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Piper PA-28 Cherokee

Piper PA-28 Cherokee

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PA-28-140 Cherokee Cruiser
Two place, fixed landing gear landplane, Lycoming O-320-E2A engine of 150 hp (112 kW), gross weight 1,950 lb (885 kg). First certified on 14 February 1964. Approved as a 2,150 lb (975 kg) gross weight four place aircraft on 17 June 1965.
 
PA-28-150 Cherokee
Four place, fixed landing gear landplane, Lycoming O-320-A2B or O-320-E2A engine of 150 hp (112 kW), gross weight 2,150 lb (975 kg). First certified on 2 June 1961.
 
PA-28-151 Cherokee Warrior
Four place, fixed landing gear landplane, Lycoming O-320-E3D engine of 150 hp (112 kW), gross weight 2,325 lb (1,055 kg). First certified on 9 August 1973. Changes from the PA-28-150 include a tapered wing.
 
PA-28-160 Cherokee
Four place, fixed landing gear landplane, Lycoming O-320-B2B or O-320-D2A engine of 160 hp (119 kW), gross weight 2,200 lb (998 kg). First certified on 31 October 1960.
 
PA-28-161 Warrior II
Four place, fixed landing gear landplane, Lycoming O-320-D3G or O-320-D2A engine of 160 hp (119 kW), gross weight 2,325 lb (1,055 kg). First certified on 2 November 1976. Changes from the PA-28-160 include a tapered wing. Certified on 1 July 1982 for gross weight of 2,440 lb (1,107 kg).
 
PA-28-161 Warrior III
Four place, fixed landing gear landplane, Lycoming O-320-D3G engine of 160 hp (119 kW), gross weight 2,440 lb (1,107 kg). First certified on 1 July 1994.
 
PA-28-180 Cherokee
Four place, fixed landing gear landplane, Lycoming O-360-A3A or O-360-A4A engine of 180 hp (134 kW), gross weight 2,400 lb (1,089 kg). First certified on 3 August 1962.
 
PA-28-180 Archer
Four place, fixed landing gear landplane, Lycoming O-360-A4A or O-360-A4M engine of 180 hp (134 kW), gross weight 2,450 lb (1,111 kg). First certified on 22 May 1972. Changes from the PA-28-180 Cherokee include a five inch fuselage extension, wing span increase, larger horizontal tail, gross weight increase and other minor changes.
 
PA-28-181 Archer II
Four place, fixed landing gear landplane, Lycoming O-360-A4M or O-360-A4A engine of 180 hp (134 kW), gross weight 2,550 lb (1,157 kg). First certified on 8 July 1975. Changes from the PA-28-180 include a tapered wing.
 
PA-28-181 Archer III
Four place, fixed landing gear landplane, Lycoming O-360-A4M engine of 180 hp (134 kW), gross weight 2,550 lb (1,157 kg). First certified on 30 August 1994.
 
PA-28-201T Turbo Dakota
Four place, fixed landing gear landplane, turbocharged Continental TSIO-360-FB, engine of 200 hp (149 kW), gross weight 2,900 lb (1,315 kg). First certified on 14 December 1978.
 
PA-28-235 Cherokee Pathfinder
Four place, fixed landing gear landplane, Lycoming O-540-B2B5, O-540-B1B5, or O-540-B4B5 engine of 235 hp (175 kW), gross weight 2,900 lb (1,315 kg). First certified on 15 July 1963.
 
PA-28-235 Cherokee Pathfinder
Four place, fixed landing gear landplane, Lycoming O-540-B4B5 engine of 235 hp (175 kW), gross weight 3,000 lb (1,361 kg). First certified on 9 June 1972. Changes from the 1963 certified PA-28-235 Cherokee Pathfinder include a five inch fuselage extension, wing span increase, larger horizontal tail, gross weight increase and other minor changes.
 
PA-28-236 Dakota
Four place, fixed landing gear landplane, Lycoming O-540-J3A5D engine of 235 hp (175 kW), gross weight 3,000 lb (1,361 kg). First certified on 1 June 1978. Changes from the 1972 certified PA-28-235 Cherokee Pathfinder include tapered wing.
 
PA-28S-160 Cherokee
Four place, fixed landing gear seaplane, Lycoming O-320-D2A engine of 160 hp (119 kW), gross weight 2,140 lb (971 kg). First certified on 25 February 1963.
 
PA-28S-180 Cherokee
Four place, fixed landing gear seaplane, Lycoming O-360-A3A or O-360-A4A engine of 180 hp (134 kW), gross weight 2,222 lb (1,008 kg). First certified on 10 May 1963.
 
PA-28R-180 Arrow
Four place, retractable landing gear landplane, Lycoming IO-360-B1E engine of 180 hp (134 kW), gross weight 2,500 lb (1,134 kg). First certified on 8 June 1967.
 
PA-28R-200 Arrow
Four place, retractable landing gear landplane, Lycoming IO-360-C1C engine of 200 hp (149 kW), gross weight 2,600 lb (1,179 kg). First certified on 16 January 1969.
 
PA-28R-200 Arrow II
Four place, retractable landing gear landplane, Lycoming IO-360-C1C or C1C6 engine of 200 hp (149 kW), gross weight 2,650 lb (1,202 kg). First certified on 2 December 1971. Changes from the 1969 certified PA-28R-200 Arrow include a five inch fuselage extension, wing span increase, larger horizontal tail, gross weight increase and other minor changes.
 
PA-28R-201 Arrow III
Four place, retractable landing gear landplane, Lycoming IO-360-C1C6 engine of 200 hp (149 kW), gross weight 2,750 lb (1,247 kg). First certified on 2 November 1976.
 
PA-28R-201T Turbo Arrow III
Four place, retractable landing gear landplane, turbocharged Continental TSIO-360-F or TSIO-360-FB engine of 200 hp (149 kW), gross weight 2,900 lb (1,315 kg). First certified on 2 November 1976.
 
PA-28RT-201 Arrow IV
Four place, retractable landing gear landplane, Lycoming IO-360-C1C6 engine of 200 hp (149 kW), gross weight 2,750 lb (1,247 kg). First certified on 13 November 1978. Features a T tail.
 
PA-28RT-201T Turbo Arrow IV
Four place, retractable landing gear landplane, turbocharged Continental TSIO-360-FB engine of 200 hp (149 kW), gross weight 2,900 lb (1,315 kg). First certified on 13 November 1978. Features a T tail.

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