MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
SECTION V
WEIGHT AND
BALANCE
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)……………………._________Lbs.
Gross Weight………………………………………………………__2400___Lbs.
Useful Load……………………………………………………….._________Lbs.
Empty Center of Gravity…………………………………………._________Inches
Empty Weight Moment………………………………..…………_________ Inch Lbs.
CENTER OF GRAVITY RANGE:
Center of Gravity Range At Weight of
+15.9 to +20.5 inches 2400 lbs.
+12.4 to +20.5 inches 1740 lbs. or less
NOTE: Straight line variation between given points
DATUM: Wing leading edge
CERTIFIED BY______________________________DATE____________________
FORM 61 PAGE 17
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