Airbus Helicopters Deutschland GmbH Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC125T2+, and EC135T3 Helicopters, to Require Modifying the Tail Rotor Control Installation to Prevent Interference Between the Head of the Close-Tolerance Bolt and the Stringer.
🏛 Federal Aviation Administration (FAA)FAA-2019-0293
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