Weight and Balance Flashcards

1
Q

What is a consequence of being overweight?

A

The airframe might not be able to handle the loads of flight or even takeoff

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2
Q

What is included in the basic empty weight?

A

Airframe, unusable fuel, Engine, permanently installed equipment, full engine oil

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3
Q

What is added to the basic empty weight to calculate total weight?

A

People, fuel, baggage

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4
Q

How much does 100LL weigh?

A

6 lbs per gallon

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5
Q

What is the consequence of a CG that is too far forward?

A

Reduced elevator authority to rotate for takeoff, risk of hitting nosewheel first on landing

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6
Q

What is the consequence of a CG that is too far aft?

A

Reduced stability in pitch, beyond the aft limit its become instable in pitch and will go nose up until a stall and spin

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7
Q

What is the datum? On the 172?

A

A reference point for calculating CG, it’s the engine bulkhead on the 172

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8
Q

What is the arm?

A

The distance from the datum in measuring CG

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9
Q

What is moment? How is it calculated? What is the moment index?

A

Moment is the effect something causes on the CG / Moment = Arm x Weight / The moment/100 is the moment index

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10
Q

Why is it important to calculage CG from start of flight to burned fuel changes at end of flight?

A

The burning of fuel reduces the weight and moment and may cause the CG by the end of flight to be out of the limits

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11
Q

What is the “utility category” vs “normal category”?

A

More allowable maneuvers, especially spins and spin recovery… utility doesn’t allow rear passengers or baggage

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12
Q

What is the calculation for CG?

A

Total moment / Total Weight = CG

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13
Q

What is maximum ramp weight? Max landing weight? Zero fuel weight

A

Maximum weight before taxi and fuel burn / Max weight to land / Basic empty weight plus crew, passengers, and baggage

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