The Mooney M-18 Mite is a personal use aircraft designed by Al Mooney and produced by Mooney Aircraft Company for fighter pilots that came from the Second World War. It was introduced in 1947 as a single-place monoplane with low wings and retractable tricycle-type undercarriage. In the same year, it performed its maiden flight and was produced until 1954 with a total number of 283 aircraft built.

Mooney Aircraft
United States
1947 to: 1954
US$0.003 million (1947)
1x Continental A65
65 horsepower
Max Cruise Speed:
120 knots
222 Km/h
Approach Speed (Vref):
37 knots
Travel range:
382 Nautical Miles
707 Kilometers
Fuel Economy:
Service Ceiling:
19,400 feet
Rate of Climb:
1090 feet / minute
5.54metre / second
Take Off Distance:
305 metre - 1,000.64 feet
Landing Distance:
305 metre - 1,000.64 feet
Max Take Off Weight:
354 Kg
780 lbs
Max Landing Weight:
354 Kg
780 lbs
Max Payload:
118 Kg
260 lbs
Fuel Tank Capacity:
12 gallon
45 litre
Baggage Volume:
Seats - Economy / General:
1 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
Cabin Width:
Cabin Length:
Exterior Length:
5.5 metre - 18.04 feet
Tail height:
1.9 metre - 6.23 feet
Fuselage Diameter:
0.85 metre - 2.79 feet
Wing Span / Rotor Diameter:
8.18 metre - 26.84 feet
Wing Tips:
No Winglets

The design of the M-18 Mite aimed an exceptionally low operating cost aircraft. It is mostly built of wood covered in fabric, with a wing spar made of spruce and plywood. The aircraft is also fitted with a distinct safe-trim system that connects the wing flaps to the tail trim system and fits the horizontal stabilizer angle automatically during the deflection of flaps, decreasing or removing pitch changes while the flaps are being lowered. In 1947, the aircraft took to the air for the first time. A total of 283 M-18 Mites were built in Wichita, Kansas, and Kerrville, Texas facility from 1947 to 1954.

The Mooney M-18 Mite is a single-seat trainer with a capacity of 118 kg. It has an external length of 5.5 meters, an external height of 1.4 meters, and a fuselage width of 0.85 meters. It has a tail height of 1.9 meters and a retractable tricycle landing gear with a wheelbase of 1.2 meters. The low wing has a wingspan of 8.18 meters and a wing area of 8.8 square meters. It has an empty weight of 236 kg, a gross weight of 354 kg, and a maximum takeoff weight of 354 kg. The fuel tank capacity is 12 US gal.

The aircraft is powered by a single Continental A65 engine. It is a four-cylinder, horizontally opposed piston engine with one intake and one exhaust valve per cylinder, updraft carburetor fuel system, wet-sump oil system, and an air-cooling system. The engine is rated at 65 hp thrust.

The M-18 Mite has a maximum speed of 120 knots, a cruise speed of 109 knots, and a stall speed of 37 knots. The maximum range is 382 nautical miles. It can fly up to 19,400 feet and can climb at a rate of 1,090 feet per minute. The takeoff and landing distance is 305 meters.

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