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Engine/transmission: Originally a Parsons petrol / Wilsons 4 speed at 52 kW. Latterly a Detroit 4-71 / Allison torque converter at 78 kW/ 23 kN. Maximum speed: 33 km/h.9.4tonnes. Operational MOTAT 2. NZR TR class No.171 0-4-0 1960 A & G Price of Thames No.195. Light shunting tractor. Engine: Gardner 6L3, Power: 114KW, Tractive effort: 49 kN.
The engine from Jean Batten's Percival Gull is displayed at MOTAT 2. The Road transport collection rotationally displays in excess of 100 cars, trucks, motorbikes and emergency vehicles. Some of the iconic vehicles in the collection include one of the first Trekka utility vehicles, New Zealand's only homegrown production vehicle built between ...
ADC (from "Aircraft Disposal Company") [3] bought 35,000 war-surplus engines in 1920. Initially produced engines from Renault 70 hp spares. ADC Cirrus. ADC Airdisco; ADC Cirrus; ADC Nimbus, development of Siddeley Puma; ADC Airsix, air-cooled version of Nimbus. Not put into use; ADC BR2 [1] ADC Viper [1] ADC Airdisco-Renault [1]
This category lists multi-engine passenger airline accidents involving loss of all engines in flight and subsequent gliding flight. Causes of these rare situations have included fuel exhaustion or starvation, multiple bird strikes, volcanic ash, extreme weather and hijacking.
German engine maker MTU Aero Engines purchased a Kuznetsov report on the noise characteristics of the NK-93 engine for 600,000 Deutsche marks. [23] When the NK-93 was displayed on the Il-76LL demonstrator at the 2007 MAKS air show, Chinese aircraft manufacturers reportedly made a "tempting offer" to buy all of the NK-93's blueprints and ...
Following an engine shutdown, a precautionary landing is usually performed with airport fire and rescue equipment positioned near the runway. The prompt landing is a precaution against the risk that another engine will fail later in the flight or that the engine failure that has already occurred may have caused or been caused by other as-yet unknown damage or malfunction of aircraft systems ...
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 ...
The engine is a four-cylinder four-stroke, horizontally-opposed, 2,600 cc (158.7 cu in) displacement, air-cooled, direct-drive, gasoline engine design. It employs capacitor discharge ignition and produces 95 hp (71 kW) at 2800 rpm.