Section V; Weight And Balance - MAULE M-7-260C Airplane Flight Manual

SECTION V

5.1 WEIGHT AND BALANCE

Serial Number______________________ Registration Number______________________
It is the responsibility of the airplane owner and the pilot to insure that the airplane is
loaded properly. The empty weight, empty weight center of gravity and useful load are listed
below for this airplane as delivered from the factory. If the airplane has been altered, refer to
the aircraft log and/or aircraft records for this information.
WEIGHT AND BALANCE DATA SUMMARY AS DELIVERED FROM THE FACTORY:
Basic Empty Weight (including engine
oil).........................
Gross
Weight...............................................................
Useful Load........................................................
Empty Center of Gravity.......................................
Empty Weight Moment.........................................
CENTER OF GRAVITY RANGE:
Center of Gravity Range
+16.2 to +20.5 inches
+12.5 to +20.5 inches
NOTE: Straight line variation between given points
DATUM: Wing leading edge
CERTIFIED BY______________________________DATE____________________
DETAILED CALCULATIONS OF EMPTY WEIGHT AND EMPTY WEIGHT CENTER OF
GRAVITY AS DELIVERED FROM FACTORY:
FAA APPROVED
DATE: 11-16-16
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE M-7-260C
2800# Upgross Per STC SA04077CH
21 of 29
_________Lbs.
__2800___Lbs.
_________Lbs.
_________Inches
_________ Inch Lbs.
At Weight of
2800 lbs.
1700 lbs. or less
Rev. A