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Exam (elaborations)

Assembly and Rigging FAA (AF1) Chapter 1 Exam With 100% Verified Solutions

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Assembly and Rigging FAA (AF1) Chapter 1 Exam With 100% Verified Solutions...

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Assembly And Rigging FAA Chapter 1
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Assembly and Rigging FAA Chapter 1









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Institution
Assembly and Rigging FAA Chapter 1
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Assembly and Rigging FAA Chapter 1

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Uploaded on
December 15, 2024
Number of pages
6
Written in
2024/2025
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Assembly and Rigging FAA (AF1) Chapter 1 Exam
With 100% Verified Solutions


Longitudinal (fore and aft) structural members of a semi monocoque fuselage are called
- ANSWER Longerons and stringers



Which statemwnt is true regarding a cantilever wing? - ANSWER No external bracing is
needed



The monocoque fuselage relies largely on the strength of - ANSWER Skin or covering



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



The acute angle formed by the chord line of a wing and the relative wind is known as the
- ANSWER Angle of attack



As the angle of attack of an airfoil increases, the center of pressure will - ANSWER Move
toward the leading edge



The chord of a wing is measured from - ANSWER Leading edge to trailing edge



As the lifr of an airfoil increases, the drag will - ANSWER Also increase



What physical factors are involved in the aspect ratio of airplane wings? - ANSWER
Span and chord



Where is the buttock line or buttline of an aircraft? - ANSWER A width measurement left

, or right of, and parallel to, the vertical centerline



Where is the fuselage station No. 137 located? - ANSWER 137 inches aft of the zero or
fixed reference line



Wing dihedral, a rigging consideration on most airplanes of conventional design,
contributes most to stability of the airplane about is - ANSWER Longitudinal axis



Other than the manufacturer's maintenance manual what other document could he used
to determine the primary flight control surface deflection for an imported aircraft that is
reassembled after shipment? ANSWER Aircraft type certificate data sheet



If a pilot reports that an airplane flies lefr wing heavy, this condition may be corrected by
- ANSWER Increasing the dihedral angle of the left wing, or decreasing the angle of
incidence of the right wing, or both



If the vertical fin of a single engine, propeller driven airplane is rigged properly, it will
generally be parallel to - ANSWER The vertical axis but not the longitudinal axis



An airplane which has good longitudinal stability should have a minimum tendency to -
ANSWER Pitch



The anfle of incidence is that acute angle formed by - ANSWER A line parallel to the wing
chord and a line parallel to the longitudinal axis of the aircraft



An airplane's center of lift is usually located aft of its center of gravity - ANSWER So that
the airplane will have a nose heavy tendency



An airplane is controlled directionally about its vertical axis by the - ANSWER Rudder



The elevators of a conventional airplane are used to provide rotation about the -

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