AD 2013-03-02

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Helicopters

AD Number
2013-03-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2013-0075
FR Citation
78 FR 9777

Applicability

TypeManufacturerModelDetails
aircraft Eurocopter France Airworthiness Directives; Eurocopter France Helicopters

Unsafe Condition

Cracks in the tail rotor hub (TRH) could lead to tail rotor jamming, which could result in reduced or 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 the TRH for cracks within 55 hours time in service (TIS). If a crack is found, remove the TRH from service. Repeat the inspection at intervals not exceeding 55 hours TIS.

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

Compliance Time

Within 55 hours time in service (TIS)

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

Affected Aircraft

Eurocopter France Model EC 155B, EC155B1, SA-365N1, AS-365N2, and AS 365 N3 helicopters with 10-bladed or 11-bladed TRHs, part numbers 365A33351100, 365A33351101, 365A33351102, and other affected part numbers.

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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