Fluid Capacities And Specification - MAULE Sportplane Trigear MXT-7-160 Maintenance Manual

DESIGN SPECIFICATIONS: (Cont'd)
Wings:
a.
b.
c.
d.
e.
Areas:
a.
b.
c.
d.
e.
f.
g.
h.
i.
FLUID CAPACITIES AND SPECIFICATIONS:
a. Main Fuel Tanks - Inboard - 100 Octane
b. Auxiliary Fuel Tanks - Outboard - 100 Octane
c. Engine Oil
d. Brakes (Texaco Aircraft Hydraulic Oil 15, MIL-H-5606E or equiv.)
Nosewheel Oleo Strut (Hydraulic Fluid, Texaco Aircraft Hydraulic Oil 15,
e.
Rev. E
MAULE AEROSPACE TECHNOLOGY, INC.
MAINTENANCE MANUAL
MXT-7-160
FOR
Airfoil
Chord
Incidence
Dihedral
Sweepback
Wing, Aileron and Flaps
Ailerons (total)
Flaps (total)
Horizontal Stabilizer
Elevators (including tab)
Vertical Stabilizer
Rudder
Elevator Trim tab
Rudder Tab
Right Main Tank
Left Main Tank
Note: 1.5 gallons unusable fuel per 21.5 gallon main tank
2.3 gallons unusable fuel per 23.8 gallon main tank
Right Auxiliary Tank
Left Auxiliary Tank
(SAE 50 above 60°F, SAE 40 at 30° to 90°F, SAE 20 below
10°F ambient air temp. at sea level. Refer to Engine Manual for
AD Oil grades.)
Mil-H-5606 or equiv.)
Modified USA 35-B
63 inches
+30 minutes
1.2 degrees
None
173.7 sq.ft.
14.2 sq.ft.
23.9 sq. ft.
14.2 sq. ft.
15.7 sq. ft.
12.9 sq. ft.
6.4 sq. ft.
1.03 sq. ft.
.34 sq. ft.
21.5 or 23.8 gallons total
21.5 or 23.8 gallons total
15.0 gallons or 21.0 gallons
15.0 gallons or 21.0 gallons
8.0 qt. Maximum
5.0 qt. Minimum
1 pint
2 pints (approx.)
6/39