Weight and Balance
Fuel, Load, & Moments
Aircraft Weight Limits
Performance Changes with Weight
CG Effects
100

This is the horizontal distance in inches from the datum to the item's center of gravity 

What is Arm 

100

This load includes only usable fuel—not trapped fuel or line fuel.

What is fuel load?

100

This is the maximum weight an aircraft can have while sitting on the ramp before engine start.

What is maximum ramp weight?

100

An overloaded airplane requires this to be higher before liftoff.

What is takeoff speed?

100

A forward CG requires this type of trim setting in cruise, increasing drag

What is nose-up trim?

200

This imaginary vertical plane is established by the manufacturer and used for all W&B measurements.

What is the datum?

200

Pilots and passengers, baggage, usable fuel, and drainable oil together make up this category.

What is useful load?

200

The highest weight at which the aircraft is allowed to take off.

What is maximum takeoff weight?

200

An increase in weight leads to this climb characteristic.

What is reduced climb rate?

200

With an aft CG, the aircraft has less of this recovery ability

What is stall recovery?

300

This is the point where the aircraft would balance if suspended.

What is the center of gravity (CG)?

300

This value is calculated by multiplying weight × arm.

What is moment?

300

The highest weight at which the airplane may safely land.

What is maximum landing weight?

300

Overweight aircraft have this cruise characteristic.

What is reduced cruise speed?

300

A forward CG results in this cruise performance change due to added drag.

What is slower cruise speed?

400

This maximum authorized weight includes the aircraft and all of its equipment.

What is maximum weight?

400

The weight of occupants, cargo, and baggage is called this.

What is payload?

400

This limit excludes usable fuel; any weight added beyond it must be fuel only

What is maximum zero fuel weight?

400

One of the landing effects of excessive weight — this value becomes higher.

What is landing speed?

400

With the CG far aft, the elevator and rudder have less of this

What is control authority?

500

This term refers to the standard empty weight plus installed optional equipment.

What is basic empty weight?

500

When a moment is divided by 100, 1,000, or 10,000, it becomes this simplified number.

What is moment index?

500

This weight includes the airframe, engines, and permanently installed equipment

What is standard empty weight?

500

Because of reduced performance, a heavily loaded aircraft will experience this shorter operational capability.

What is reduced maximum range?

500

A forward CG creates this stall characteristic because the wings “feel heavier.”

What is a higher stall speed?

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