![]() It has a maximum payload of 245 kg and a usable fuel capacity of 30 US gal. 14 On Trade-A-Plane, there are just a few Tomahawks up for sale, ranging from about 25,000 to 33,000, and on Barnstormers there are postings for the aircraft and aircraft parts as well. The empty weight is 512 kg and the maximum takeoff weight is 757 kg. AOPA Insurance Services estimates an average cost, Piper Tomahawk flown by a low-time pilot will cost 1,000 to 1,500 per year to insure. It has a T-tail configuration with a tail height of 2.77 meters and a fixed tricycle landing gear with a wheelbase of 1.6 meters. The aircraft is a low-wing cantilever monoplane with a wingspan of 10.36 meters and a wing area of 11.59 square meters. It has an external length of 7.04 meters, an external height of 1.95 meters, and a fuselage width of 1.1 meters. The PA-38 Tomahawk featured an enclosed cabin that can accommodate one pilot and one passenger in flight. It featured several improvements such as enhanced cabin heating, a windshield defroster, and an updated elevator trim system. Tomahawk II was the designation given to the 19 versions. The Tomahawk was produced from 1978 to 1982 with a total number of 2,484 Tomahawks built. In 1977, the aircraft was introduced as a 1978 version. ![]() To view the various models currently available, please check out our Piper aircraft for sale for descriptions and photos or PLACE A LISTING of your aircraft for sale.The Piper Tomahawk was developed by Piper in an effort to build an economical two-place trainer aircraft. The aircraft is a widely used primary trainer, but it is also an effective budget cross-country aircraft for two people with its spacious and comfortable cabin. The Tomahawk II featured improved cabin heating and windshield defroster performance improved engine thrust vector an improved elevator trim system better cockpit soundproofing 100% airframe zirconium anti-corrosion treatment larger 6" wheels and tires for greater propeller ground clearance and improved performance on grass and dirt runways. Models built in 19 were known as the Tomahawk II. In production from 1978 to 1982, 2484 Tomahawk aircraft were built. Therefore, student pilots that learn to fly in the Tomahawk transition more successfully to a larger aircraft. PA-38 Tomahawk Avionics Upgrade Equipment. The flight controls of the aircraft mimic those of a much heavier aircraft. We now offer Aircraft Maintenance Capabilities as an AMO with ratings in Aircraft, Avionics. Equipped with the NASA GA(W)-1 Whitcomb airfoil the Tomahawk addresses this requirement by making specific pilot input necessary in recovering from spins. Piper surveyed flight instructors and found they wanted a more spinnable aircraft for training purposes. The Tomahawk PA-38-112 is a single engine monoplane with an enclosed cabin. The airplane was Piper's attempt to create an affordable two-place trainer. ![]() The rate of climb is 718 ft/min (3.65 m/s). Cruise speed is 100 knots (115 mph, 185 km/h), stall speed is 49 knots (56.5 mph, 91 km/h), and maximum speed is 109 knots (126 mph, 202 km/h). The empty weight is 1128 lb (512 kg) and the maximum takeoff weight is 1670 lb (757 kg). The Tomahawk has the capacity for two crew members. A two- seat, fixed tricycle landing gear general aviation airplane, the Piper PA-38 Tomahawk was originally designed for flight training, touring, and personal use. A two-seat, fixed tricycle landing gear general aviation airplane, the Piper PA-38 Tomahawk was originally designed for flight training, touring, and personal use. ![]()
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