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FAA AD on General Electric Company CT7-5, -7, and -9 series turboprop engines
Washington, Usa - To prevent stage 2 aft cooling plate separation, resulting in uncontained engine failure and damage to the airplane
Airworthiness Directive Federal Register Information [Federal Register: September 19, 2005 (Volume 70, Number 180)] [Page 54835-54837] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20944; Directorate Identifier 2003-NE-64-AD; Amendment 39-14247; AD 2005-18-01] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 127191
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency