Section I - General Data; General Description; Design Specification - MAULE Sportplane Trigear MXT-7-160 Maintenance Manual

GENERAL DESCRIPTION:

Type:
Engine Installation:
Wing:
Fuselage:
Landing Gear:
Control Systems:
DESIGN SPECIFICATIONS:
Wing Span
Length
Height
Gross Weight
Empty Weight
Wing Loading
Power Loading
Useful Load
Seats
Flaps
Center Cargo Allowance (Sta. 42")
Baggage Allowance (Sta. 70")
Baggage Compartment Dimensions
Rev. E
MAULE AEROSPACE TECHNOLOGY, INC.
MAINTENANCE MANUAL
MXT-7-160
FOR
SECTION I
GENERAL DATA
Four place high wing cabin monoplane.
Single tractor engine in nose of fuselage.
Strut braced, two spar, metal covered, modified USA 35-B airfoil. Fi-
berglass wing tips.
Welded steel tube structure.
Fuselage and tail group covered with Ceconite synthetic fabric.
Fiberglass engine cowl. Aluminum skin on forward fuselage and
doors.
Air-oil nosewheel oleo strut, steerable from rudder pedals.
Spring aluminum main gear. Hydraulic Brakes.
Dual controls wheels, rudder pedals and brakes. All con-
trols directly cable 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.
32 feet 11 inches
23 feet 7½ inches
6 feet 10 inches over wing
8 feet 4 inches over rudder
2200 lbs.
Approx. 1400 lbs.
13.3 lbs./sq.ft.
13.8 lbs./HP
Approx. 800 lbs.
Four
Neg. 7°, 0°, 24°, 40°
175 lb. Structural Limit
125 lb. Structural Limit
35 ½ H x 30W x 21L (Approx.)
5/39