AD 2024-10-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Helicopters Model SA-365N | Airworthiness Directives; Airbus Helicopters |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Helicopters |
Unsafe Condition
Interference between the cable tie head of the TR actuator harness and the pin fastener of the tail gearbox cowling, which could obstruct the tail rotor (TR) pedal control during flight, leading to loss of yaw control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the positioning of the TR actuator harness and cable ties installation. If interference is found, replace the cable ties as specified in the referenced EASA AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 100 hours time-in-service
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Affected Aircraft
All Airbus Helicopters Model SA-365N, SA-365N1, AS-365N2, and AS 365 N3 helicopters, certificated in any category.
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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