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Helicopter rotor / Fatigue / Helicopter / Adhesive / Blade inspection method / Materials science / Rotorcraft / Aircraft


AVIATION INVESTIGATION REPORT A11O0205 IN-FLIGHT SEPARATION OF MAIN ROTOR BLADE AND COLLISION WITH TERRAIN SUNRISE HELICOPTERS INC.
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Document Date: 2013-12-10 09:53:25

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File Size: 1,01 MB

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