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FAA AD on Turbomeca S.A. Makila models 1A, 1A1, and 1A2 turboshaft engines with exhaust pipes incorporating modification TU 200A installed

Washington, Usa - To prevent the ejector from becoming loose from the exhaust pipe, resulting in damage to the main rotor and tail rotor and loss of helicopter control

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NE-42-AD; Amendment 39-12882; AD 2002-19-02] RIN 2120-AA64 Airworthiness Directives; Turbomeca S.A. Makila Models 1A, 1A1, and 1A2 Turboshaft Engines Regulatory Information 2002-19-02 Turbomeca S.A.: Amendment 39-12882. Docket No. 2001-NE- 42-AD. Applicability...

AVIONEWS - World Aeronautical Press Agency - 33774

AVIONEWS - World Aeronautical Press Agency