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FAA AD on Turbomeca Arriel 1 series turboshaft engines

Washington, Usa - To prevent engine failure due to rubbing of the 2nd stage turbine disk on the 2nd stage nozzle guide vanes, which could result in complete engine failure and damage to the helicopter

Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 94-ANE-08-AD; Amendment 39-13256; AD 2003-16-03] RIN 2120-AA64 Airworthiness Directives; Turbomeca Arriel 1 Series Turboshaft Engines PDF Copy (If Available): Preamble Information AGENCY: Federal Aviation...

fra/pec - 51976
Rome, Italy, 08/26/2003 14:37
AVIONEWS - World Aeronautical Press Agency

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