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The engines, designated PW535E1, are rated at 3,478 lbf (15.47 kN)/ [4] Unveiled at the May 2023 EBACE show, the FADEC-controlled PW545D is developed for the Cessna 560XL Ascend variant, to be rated at 4,200 lbf (19 kN) and optimized for improved fuel burn and longer time between overhauls (TBO) up to 6,000 hours. [ 2 ]
The PW 300 series has been developed in partnership with MTU who are responsible for the low pressure turbine. The first variant, the PW305A, has the following configuration and was designed with a core flexible enough for engines with take-off thrusts from 20 kN to 31 kN (4,500 to 7,000 lb): a single-stage fan driven by a three-stage low pressure turbine, supercharging a four-stage axial ...
Honeywell HTF7500E turbofans were selected along a Rockwell Collins Pro Line Fusion avionics suite integrated cockpit and a Parker Hannifin fly-by-wire flight control system. [2] At the May 2008 European Business Aviation Convention and Exhibition, the larger was named Legacy 500 priced at $18.4 million and the smaller Legacy 450, priced at $15 ...
Data from Austro Engine and type certificate General characteristics Type: Four-cylinder, four-stroke diesel aircraft engine Bore: 83 mm (3.3 in) Stroke: 92 mm (3.6 in) Displacement: 1,991 cm 3 (121 cu in) Length: 738 mm (29 in) Width: 855 mm (34 in) Height: 574 mm (23 in) Dry weight: 186 kg (410 lb) Mean time between failures: > 100,000 h Time between overhauls: 1,800 h Components Fuel type ...
The GO-300 employs a reduction gearbox, so that the engine turns at 3200 rpm to produce a propeller rpm of 2400. The GO-300 produces 175 hp (130 kW) whereas the ungeared O-300 produces 145 hp (108 kW). [1] The GO-300 engine has a TBO (Time Between Overhaul) of 1200 hours, while 1800 hours is the standard for ungeared O-300 engines.
The Pratt & Whitney PW4000 is a family of dual-spool, axial-flow, high-bypass turbofan aircraft engines produced by Pratt & Whitney as the successor to the JT9D.It was first run in April 1984, was FAA certified in July 1986, and was introduced in June 1987.
The Bombardier Challenger 300 is a 3,100-nautical-mile (5,700 km; 3,600 mi) range super mid-sized business jet designed and produced by the Canadian aircraft manufacturer Bombardier Aerospace. Development of the aircraft, originally called the Bombardier Continental , begun during the late 1990s and was formally launched at the 1999 Paris Air ...
RT300 Jet-A1 Model that runs on Jet A-1 fuel, with a compression ratio of 8.5:1 and produces 31 hp (23 kW) at 7500 rpm. [2]RT300 LCR Model that runs on petroleum or avgas, with a compression ratio of 9.6:1 and produces 32 hp (24 kW) at 7500 rpm.
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