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AMT103

Test Retake

TermDefinition
(8153) When Computing Weight and Balance, an Airplane is considered to be in balance when? The average Moment arm of the loaded airplane falls within its CG range.
(8155) The useful load of an aircraft Consists of the? Crew, usable fuel, passengers, and cargo.
(8157) In the theory of weight and balance, what is the name of the distance from the fulcrum to an object? Lever arm
(8161) What type of measurement is used to designate the arm in weight and balance computation? Distance
(8162)What Determines weather the Value of a moment is preceded by a (+)or a minus (-)sign in aircraft weight and balance? The result of the weight being added or removed and its location relative to the datum.
(8163) The Maximum weight of an aircraft is the? Empty weight plus useful load...
(8166) If the reference datum line is placed at the nose of an airplane rather than at the firewall or some other location of the nose, All measurement arms will be in positive numbers.
(8167) Maximum zero fuel weight is the Maximum permissible weight of a loaded aircraft (Passengers, crew,and cargo)
(8169) When Dealing with weight and balance of an aircraft, the term "Maximum Weight" is interrupted to mean the maximum. Authorized weight of the aircraft and its contents.
(8170) The useful load of an aircraft is the difference between The maximum takeoff weight and basic empty weight...
(1883) All other things being equal, if an item of useful load located aft of an aircraft CG is removed, the aircraft CG change will be (-)weight X(+)arm(-)moment
Created by: kstokes
 

 



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