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FAA Emergency AD on MD Helicopters (2007-09-51)

Washington, Usa - To prevent the loss of a tail rotor blade and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Directorate Identifier 2007-SW-18-AD; AD 2007-09-51 MD Helicopters PDF Copy (If Available): Preamble Information AGENCY: Federal Aviation Administration, DOT John Cecil, Aviation Safety Engineer, FAA, Los Angeles Aircraft...

fra/pec - 1073532

AVIONEWS - World Aeronautical Press Agency
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