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The Tomahawk is a single-engined low-wing cantilever monoplane with a T-tail and an enclosed cabin for two. It has a fixed tricycle landing gear and is powered by a Lycoming O-235 four-cylinder piston engine with a twin-bladed tractor propeller.
The Tomahawk II, the later model, is the preferred variant when searching for a secondhand Piper Tomahawk. The Tomahawk IIs are also harder to find than the original Tomahawks because, in addition to their higher demand, fewer than 500 of them were produced.
17 lip 2023 · Piper Tomahawk II PA-38-112 Performance. Takeoff Distance Ground Roll: 820 feet; Takeoff Over 50 ft. Obstacle: 1,460 feet; Rate of Climb, Sea Level: 718 feet per minute; Top Speed: 126 miles per hour; Cruise Speed: 115 miles per hour; Stall Speed: 56.5 mph; Fuel Consumption: 6.5 gallons per hour at 75% power; Range: 539 miles; Service Ceiling ...
Tomahawk II was the designation given to the 1981 and 1982 versions. It featured several improvements such as enhanced cabin heating, a windshield defroster, and an updated elevator trim system. The PA-38 Tomahawk featured an enclosed cabin that can accommodate one pilot and one passenger in flight.
Performance specifications. Horsepower: 1 x 112 HP. Best Cruise Speed: 108 KIAS. Best Range (i): 384 NM. Fuel Burn @ 75%: 7.0 GPH. Stall Speed: 49 KIAS. Rate of climb:
Piper ceased production of the Tomahawk during 1983. Powerplants. One 85kW (112hp) Avco Lycoming O-235-L2A or L2C flat four piston engine driving a two blade fixed pitch Sensenich propeller. Performance. Max speed 202km/h (109kt), max cruising speed 200km/h (108kt), normal cruising speed 185km/h (100kt).
PA38. Light aircraft and basic trainer. In service since 1978. Two seat trainer with a T-tail. 2497 aircraft were built between 1978 and 1983. 1 x 112 HP Avco Lycoming O-235-L2A or L2C piston engine with two blade propeller.
