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The turbine version of the Evolution is powered by the 750 hp (559 kW) Pratt & Whitney PT6A-135A and has a maximum cruise of 300 kn (556 km/h) at 25,000 ft (7,620 m) on a fuel burn of 39 US gal (148 L) per hour of Jet-A. Cruising at an economy cruise of 270 kn (500 km/h) at 28,000 ft (8,534 m) it burns 23 US gal (87 L) per hour.
Percival P.66 Pembroke — 2 x Mk. 127, 540 hp; Percival Provost — 1x Mk. 126, 550 hp; Server-Aero Leo-cat — 1x 560 hp (418 kW) Scottish Aviation Pioneer 2 — 1 x 503/7A, Mk 128 01/2, 520 hp; Scottish Aviation Twin Pioneer CC.1 — 2 x 514/8, 550 hp; Scottish Aviation Twin Pioneer CC.2 — 2 x 531/8,Mk138, 640 hp (564 kW) SR.N1 Hovercraft ...
SOC-1 in 1947 XO3C-1 (Curtiss Model 71) Prototype aircraft, powered by 550 hp (410 kW) Pratt & Whitney R-1340-12 engine. One built, redesignated XSOC-1 on 23 March 1935. [8] SOC-1 (Curtiss Model 71A) Initial production version, with 550 hp (410 kW) Pratt & Whitney R-1340-18 engine enclosed in NACA cowling. Interchangeable float and wheeled ...
The L550E is an air-cooled horizontally-opposed 550cc four-cylinder two-stroke petrol engine developing 37 kW (50 hp) at 7500 rpm which can drive a propeller either directly or geared. It employs a single magneto ignition, four carburettors , and is lubricated by oil mixture lubrication with a fuel to oil ratio of 25:1 for mineral oil or 50:1 ...
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On the top model, the Tramontana XTR, it produces 653 kW (888 PS; 881 hp) and 1,100 N·m (809 lb·ft). The Tramontana C, S and R also feature this V12 in a lower output trim, with outputs ranging from 550–720 hp (410–537 kW). [7] Applications: M285: 2002–2012 Maybach 57 and 62; M285 AMG: 2005 Tramontana; 2009 Tramontana R; 2013 Tramontana XTR
The IOF-550 is an Aerosance FADEC equipped version of the same basic engine, the TSIO-550 is a dual turbocharged version and the TSIOL-550 is a liquid-cooled variant. [ 1 ] [ 2 ] [ 3 ] There is no O-550 engine, which would be a carburetor-equipped variant, hence the base model is the IO-550.
It was re-engined with a single 425 hp (317 kW) Turbomeca Artouste IIB turboshaft replacing the two piston engines, flying in this form in June 1959. [3] After being loaned to the U.S. Navy for evaluation as the Model 59N where it was fitted with floats, it was returned to the Army and its engine replaced by a lighter and more powerful 550 hp ...