MAULE MX-7-180 - Section V: Weight and Balance; Weight and Balance Data Summary

MAULE
AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
SECTION V
WEIGHT AND BALANCE
Serial Number______________________ Registration Number______________________
It is the responsibility of the airplane owner
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 a
nd/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………………………………………………………__
Useful Load…………………………………………
Empty Center of Gravity…………………………………………._________Inches
Empty Weight Moment………………………………..…………_________
CENTER OF GRAVITY RANGE:
Center of Gravity Range
+16.7
to +20.5 inches
+13.6
to +20.5 inches
NOTE: Straight line variation between given points
DATUM: Wing leading edge
CERTIFIED BY______________________________DATE____________________
FORM 50
Rev. G dated:
Page 17
AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
MX-7-180
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
nd/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………………………………………………………__
25
Useful Load…………………………………………
…………….._________Lbs.
Empty Center of Gravity…………………………………………._________Inches
Empty Weight Moment………………………………..…………_________
CENTER OF GRAVITY RANGE:
Center of Gravity Range
At Weight of
to +20.5 inches
2500 lbs.
to +20.5 inches
1600 lbs. or less
NOTE: Straight line variation between given points
DATUM: Wing leading edge
CERTIFIED BY______________________________DATE____________________
SECTION V
WEIGHT AND
BALANCE
Serial Number______________________ Registration Number______________________
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
WEIGHT AND BALANCE DATA SUMMARY AS DELIVERED FROM THE FACTORY:
Basic Empty Weight (including engine oil)……………………._________Lbs.
25
00___Lbs.
…………….._________Lbs.
Empty Center of Gravity…………………………………………._________Inches
Empty Weight Moment………………………………..…………_________
Inch Lbs.
CERTIFIED BY______________________________DATE____________________