MAULE MX-7-180A - Maximum Weight; Center of Gravity Limits; Maneuvers; Fuel Capacity

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. Refer to
the Weight and Balance Data for baggage/cargo loading recommendations and loading
graphs.
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////CAUTION////
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CHECK WEIGHT AND BALANCE CAREFULLY 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.
1.3 MANEUVERS:
Only Normal Category Maneuvers including Stalls, Lazy Ei
and steep turns involving bank angles
this airplane.
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////CAUTION////
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AEROBATICS AND INTENTIONAL SPINS PROHIBITED.
1.4 FUEL CAPACITY:
Usable Fuel and Unusable Fuel: See Table Below
Fuel Capacity -
See Instrument Panel Placard for Auxiliary T
Tank
Configuration
Tank
Location
A
Main
Aux.
B
Main
Aux.
C
Main
Aux.
D
Main
Aux.
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////CAUTION////
////////////////////////
FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY
CANNOT BE USED SAFELY IN FLIGHT.
FAA APPROVED: 6/3/93
Rev. A dated: 10/28/94
Rev. C dated: 5/28/99
Rev. E dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
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. Refer to
the Weight and Balance Data for baggage/cargo loading recommendations and loading
CHECK WEIGHT AND BALANCE CAREFULLY 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 Ei
and steep turns involving bank angles
not
greater than 60
this airplane.
AEROBATICS AND INTENTIONAL SPINS PROHIBITED.
Usable Fuel and Unusable Fuel: See Table Below
See Instrument Panel Placard for Auxiliary T
ank configuration installed in
Tank
Location
Usable
Fuel (Gal)
Unusable
Fuel (Gal)
Main
Aux.
20.0
15.0
1.5
0.0
Main
Aux.
20.0
21.0
1.5
0.0
Main
Aux.
21.5
15.0
2.3
0.0
Main
Aux.
21.5
21.0
2.3
0.0
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. Refer to
the Weight and Balance Data for baggage/cargo loading recommendations and loading
CHECK WEIGHT AND BALANCE CAREFULLY WHEN CARGO OR
BAGGAGE IS CARRIED IN THE REAR CABIN AREA. ALSO, FLIGHT
PLANNING SHOULD INCLUDE ALLOWANCE FOR FORWARD C.G. SHIFT
Only Normal Category Maneuvers including Stalls, Lazy Ei
ghts, Chandelles
greater than 60
° are approved in
AEROBATICS AND INTENTIONAL SPINS PROHIBITED.
ank configuration installed in
this aircraft.
FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY