1

Question 1

Center of Gravity Calculated as:

Answer 1

Total Moment divided by Total Weight

1. Total Weight Divided by Total Moment
2. Total Moment Divided by Total Height

Question 2

Empty Weight of the aircraft includes:

Answer 2

All the Above

1. Residual Fuel and Oil
2. Weight of the airframe, powerplant and optional or special equipment
3. Hydraulic fluid

Question 3

Electronically operated scale called:

Answer 3

Load Cell

1. Spring Type
2. Beam Scale

Question 4

Find the moment, if a 5 lb radio located 80” from the datum?

Answer 4

400 in-lb

• 400 lb
• 200 in-lb

Question 5

Find the New Center of Gravity?
Airplane Empty Weight - 2,350 lb, Airplane Empty Weight CG - +24.7”, Airplane Datum - Leading edge of the wing, Radio Installed - 5.8 lb at an arm of (-28)”, Global Positioning System Installed - 7.3 lb at an arm of (-26)”, Emergency Locater Transmitter Installed - 2.8 lb at an arm of (+105)”, Strobe Light Removed - 1.4 lb at an arm of (+75)”, Automatic Direction Finder (ADF) removed - 3 lb at an arm of (-28)”, Seat removed - 34 lb at an arm of (+60)”.

Answer 5

24.03”

Question 6

How to determine Useful load?

Answer 6

Subtract the empty weight from the maximum allowable gross weight

1. Add the empty weight from the maximum allowable gross weight
2. Multiply the empty weight from the maximum allowable gross weight

Question 7

How weight and balance extreme condition check done?

Answer 7

By pencil and paper only

1. None of the above.
2. Weighing aircraft on scale

Question 8

Maximum Zero Fuel Weight means:

Answer 8

The heaviest weight an aircraft can be loaded to without having any usable fuel in the fuel tank.

1. The heaviest weight of the aircraft without oil and fuel
2. The heaviest weight an aircraft can be loaded with full fuel in the fuel tank

Question 9

Payload Includes:

Answer 9

Useful weight minus Fuel

1. Without the weight of Passengers.
2. Useful weight minus Fuel