Fluid Capacities And Specification - MAULE Orion M-7-260C 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.)
Rev. C
MAULE AEROSPACE TECHNOLOGY, INC.
MAINTENANCE MANUAL
M-7-260C
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.)
Modified USA 35-B
63 inches
+30 minutes
1.2 degrees
None
165.6 sq.ft.
14.2 sq.ft.
23.9 sq. ft.
18.1 sq. ft.
14.1 sq. ft.
13.1 sq. ft.
6.2 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
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