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AIRCRAFT STRUCTURAL ASSEMBLY AND RIGGING QUESTIONS WITH CORRECT ANSWERS

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AIRCRAFT STRUCTURAL ASSEMBLY AND RIGGING QUESTIONS WITH CORRECT ANSWERS

Institution
Aircraft Structural Assembly And Rigging
Course
Aircraft Structural Assembly and Rigging

Content preview

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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Rejected.




Which statement is true regarding a cantilever wing?


No external bracing is needed.
It requires only one lift strut on each side.
It has non adjustable lift struts.


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, No external bracing is needed.




The primary purpose of stall strips is to...


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Stall the inboard portion of the wings first.




What nondestructive checking method is normally used to ensure that the correct
amount of swaging has taken place when installing swaged-type terminals on aircraft
control cable?


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Use a terminal gauge to check the diameter of the swaged portion of the
terminal.




Main rotor blades that do not cone but that same amount during are said to be out
of...


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Track.

, During inspection of the flight control system of an airplane equipped with
differential-type aileron control, side to side movement of the control stick will
cause...


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Each aileron to have a greater up travel (from the streamlined position) than
down travel.




A decrease in pitch angle of the tail rotor blades on a helicopter...


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Causes the tail to pivot in the direction of torque rotation around the main
rotor axis.




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


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1/8 inch.




Which part(s) of a semi monocoque fuselage prevent(s) tension and compression
from bending the fuselage?


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Institution
Aircraft Structural Assembly and Rigging
Course
Aircraft Structural Assembly and Rigging

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Uploaded on
April 16, 2026
Number of pages
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Written in
2025/2026
Type
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Questions & answers

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