Cessna 172 S – Weight & Balance Work Sheet
This sheet is for reference only; always consult with the aircraft POH and documented Weight & Balance.
* Pilot or passenger center of gravity on adjustable seats positioned for average occupant. Numbers in
parentheses indicate forward and aft limits of occupant center of gravity range.
** Arm measured to the center of the areas shown.
N513WF as of 7/17/2015
Basic Empty Weight
+ Front Pilots *
+ Rear Passengers
+ Baggage Area 1 **
+ Baggage Area 2 **
= Zero Fuel Weight
+ Usable Fuel
= Ramp Weight
- Taxi Fuel
= Takeoff Weight / CG
- Fuel Burn
= Landing Weight / CG
WEIGHT
1,702.8
x ARM
41.11
73.00
48.00
8.0
48.00
48.00
= MOMENT
70,005.54