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Piper PA-20 Pacer

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The PA-20 Pacer and PA-22 Tri-Pacer are a family of four-place, strut braced, high-wing light aircraft that were built by Piper Aircraft. The PA-20 and PA-22 were produced from 1950-1954 and 1950-1964, respectively.
 
PA-20
Four-seat, conventional landing gear, light cabin aircraft, powered by a 125 hp (93 kW) Lycoming O-290-D engine. Certified 21 December 1949
PA-20S
Three-seat, conventional landing gear, light cabin aircraft, with optional float installation, powered by a 125 hp (93 kW) Lycoming O-290-D engine. Certified 18 May 1950.
PA-20 115
Four-seat, conventional landing gear, light cabin aircraft, powered by a 115 hp (86 kW) Lycoming O-235-C1 engine. Certified 22 March 1950.
PA-20S 115
Three-seat, conventional landing gear, light cabin aircraft, with optional float installation, powered by a 115 hp (86 kW) Lycoming O-235-C1 engine. Certified 18 May 1950.
PA-20 135
Four-seat, conventional landing gear, light cabin aircraft, powered by a 135 hp (101 kW) Lycoming O-290-D2 engine. Certified 5 May 1952.
PA-20S 135
Three-seat, conventional landing gear, light cabin aircraft, with optional float installation, powered by a 135 hp (101 kW) Lycoming O-290-D2 engine. Certified 15 May 1952.
PA-22
Four-seat, tricycle landing gear, light cabin aircraft, powered by a 125 hp (93 kW) Lycoming O-290-D engine. Certified 20 December 1950.
PA-22-108 Colt
Two-seat, tricycle landing gear, light cabin aircraft, powered by a 108 hp (81 kW) Lycoming O-235-C1 or C1B engine. Certified 21 October 1960.
PA-22-135
Four-seat, tricycle landing gear, light cabin aircraft, powered by a 135 hp (101 kW) Lycoming O-290-D2 engine. Certified 5 May 1952.
PA-22S-135
Three-seat, tricycle landing gear, light cabin aircraft, with optional float installation, powered by a 135 hp (101 kW) Lycoming O-290-D2 engine. Certified 14 May 1954.
PA-22-150
Two or four-seat, tricycle landing gear, light cabin aircraft, powered by a 150 hp (112 kW) Lycoming O-320-A2A or A2B engine. Certified 3 September 1952 as a four place in the normal category and 24 May 1957 as a two place in the utility category.
PA-22S-150
Three-seat, tricycle landing gear, light cabin aircraft, with optional float installation, powered by a 150 hp (112 kW) Lycoming O-320-A2A or A2B engine. Certified 3 September 1954.
PA-22-160
Two or four-seat, tricycle landing gear, light cabin aircraft, powered by a 160 hp (119 kW) Lycoming O-320-B2A or B2B engine. Certified 3 September 1952 as a four place in the normal category and as a two place in the utility category.
PA-22S-160
Three-seat, tricycle landing gear, light cabin aircraft, with optional float installation, powered by a 160 hp (119 kW) Lycoming O-320-B2A or B2B engine. Certified 25 October 1957.

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