Weight & Balance Flashcards

1
Q

What is the definition of Basic Operating Weight (BOW)?

A

Standard aircraft items + crew

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2
Q

What is the maximum baggage compartment floor loading?

A

2500 lbs

65 lbs / square ft

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3
Q

What is the definition of Zero Fuel Weight?

A

BOW + crew + passengers + cargo

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4
Q

What is ramp weight?

A

Zero Fuel Weight + fuel

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5
Q

What is the center of gravity?

A

CG is a point about which the aircraft would balance, normally measured in inches aft of the reference datum or % MAC.

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6
Q

What is MAC?

A

Mean Aerodynamic Chord is the distance from LEMAC to TEMAC.

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7
Q

What are LEMAC and TEMAC?

A

Leading edge and trailing edge of the MAC.

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8
Q

What is the reference datum (reference data line)?

A

A reference point on an airframe from which the horizontal arm can be measured.

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9
Q

What is the horizontal arm?

A

Distance along the longitudinal axis from the RDL to the CG of an item, usually measured in inches to a fuselage station.

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10
Q

What is a fuselage station?

A

The horizontal distance (called an ARM, usually expressed in inches) from RDL used in a formula with weight to determine moment.

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11
Q

What is a moment in reference to the weight and balance formula?

A

The product of a weight and its arm, expressed in inch-pounds.
Gulfstream indexes the number and divides by 10000 for simplicity in calculations.

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12
Q

Why is the zero fuel CG arm (inches) converted to % MAC?

A

To determine the correct elevator trim setting for takeoff using the trim table.

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13
Q

What does the correct elevator trim setting provide for takeoff?

A

Provides a “no additional elevator trim” setting (to maintain V2) in the unlikely event that an engine failure occurs on takeoff.

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14
Q

Where is the reference datum line located on the G550?

A

4 inches aft of the nose of the radome.

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15
Q

What is the G550 maximum ramp weight?

A

91400 lbs

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16
Q

What is the G550 maximum takeoff weight?

A

91000 lbs

17
Q

What is the G550 maximum zero fuel weight?

A

54500 lbs

18
Q

What the G550 maximum landing weight?

A

75300 lbs