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Fri, Dec 29, 2006

AD: Eurocopter Deutschland

AD NUMBER: PL2006-26-51
MANUFACTURER: Eurocopter Deutschland
SUBJECT: Airworthiness Directive PL2006-26-51
SUMMARY:
This Emergency Airworthiness Directive (AD) is prompted by an in-flight incident in which a dynamic weight broke off the tail rotor control lever subsequently leading to considerable vibrations.

A visual inspection revealed that the threaded bolt of the control lever had broken off.

This condition, if not corrected, could result in separation of the tail rotor control lever dynamic weights (weights) in flight, severe vibration, and subsequent loss of control of the helicopter.

FMI: www.faa.gov/regulations_policies/airworthiness_directives/

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