BEFC-STL

N8716U Weight and Balance Calculator (Wheel Pants Removed)


Disclaimer: The following Weight and Balance calculator for N8716U with the wheel pants removed based on the latest aircraft weight and balance data dated February 2, 2015. Pilots are responsible for verifying proposed flights are within the weight and balance limits for their aircraft.

Weight and Balance Weight (lbs) Moment (lb-ins/1000)
Basic Empty Weight (including unusable fuel and full oil) 1384.65 51.1351
Usable fuel (38 gallons maximum. 6 lbs/gal)
Enter 228 for full tanks

Pilot and front passenger (station 34 to 46)
Rear passengers
Baggage area (station 82 to 108, 120 lbs max)
RAMP WEIGHT AND MOMENT
Fuel allowance for engine start, taxi, and runup -7.0 -0.34
TAKEOFF WEIGHT AND MOMENT (maximum 2300 lbs)
Center of Gravity Moment Envelope Min Moment
Max Moment

LOADING LIMITS GRAPH
LOADING ARRANGEMENTS
*Arm for Pilot or passenger center of gravity on adjustable seats positioned for average occupant (used in above W&B Calculator). Number in parentheses indicate forward and aft limits of occupant center of gravity range

**Arm Measured to center of areas shown. These values are used in the above W&B calculator

NOTE: The rear cabin wall (appoximate station 108) can be used as a convenient interior reference points for determining the location of baggage area fuselage stations.