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The plans for the Pietenpol Aircamper were originally published in a four-part serial in the "Flying and Glider" Manual of 1932-33. [4] [5] The original model was flown using an Ace four cylinder water-cooled engine. [4] The Model A Ford engine later became the standard powerplant used; the design was first flown with one in May 1929. [1]
The T-47A was a modified version of the Citation S/II (Model 552) for the U.S. Navy, featuring a 5 ft (1.5 m) wingspan reduction and hydraulically boosted ailerons for enhanced maneuverability, 2,900 lbf (13 kN) thrust JT15D-5 engines, a cockpit roof window for better pilot visibility during hard maneuvering, strengthened windshields for ...
Certified on 7 May 1971 and introduced in late 1971 as a 1972 model, the PA-34-200 Seneca is powered by a pair of Lycoming IO-360-C1E6 engines. The righthand engine is a Lycoming LIO-360-C1E6 engine variant, the "L" in its designation indicating that the crankshaft turns in the opposite direction, giving the Seneca counter-rotating engines.
Variant with slotted flaps powered by a 65 hp (48 kW) Lenape LM-3-65 engine. [1] J-3X 1944 variant with cantilever wing powered by a 65 hp (48 kW) Continental A-65-8 engine. [1] L-4B Prospector Canadian manufactured model, with removable rear seat and control, additional capacity, optional extra fuel tank and painted in a PA-12 color scheme. [32]
Data from 1956 Observers Book of Aircraft General characteristics Crew: one Capacity: four passengers Length: 27 ft 0 in (8.23 m) Wingspan: 35 ft 0 in (10.67 m) Height: 10 ft 6 in (3.20 m) Wing area: 175 sq ft (16.3 m 2) Empty weight: 2,850 lb (1,293 kg) Gross weight: 4,600 lb (2,087 kg) Fuel capacity: 100 US gal (83 imp gal; 380 L) Powerplant: 2 × Continental O-470-B horizontally opposed ...
Data from Janes' All The World's Aircraft 1982-83 General characteristics Crew: One Capacity: Five passengers Length: 28 ft 2 in (8.59 m) Wingspan: 36 ft 9 in (11.20 m) Height: 9 ft 8 in (2.95 m) Wing area: 175 sq ft (16.3 m 2) Empty weight: 2,303 lb (1,045 kg) Gross weight: 4,000 lb (1,814 kg) Fuel capacity: 87 US gal (72 imp gal; 330 L) (usable capacity) Powerplant: 1 × Continental Motors ...
The Piper PA-30 Twin Comanche was designed as a twin-engined variant of the Piper PA-24 Comanche.A complex light twin, with retractable landing gear, seating 4 (in original models) to 6 (in later models), and cruise speeds ranging from 160–210 mph on twin 160 horsepower engines, it competed with the more-powerful Cessna 310 and Beech Baron, and later with Piper's other light twins.
Cessna Model 560XL Citation XLS taking off from Innsbruck Airport (February 2014) To produce the Excel, Cessna took the X's cabin fuselage (itself inherited from the Citation III ), shortened it by about 2 feet (0.61 m), and mated it with an unswept wing utilising a supercritical airfoil based on the Citation S/II 's wing and the tail from the ...