MAULE MX-7-180B - Weight and Balance Data

MAULE AEROSPACE TECHNOLOGY,
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
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………………………………………………………__
Useful Load……………………………………………………….._________Lbs.
Empty Center of Gravity…………………………………………._________Inches
Empty Weight Moment………………………………..…………_________
CENTER OF GRAVITY RANGE:
Center of Gravity Range
+15.9 to
+20.5 inches
+12.4 to +20.5 inches
NOTE: Straight line variation between given points
DATUM: Wing leading edge
CERTIFIED BY______________________________DATE____________________
Rev. F dated:
FORM 63
MAULE AEROSPACE TECHNOLOGY,
INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180B
AND BALANCE
Serial Number______________________ Registration Number______________________
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
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………………………………………………………__
25
Useful Load……………………………………………………….._________Lbs.
Empty Center of Gravity…………………………………………._________Inches
Empty Weight Moment………………………………..…………_________
CENTER OF GRAVITY RANGE:
Center of Gravity Range
At Weight of
+20.5 inches
2500 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____________________
PAGE 17
SECTION V
WEIGHT AND
BALANCE
Serial Number______________________ Registration Number______________________
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
WEIGHT AND BALANCE DATA SUMMARY AS DELIVERED FROM THE FACTORY:
Basic Empty Weight (including engine oil)……………………._________Lbs.
25
00___Lbs.
Useful Load……………………………………………………….._________Lbs.
Empty Center of Gravity…………………………………………._________Inches
Empty Weight Moment………………………………..…………_________
Inch Lbs.
CERTIFIED BY______________________________DATE____________________