace the pitch horn with an airworthy one before further flight. Before installing any pitch horn, perform a dye-penetrant inspection for cracks.

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

Compliance Time

Within 10 hours time-in-service for helicopters with parts exceeding 155 hours time-in-service.

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

Affected Aircraft

Eurocopter Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters with FAA type certificates.

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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