AD 2021-04-08

final rule
Data completeness: 80%

Airworthiness Directives; Airbus Helicopters

AD Number
2021-04-08
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2020-0907
FR Citation
86 FR 11419

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters Model AS350B3 Airworthiness Directives; Airbus Helicopters

Unsafe Condition

Failure of the electrical operation of the throttle twist grip, which can prevent switching from ``IDLE'' mode to ``FLIGHT'' mode, resulting in unintended touchdown to the ground at a flight-idle power setting, damage to the helicopter, and injury to occupants.

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

Required Actions

Modifying the electrical system of the throttle twist grip, inspecting the routing of a microswitch electrical harness, and correcting the electrical harness routing if it is incorrect.

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

Compliance Time

Before the next practice autorotation, before the next simulated governor failure, or within 330 hours time-in service, whichever occurs first.

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

Affected Aircraft

Airbus Helicopters Model AS350B3 helicopters with a Turbomeca ARRIEL 2B engine installed.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.