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The Cherokee PA28-140 is part of the esteemed Piper Cherokee series, which has been a popular choice for pilots worldwide. Originally introduced in the 1960s, the Cherokee PA28-140 quickly became known for its dependable performance and user-friendly operation.
1 sty 2024 · Performance specifications. Horsepower: 1 x 150 HP. Best Cruise Speed: 117 KIAS. Best Range (i): 457 NM. Fuel Burn @ 75%: 8.4 GPH. Stall Speed: 45 KIAS. Rate of climb: 820 FPM.
CHEROKEE 140 "B" SECTION Il DESIGN INFORMATION ENGINE AND PROPELLER SECTION Il The Lycoming 0-320-E2A engine installed in the Cherokee PA-28-140 is rated at 140 horsepower at 2450 rpm or 150 horsepower at 2700 rpm. This engine has a compression ratio of 7 to 1 and requires 80/87 minimum octane fuel. Refer to Fuel Requirements, page 41,
Piper has created variations within the Cherokee family by installing engines ranging from 140 to 300 hp (105–220 kW), offering turbocharging, retractable landing gear, constant-speed propellers and stretching the fuselage to accommodate six people.
Cherokee 140 Owner's Handbook. PIPER. 0 2150 pounds weight. airplanes from Gtory at 2150 pounds gross weight. at gross weight under standard Conditions atsea equipment may in 1950 725 Instructional Power Cruise Speed (50% PO Fuel (gal. per hr. 75%) Fuel Consumption (g.ñ. per hr. 50%) Cruising Range (75k; power, sea level.
THE PIPER CHEROKEE SECTION II .DESIGN INFORMATION ENGINE AND PROPELLER . SECTION Il The Lycoming 0-320-E2A engine installed in the Cher.okee PA-28-140 is rated at 140 horsepower 24S0 rpm or 1S0 at 2 700 rpm••. This engine has a compression ratio of 7 to · 1 and · requires 80/87 minimum octane fuel. Ref
The original two-seat Piper Cherokee 140, with a 140 hp Lycoming engine, was announced in February 1964, primarily as a sporting and training aircraft to replace the Piper Colt, but equally suitable for general transportation use.
