<P> Some earlier Cherokees used control knobs for the throttle, mixture, and propeller advance (where applicable), while later Cherokees use a collection of two or three control levers in a throttle quadrant . </P> <P> Cherokees normally include a rudder trim knob, which actually controls a set of springs acting on the rudder pedals rather than an external trim tab on the rudder--in other words, the surface is trimmed by control tension rather than aerodynamically . </P> <Dl> <Dt> PA - 28 - 140 Cherokee Cruiser </Dt> <Dd> Two - place, fixed landing gear landplane, Lycoming O - 320 - E2A or O - 320 - E3D 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 . </Dd> <Dt> PA - 28 - 150 Cherokee </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 151 Cherokee Warrior </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 160 Cherokee </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 161 Warrior II </Dt> <Dd> 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). </Dd> <Dt> PA - 28 - 161 Warrior III </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 180 Cherokee </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 180 Archer </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 181 Archer II </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 181 Archer III </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 201T Turbo Dakota </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 235 Cherokee Pathfinder </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 235 Cherokee Pathfinder </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 236 Dakota </Dt> <Dd> 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 . </Dd> <Dt> PA - 28S - 160 Cherokee </Dt> <Dd> 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 . </Dd> <Dt> PA - 28S - 180 Cherokee </Dt> <Dd> 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 . </Dd> <Dt> PA - 28R - 180 Arrow </Dt> <Dd> 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 . </Dd> <Dt> PA - 28R - 200 Arrow </Dt> <Dd> 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 . </Dd> <Dt> PA - 28R - 200 Arrow II </Dt> <Dd> 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 . </Dd> <Dt> PA - 28R - 201 Arrow III </Dt> <Dd> 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 . </Dd> <Dt> PA - 28R - 201T Turbo Arrow III </Dt> <Dd> 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 . </Dd> <Dt> PA - 28RT - 201 Arrow IV </Dt> <Dd> 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 . </Dd> <Dt> PA - 28RT - 201T Turbo Arrow IV </Dt> <Dd> 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 . </Dd> <Dt> PA - 28 - 161 Cadet </Dt> <Dd> Two - place, fixed landing gear landplane, Lycoming O - 320 - D2A or - D3G engine of 160 hp (119 kW), gross weight 2,325 lb (1,055 kg). Replaced the PA - 38 Tomahawk trainer in the late 1980s . Features the older Cherokee "2 side window" fuselage with the later tapered wing . </Dd> <Dt> Archer DX </Dt> <Dd> Four - place, fix landing gear landplane, turbocharged Continental CD - 155 diesel engine of 155 hp (116 kW). Introduced at AERO Friedrichshafen in April 2014 . </Dd> </Dl> <Dt> PA - 28 - 140 Cherokee Cruiser </Dt>

What type of flaps are on a pa28