AD Amdt-39-13524
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Eurocopter | France Model EC 155B | Airworthiness Directives; Eurocopter France Model EC 155B Helicopters |
Unsafe Condition
Tail rotor induced vibrations during flight tests can lead to vibration in the tail rotor and pilot's anti-torque pedals, potentially causing blade pitch control failure and loss of control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install a tail rotor blade-to-torsion bar attachment tuning weight assembly on each blade of the Quiet Fenestron tail rotor. Replace each blade attachment bushing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Eurocopter France EC 155B helicopters with the specified configuration.
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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