AIRCRAFT STRUCTURAL ASSEMBLY AND RIGGING CHAPTER 1 PHASEBOOK QUESTIONS WITH CORRECT ANSWERS

Which should be accomplished before jacking an aircraft?


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A: Install critical stress panels or plates




An airplane's center of lift is usually located aft of its center of gravity


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C: So that the aircraft will have a nose heavy tendency




If a single-rotor helicopter is in forward horizontal flight, the angle of attack of the
advancing blade is

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C: Less than the retreating blade




If the right wing of a monoplane is improperly rigged to a greater angle of incidence
than designated in the manufacturer's specifications, it will cause the


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A: Airplane to be off balance both laterally and directionally




1-69 AMA038
REFER TO F-9 ON 1-21


ANSWER 1-69 ON PAGE 1-20


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1-69 AMA038
REFER TO F-9 ON 1-21

ANSWER 1-69 ON PAGE 1-20




What is the smallest size cable that may be used in aircraft primary control systems?


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, A: 1/8 inch




Proper wing twist in a sheet metal constructed wing can usually be checked by
utilizing a


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C: Bubble level and special fixtures described by the manufacturer




Which statement is true regarding a cantilever wing?


A: No external bracing is needed
B: It requires only one lift strut on each side
C: It has nonadjustable lift struts


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A: No external bracing is needed




When a fiber or nylon insert-type, self-locking nut can be threaded on a bolt or stud
through the insert with only the fingers, it should be


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B: Rejected