Aviation Structural Mechanic - Ch 02: Aircraft Con
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On a semimonocoque fuselage, what component absorbs the primary bending loads? >>> Longerons. What aircraft structure is designed to transmit engine loads, stresses, and vibrations to the aircraft structure? >>> Nacelle. What is the main structural member of a wing assembly? >>> Spar. What is the primary purpose of a stabilizer? >>> To keep the aircraft in straight and level flight. What type of flight controls provides control over pitch, roll, an...
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Aviation Structural Mechanic - Ch 02: Aircraft Con•Aviation Structural Mechanic - Ch 02: Aircraft Con