MAULE AEROSPACE TECHNOLOGY, INC.
MAINTENANCE MANUAL
FOR
MT-7-420
9/02
2
Areas:
a. Wing, Aileron and Flaps
165.6 sq. ft.
b. Ailerons (total)
14.2 sq. ft.
c. Flaps (total)
23.9 sq. ft.
d. Horizontal Stabilizer
18.1 sq. ft.
e. Elevators (including tab)
14.1 sq. ft.
f.
Vertical Stabilizer
13.2 sq. ft.
g. Rudder
6.2 sq. ft.
h. Elevator Trim tab
1.03 sq. ft.
i.
Rudder Tab
.34 sq. ft.
FLUID CAPACITIES AND SPECIFICATIONS:
a. Main Fuel Tanks – (Jet A – wing leading edge inboard)
Right Main Tank 23.8 gallons
Left Main Tank
23.8 gallons
Note: 4.6 gallons unusable fuel (Main fuel tanks considered one tank.)
b. Auxiliary Fuel Tanks – (Jet A – wing leading edge outboard)
Right Auxiliary Tank 21.0 gallons
Left Auxiliary Tank
21.0 gallons
c.
Engine Oil (Mil-L-7808 and later and Mil-L-23699 and later) 10 quart max.
d. Brakes (Texaco Aircraft Hydraulic Oil 15, MIL-H-5606E or equiv.) 1 pint
e. Nosewheel Oleo Strut
(Texaco Aircraft Hydraulic Oil 15, MIL-H-5606E or equiv.) 2 pint (approx.)
Engine Fuel Specifications:
Primary
MIL -T-5624L, grade JP-4 and JP-5
MIL-T-83133A, grade JP-8
ASTM D-1655, Jet B
ASTM D-1655, Jet A or A1
JP-1 fuel conforming to ASTM D-1655, Jet A
Arctic Diesel Fuel DF-A (VV-F-800B) conforming to ASTM D-1655, Jet A or A1
Diesel #1 fuel conforming to ASTM D-1655, Jet A
CAUTION:
Not all No. 1 diesel fuels or JP-1 fuels meet the primary fuel specifications. It
is the responsibility of the operator and supplier to determine whether a given
fuel meets these specifications.
