AD 2022-01-05

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Helicopters

AD Number
2022-01-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2021-1165
FR Citation
86 FR 74353

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters Model EC130T2 Airworthiness Directives; Airbus Helicopters
aircraft Aviat Various Airworthiness Directives; Airbus Helicopters

Unsafe Condition

Degradation of the rear transmission shaft bearing support on a Model EC 130 T2 helicopter, which could lead to failure of the tail rotor drive shaft and subsequent loss of yaw control of the helicopter.

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

Required Actions

Accomplish repetitive visual inspections of the rivets on the rear transmission upper and lower bearing support, the local structure, and the rivet heads on the left-hand and right-hand sides of the rear transmission shaft bearing support. Depending on the results, contact Airbus Helicopters to obtain approved repair instructions and accomplish those instructions, or replace each affected rivet. Report inspection findings to Airbus Helicopters.

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

Compliance Time

Before each first flight of the day

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

Affected Aircraft

Airbus Helicopters Model EC130T2 helicopters, all serial numbers, on which Airbus Helicopters Modification 074581 had been embodied in production.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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