Mooney M-20 Civil Aircraft Model Details

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General Information of Mooney M-20

Designer : Al Mooney

Introduction : 1955

Manufacturer : Mooney Airplane Company

Produced : 1955–2008[1]

Role : Personal use civil aircraft

Status : Production halted in 2008

Unit_Cost : USD$579,000 (2008 model Mooney Acclaim)[2]

General characteristics of Mooney M-20

Airfoil : NACA 63-215

Capacity : 3 passengers

Crew : one pilot

Empty Weight : 2370 lb (1074 kg)

Height : 8 ft 4 in (2.5 m)

Length : 26 ft 9 in (8.15 m)

Loaded_Weight : 3374 lb (1528 kg)

Max Takeoff Weight : 3374 lb (1528 kg)

Powerplant : 1 × Continental TSIO-550-G Turbo-normalized with twin turbo and dual intercoolers air-cooled, 6-cylinder, horizontally opposed piston engine, 280 hp (171 kW)

Useful Load : 1004 lb (454 kg)

Wing Area : 175.7 sq ft (16.3 m²)

Wingspan : 36 ft 5 in (11.1 m)

Performance of Mooney M-20

Cruise Speed : 237 knots (272 mph, 438 km/h)

Maximum Speed : 242 knots (278 mph, 448 km/h)

Power/Mass : 12.0 lb/hp (0.11 kW/kg)

Range : 1445 nm (std tanks) (1662 mi, 2676 km)

Rate Of Climb : 1240 ft/min (378 m/min)

Service Ceiling : 25,000 ft (7625 m)

Wing Loading : 19.2 lb/ft² (96 kg/m²)

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