Weighty Words
Weighty Calculations
Weighty Matters
Balancing Act
100

Theoretical point at which the entire weight of the aircraft is assumed to be concentrated.

Center of gravity (CG)

100

Weight x Arm = _________

Moment

100

Center of Lift is also known as _______________.

Center of Pressure

100

TRUE of FALSE: When weight is shifted on an aircraft, the total moment and the CG location will change.

True

200

The distance from the datum to the applied force.

Arm

200

Total Moment / Total Weight = ____________

Center of gravity (CG)

200

TRUE or FALSE: To maintain balance, the CG is located slightly behind the center of lift.

False

200

TRUE or FALSE: The addition or removal of weight will not change the CG.

False.

300

Arbitrary point chosen by the manufacturer from which all measurements of arm are taken.

Datum

300

An item located -55 inches would be located 55 inches ________ of datum.

Forward

300

TRUE or FALSE: The arm is positive if it is measured aft of the datum.

True

300

If a Cessna 172 is under max takeoff weight but the CG is slightly aft of CG range, the pilot can legally takeoff if __________.

Shifting the weight brings CG within acceptable range.

400

The product of the weight of an item multiplied by its arm.

Moment

400

The location of Station -67 inches + 67 inches 

Station 0 or the datum

400

TRUE or FALSE: When weight is shifted forward, the total moment increases.

False

400

Item A is loaded on an aircraft. The moment is 5000 lb-in. and the arm is 50 inches. What is the weight?

100 lb.

500

A location in the airplane identified by its arm.

Station

500

Weight Shifted / Total Weight = Change in CG / _____

Distance Weight is Shifted

500

The weight of aviation fuel is __________.

6 lbs. per gallon

500

When attempting to fly an aircraft with a CG aft of the acceptable range, it will stall at a _________ airspeed.

Lower