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FAA AD on Hartzell Propeller Inc., model HD-E6C- 3 propellers

Washington, USA - To prevent loss of aircraft control due to loss of blade pitch control, inability to fully feather the propeller, hub fracture, and blade release

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NE-43-AD; Amendment 39-12933; AD 2002-22-08] RIN 2120-AA64 Airworthiness Directives; Hartzell Propeller Inc., Model HD-E6C- 3( ) Propellers PDF Copy (If Available): Preamble Information Regulatory Information 2002-22-08 Hartzell Propeller...

AVIONEWS - World Aeronautical Press Agency - 35495

AVIONEWS - World Aeronautical Press Agency
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