MAULE AEROSPACE TECHNOLOGY, INC.
MAINTENANCE MANUAL
FOR M-5-220C
Rev. B 5/38
SECTION I
GENERAL DATA
Type:
Four place high wing cabin monoplane.
Engine Installation:
Single tractor engine in nose of fuselage.
Wing:
Strut braced, two spar, metal covered, modified USA 35-B airfoil. Fiberglass
wing tips.
Fuselage: Welded steel tube structure.
Fuselage and tail group covered with Fiberglass synthetic fabric. Fiberglass
engine cowl. Aluminum skin on forward fuselage and doors.
Landing Gear:
Main gear split axle type, spring-oil oleo shock absorber. Hydraulic
Brakes. Steerable tailwheel (Automatic locking).
Control Systems:
Dual controls wheels, rudder pedals and brakes. All controls directly
cable driven. Fuel control/shut off valve is at the left lower side pan-
el. Mechanical flap and trim controls are at the center on the floor.
All other controls, switches, etc., are instrument panel mounted.
Wing Span 30 feet 10 inches
Length 22 feet 6 ½ inches
Height 6 feet 4 inches
Gross Weight 2300/2500* lbs.
Empty Weight Approx. 1350 lbs.
Wing Loading 14.6/15.8 lbs./sq.ft.
Power Loading 10.9/11.9 lbs./HP
Useful Load Approx.
950/1150 lbs.
Seats Four
Flaps
0°, 15°, 35° or 0°, ** 20°, **40°
Center Cargo Allowance (Sta. 42”) 175 lb. Structural Limit
Baggage Allowance (Sta. 70”) 125 lb. Structural Limit
Baggage Compartment Dimensions 30H x 26W x 21L (Approx.)
*2500 lb. gross weight is applicable if Maule Service Letter No. 51 is complied with.
**20° and 40° Flap Setting is applicable if Maule Service Letter No. 48 is complied with.
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