Mooney M20C Ranger

Personal use civil aircraft introduced in 1962

Overview

Mooney United States ICAO: M20C 1962–1978

The Mooney M20C Ranger was manufactured by Mooney International Corporation as part of the series of piston-powered, propeller-driven, low-winged, four-seater general aviation aircraft derived from the Mooney M-18 Mite. The M20C Ranger was introduced in 1962 after the all-metal M20B version.

Live Fleet Activity (M20C)

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Specifications

Units
Engine
1 × Lycoming O-360
Engine type
Piston
Power
180 hp · 134 kW
Avionics
—
Wing tips
No winglets
Seats
4
Crew
—
Cabin width
3 ft 7 in  ·  1.09 m
Cabin height
3 ft 8 in  ·  1.11 m
Cabin length
10 ft 10 in  ·  3.30 m
Exterior length
23 ft 2 in  ·  7.06 m
Tail height
8 ft 2 in  ·  2.50 m
Fuselage diameter
3 ft 11 in  ·  1.20 m
Wing span
35 ft 0 in  ·  10.67 m
Baggage volume
21 ft³  ·  0.6 m³
Gross weight
—
Empty weight
—
Max takeoff weight
2,550 lb  ·  1,150 kg
Max landing weight
1,500 lb  ·  700 kg
Max payload
750 lb  ·  350 kg
Fuel capacity
50 gal · 200 L · 100 kg (AvGas)
Max cruise speed
174 kt  ·  200 mph  ·  322 km/h
Maximum speed
—
Cruise speed
—
Approach speed
50 kt  ·  58 mph  ·  93 km/h
Range
660 nm  ·  760 mi  ·  1,220 km
Fuel burn
—
Ceiling
17,500 ft  ·  5,300 m
Rate of climb
1,010 ft/min  ·  5 m/s
Takeoff distance
1,390 ft  ·  430 m
Landing distance
1,550 ft  ·  470 m
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Mooney M20C Mark 21 ‘D-ECRI’

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Operational Context

In January 1960, the manufacturing company Mooney International Corporation began to produce aluminum-based aircraft that would replace the initial wooden structure of the M20. The company persuaded Ralph Harmon to leave McDonnel Aircraft and be in charge of the engineering efforts of the M20. Toward the end of the year, the all-metal M20B was finalized.

After a year, Mooney was able to sell M20B aircraft. In 1962, the M20C was presented. It also went by the name of Mark 21 and then the Ranger. A total of 336 M20Cs were sold in 1962.

The M20C version incorporated few upgrades compared with the M20B such as better control surfaces deflection, improved engine cooling by reducing cowl flap openings, a Hanlon and Wilson exhaust system for enhanced scavenging, a new battery access door, better landing lights, as well as lightweight floor, an added gross weight of 1,168 kg, lesser empty weight, greater maximum flap angle, and newly installed instrument panel layout.

The M20C Ranger has an exterior height of 1.7 meters, an exterior length of 7.06 meters, and a fuselage diameter of 1.2 meters. The tail height is 2.5 meters and the wheelbase is 1.8 meters. It has a low wing with a wingspan of 10.67 meters and internal baggage of 3.40 cubic meters. The aircraft can accommodate a single crew and three passengers on board. It has a maximum takeoff weight of 1,168 kg and a maximum landing weight of 691 kg. It has an empty weight of 692 kg, a maximum payload of 350 kg, and a fuel tank capacity of 52 US gal.

The M20C is powered by a single Lycoming O-360 piston engine. It is a four-cylinder, direct-drive, horizontally-opposed, air-cooled piston with a wet sump oil system and rated at 180 hp thrust. The aircraft has a maximum range of 660 nautical miles and can fly up to 17,500 feet. The rate of climb is 1,010 feet per minute. It has a maximum speed of 174 knots, a normal cruise speed of 158 knots, an economic cruise of 152 knots, and a stall speed of 50 knots.