MAULE MX-7-180B - Section I General; Maximum Weight; Center of Gravity Limits; Maneuvers

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION I
GENERAL:
NORMAL CATEGORY OPERATION
1.1 MAXIMUM WEIGHT:
25
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////
////////////////////////
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 Eights, Chandelles
and steep turns involving bank angles
this airplane.
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////CAUTION////
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AEROBATICS AND INTENTI
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
CANNOT BE USED SAFELY IN FLIGHT.
FAA APPROVED: 7/12/93
Rev. A dated: 10/28/94
Rev. C dated: 5/28/99
Rev. F dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180B
NORMAL CATEGORY OPERATION
25
00 Pounds
CENTER OF GRAVITY LIMITS:
+15.9 to +20.5 @ 2500 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 Eights, Chandelles
and steep turns involving bank angles
not
greater than 60
this airplane.
AEROBATICS AND INTENTI
ONAL 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
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 Eights, Chandelles
greater than 60
° are approved in
ONAL SPINS PROHIBITED.
ank configuration installed in
this aircraft.
FUEL REMAINING IN TANK WHEN INDICATOR READS
EMPTY