MAULE AIRCRAFT CORPORATION
MAINTENANCE MANUAL
FOR
M-4/C/S/T
2
Rev. B
4/13/16
Cont’d
Areas:
a.
Wing, Aileron and Flaps 157.9 sq.ft.
b.
Ailerons (total)
12.8 sq.ft.
c.
Flaps (total)
18.8 sq.ft.
d.
Horizontal Stabilizer
18.1 sq. ft.
e.
Elevators (including tab)
14.1 sq. ft.
f.
Vertical Stabilizer
13.1 sq. ft.
g.
Rudder
5.8 sq. ft.
h.
Elevator Trim tab
1.0 sq. ft.
i.
Rudder Tab
.34 sq. ft.
FLUID CAPACITIES AND SPECIFICATIONS:
a.
Main Fuel Tanks - Inboard - 100 Octane
Right Main Tank
21.0 gallons total
Left Main Tank
21.0 gallons total
Note: 1.5 gallons unusable fuel per main tank
b.
Auxiliary Fuel Tanks (if installed)- Outboard - 100 Octane
Right Auxiliary Tank 11.5 gallons
Left Auxiliary Tank 11.5 gallons
c.
Engine Oil (SAE 50 above 40
°
F, SAE 30 or 10W30 below 40
°
F ambient
air temp, at sea level. Refer to Engine Manual for AD Oil
grades.)
10 quart
d.
Brakes (Texaco Aircraft Hydraulic Oil 15, MIL-H-5606E or equiv.)
1 pint
e.
Landing Gear (For P/N 4015B oleo spring, use New Holland No.134 hydrau-
lic oil or Ford Tractor No. ESN-M2C134-D. 10W30 engine oil may also be
used. For P/N 4161B oleo spring use API GL-4 or GL-5 85W-140 gear oil.
2 pints
