Section I; General Data; General Description; Design Specifications - MAULE Jetasen M-4 Maintenance Manual

GENERAL DESCRIPTION:

Type: Four place high wing cabin monoplane.
Engine Installation: Single tractor engine in nose of fuselage.
Wing: Strut braced, two spar, fabric or metal covered, modified USA 35-B airfoil. Fi-
berglass 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
Control Systems: Dual controls wheels and rudder pedals. All controls directly cable

DESIGN SPECIFICATIONS:

Wing Span
Length
Height
Gross Weight
Empty Weight
Wing Loading
Power Loading
Useful Load
Seats
Flaps
Baggage Allowance
Baggage Compartment Dimensions
Wings:
a. Airfoil
b. Chord
c. Incidence
d. Dihedral
e. Sweepback
Rev. B
4/13/16
MAULE AIRCRAFT CORPORATION
MAINTENANCE MANUAL
FOR

SECTION I

GENERAL DATA

Brakes. Steerable tailwheel (Automatic locking).
driven. Fuel control/shut off valve is at the left lower side panel.
Mechanical flap and trim controls are at the center on the floor. All
other controls, switches, etc., are instrument panel mounted.
M-4/C/S/T
29 feet 8 inches
22 feet
6 feet 2½ inches
2100 lbs.*
Approx. 1136 lbs.
13.75 lbs./sq. ft.
14.5 lbs./HP
Approx. 964 lbs.
Four
0°, 15°, 35°*
250 lb. Structural Limit
30H x 26W x 21L
Modified USA 35-B
63 inches
+30 minutes
1.2 degrees
None
1