MAULE AEROSPACE TECHNOLOGY, INC.
SECTION I
GENERAL: NORMAL CATEGORY OPERATION
1.1
MAXIMUM WEIGHT: 2400 Pounds
1.2
CENTER OF GRAVITY LIMITS:
Straight line variation between points given
Datum: Wing Leading Edge
NOTE: It is the responsibility of the pilot to assure that the airplane is property loaded. R
fer to the Weight and Balance Data for
and loading graphs.
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////CAUTION////
////////////////////////
CHECK WEIGHT AND BALANCE CAREFULLY, ESPECIALLY WHEN
USING THE 5
IS CARRIED IN T
SHOULD INCLUDE ALLOWANCE FOR FORWARD C.G. SHIFT WITH
FUEL BURN.
1.3 MANEUVERS: Only Normal Category Maneuvers including Stalls, Lazy Eights, Chandelles
and steep turns involving bank angles
this airplane.
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////CAUTION////
////////////////////////
AEROBATICS AND INTENTIONAL SPINS PROHIBITED.
1.4 FUEL CAPACITY:
Usable Fuel: MAIN TANKS
AUXILIARY TANKS
Unusable Fuel: 1.5 Gallons per Main Tank
*Fuel Capacity - See Instrument Panel Placard for Auxiliary Tank configuration installed in
this aircraft.
////////////////////////
////CAUTION////
////////////////////////
FUEL REMAINING IN TANK WHEN INDICA
CANNOT BE USED SAFELY IN FLIGHT.
FAA APPROVED
DATE:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
MX-7-180AC
GENERAL: NORMAL CATEGORY OPERATION
2400 Pounds
CENTER OF GRAVITY LIMITS:
+15.9 to +20.5 @ 2400 lbs.
+12.4 to +20.5 @ 1740 lbs. or less
Straight line variation between points given
Datum: Wing Leading Edge
It is the responsibility of the pilot to assure that the airplane is property loaded. R
fer to the Weight and Balance Data for baggage/cargo loading recommendations
and loading graphs.
CHECK WEIGHT AND BALANCE CAREFULLY, ESPECIALLY WHEN
USING THE 5
TH
SEAT, IF INSTALLED, OR WHEN CARGO OR BAGGAGE
IS CARRIED IN THE REAR CABIN AREA. ALSO, FLIGHT PLANNING
SHOULD INCLUDE ALLOWANCE FOR FORWARD C.G. SHIFT WITH
FUEL BURN.
Only Normal Category Maneuvers including Stalls, Lazy Eights, Chandelles
and steep turns involving bank angles not greater than 60
this airplane.
AEROBATICS AND INTENTIONAL SPINS PROHIBITED.
Usable Fuel: MAIN TANKS
21.5 Gal. Each
AUXILIARY TANKS
15.0 Gal. or 21.0 Gal. each*
Unusable Fuel: 1.5 Gallons per Main Tank
See Instrument Panel Placard for Auxiliary Tank configuration installed in
FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY
CANNOT BE USED SAFELY IN FLIGHT.
PAGE 2
SECTION I
GENERAL
+12.4 to +20.5 @ 1740 lbs. or less
It is the responsibility of the pilot to assure that the airplane is property loaded. Re-
baggage/cargo loading recommendations
CHECK WEIGHT AND BALANCE CAREFULLY, ESPECIALLY WHEN
SEAT, IF INSTALLED, OR WHEN CARGO OR BAGGAGE
HE REAR CABIN AREA. ALSO, FLIGHT PLANNING
SHOULD INCLUDE ALLOWANCE FOR FORWARD C.G. SHIFT WITH
Only Normal Category Maneuvers including Stalls, Lazy Eights, Chandelles
greater than 60
°
are approved in
AEROBATICS AND INTENTIONAL SPINS PROHIBITED.
See Instrument Panel Placard for Auxiliary Tank configuration installed in
TOR READS EMPTY
