Section I - General Data; General Description; Design Specification - MAULE Orion M-7-260C 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
Baggage Allowance (Sta. 72")
Baggage Compartment Dimensions
Rev. C
MAULE AEROSPACE TECHNOLOGY, INC.
MAINTENANCE MANUAL
FOR
SECTION I
GENERAL DATA
Four/Five 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.
Spring aluminum main gear. Hydraulic Brakes. Steerable tail-
wheel (Automatic locking)
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.
M-7-260C
32 feet 11 inches
23 feet 7½ inches
6 feet 4 inches over wing
2500 lbs.
Approx. 1535 lbs.
15.1 lbs./sq.ft.
9.6 lbs./HP
Approx. 965 lbs.
Five
Neg. 7°, 0°, 24°, 40°, 48°
250 lb. Structural Limit
38H x 32W x 27L
5/37