Beechcraft Musketeer - Variants

Variants

23 Musketeer

Four-seat light cabin aircraft, fixed tricycle landing gear, powered by a 160 hp (119 kW) Lycoming O-320-D2B piston engine, gross weight of 2,300 lb (1,043 kg), first certified 20 February 1962.

A23 Musketeer II

Four-seat light cabin aircraft, fixed tricycle landing gear, powered by a 165 hp (123 kW) Continental IO-346-A piston engine, gross weight of 2,350 lb (1,066 kg), first certified 7 June 1963.

A23A

Four-seat light cabin aircraft, fixed tricycle landing gear, powered by a 165 hp (123 kW) Continental IO-346-A piston engine, gross weight of 2,400 lb (1,089 kg), first certified 5 November 1965.

A23-19 (Model 19)

Two or four-seat light cabin aircraft, fixed tricycle landing gear, powered by a 150 hp (112 kW) Lycoming O-320-E2B, E2C or E3D piston engine, gross weight of 2,200 lb (998 kg), first certified 9 December 1965.

A23-24

Four or six-seat light cabin aircraft, fixed tricycle landing gear, powered by a 200 hp (149 kW) Lycoming IO-360-A2B or A2D, or when equipped with a constant speed propeller a Lycoming IO-360-A1B or A1D piston engine, gross weight of 2,550 lb (1,157 kg), first certified 7 March 1966.

A24

Four or six-seat light cabin aircraft, fixed tricycle landing gear, powered by a 200 hp (149 kW) Lycoming IO-360-A2B or A2D, or when equipped with a constant speed propeller a Lycoming IO-360-A1B or A1D piston engine, gross weight of 2,550 lb (1,157 kg), first certified 5 February 1970.

19A

Two or four-seat light cabin aircraft, fixed tricycle landing gear, powered by a 150 hp (112 kW) Lycoming O-320-E2B, E2C or E3D piston engine, gross weight of 2,250 lb (1,021 kg), first certified 31 August 1967, approved in the aerobatic category 12 March 1968.

M19A

Two-seat light cabin aircraft, fixed tricycle landing gear, powered by a 150 hp (112 kW) Lycoming O-320-E2B, E2C or E3D piston engine, gross weight of 2,250 lb (1,021 kg), first certified 9 December 1969, including in the aerobatic category.

B19

Two or four-seat light cabin aircraft, fixed tricycle landing gear, powered by a 150 hp (112 kW) Lycoming O-320-E2B, E2C or E3D piston engine, gross weight of 2,250 lb (1,021 kg), first certified 13 February 1970, including in the aerobatic category.

B23

Four-seat light cabin aircraft, fixed tricycle landing gear, powered by a 180 hp (134 kW) Lycoming O-360-A2G piston engine, gross weight of 2,450 lb (1,111 kg), first certified 13 December 1967 and in the aerobatic category 22 November 1968.

C23

Four-seat light cabin aircraft, fixed tricycle landing gear, powered by a 180 hp (134 kW) Lycoming O-360-A4G, A2G, A4J or A4K piston engine, gross weight of 2,450 lb (1,111 kg), first certified 13 February 1970 including in the aerobatic category.

A24R Sierra 200

Four or six-seat light cabin aircraft, retractable tricycle landing gear, powered by a 200 hp (149 kW) Lycoming IO-360-A1B or A1D piston engine, gross weight of 2,750 lb (1,247 kg), first certified 23 December 1969.

B24R Sierra 200

Four or six-seat light cabin aircraft, retractable tricycle landing gear, powered by a 200 hp (149 kW) Lycoming IO-360-A1B6 piston engine, gross weight of 2,750 lb (1,247 kg), first certified 18 June 1973.

C24R Sierra 200

Four or six-seat light cabin aircraft, retractable tricycle landing gear, powered by a 200 hp (149 kW) Lycoming IO-360-A1B6 piston engine, gross weight of 2,750 lb (1,247 kg), first certified 1 October 1976.