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7.16 AIRCRAFT WEIGHT AND BALANCE
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The ______of a body is the result of gravitational force acting on the body
2 points
Weight
Mass
Height
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in every object there is one point at which a single force, equal in magnitude to the weight of the object and directed upward, can keep the body at rest.This point is known as
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centre point
centre of gravity
centre of lift
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first class lever has the
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fulcrum between the applied effort and the resistance
resistance between the applied effort and the fulcrum
applied effort between the fulcrum and the resistance
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The tendency of a force to produce rotation around a given axis is called
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moment arm
moment of force
momentum
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To find the balance point, we must
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divide the total moment by the total weight
divide the total weight by the total arm
divide the total momemt arm by the total weight
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Weight that is installed on an aircraft for the purpose of bringing the center of gravity into the desired range.
2 points
standard weight
ballast
fulcurum
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an imaginary vertical plane or line from which all horizontal measurements of arm are taken
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LEMAC
chord line
Datum
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weight of an aircraft which includes the weight of the airframe, power plant, and required equipment that has a fixed location and is normally carried in the airplane.
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empty weight
take off weight
ramp weight
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Basic Empty Weight + Payload =
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Empty weight
Take off weight
Zero Fuel Weight
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Takeoff Weight - Fuel Used During Flight =
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Empty Weight
Zero fuel Weight
Landing Weight
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Methods for calculating crew and passenger mass values are laid down in
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CAR-47
CAR-94
CAR-128
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weight of the pilot, copilot, passengers,baggage, and usable fuel and drainable oil.
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payload
useful load
empty weight
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it is the empty weight subtracted from the maximum weight.
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useful load
payload
ramp weight
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fuel that cannot be consumed by the engine
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undrainable fuel
unusabale fuel
ramp fuel
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The weight of all items such as chocks or blocks that are used to hold the aircraft on the scales while it is being weighed
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reduction factor
tare
Net weight
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The number that the moment is divided by to get the moment index is called
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index factor
reduction factor
Loading Envelope
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Ramp Weight - Fuel Used for Start, Taxi, and Engine Run-up=
2 points
Empty weight
Payload
Takeoff Weight
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Zero Fuel Weight + Usable Fuel =
2 points
Payload
Ramp Weight
Takeoff Weight
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