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Perkins Diesel Conversions & Factory fitted units, by Allan T. Condie, 2nd edition 2000, ISBN 0-907742-79-3 The 4 107T was used in UK Military electricity generating sets, the engines when in need an overhaul were rebuilt by a Kent based engineering works in Ramsgate, adjacent to the inner Harbour known as Walkers Marine (Marine Engineers) Ltd. Houchins of Ashford an MOD contractor would send ...
A Massey Ferguson MF 3660 tractor from the early 1990s. On 16 August 1978, Conrad Black, whose family had obtained control of Argus Corporation, an investor in Massey Ferguson, became active in Massey Ferguson's management. [23] In 1977, chairman Albert A. Thornbrough received a $471,000 salary, the highest executive salary in Canada at the ...
It was 2 wheel drive and the gearbox had 6 forward and 2 reverse gears, (3+1, high / low range) with a mechanical clutch. Later versions (1970 onwards) came with an 8 speed transmission (4 forward & 1 reverse across two ranges, high and low). There was a multi-power option giving 12 forward and 4 reverse gears, plus a hydraulic clutch. [5]
F. Perkins Limited, established on 7 June 1932, was founded by Frank Perkins and Charles Wallace Chapman, on Queen Street, Peterborough, to design and manufacture high-speed diesel engines. [1] Chapman was the design engineer (technical director) and company secretary and had a ten percent shareholding in the company.
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O-335-1 Military designation of vertical installation model for helicopters :175 hp (130 kW) O-335-3 Similar to -1 but changes in starter installation O-335-5 200 hp (149 kW) O-335-5B 200 hp (149 kW) 6A-335 180 hp (134 kW) at 2,800 rpm 6AL-335 150 hp (112 kW) at 2,600 rpm 6A4-125 125 hp (93 kW) at 2,200 rpm 6A4-130 130 hp (97 kW) at 2,200 rpm ...
The DM-165 was a tandem two-seat low-wing monoplane. Powered by a 165 hp (121 kW) Continental IO-346A flat-four piston engine. It had a tailwheel and retractable landing gear which folded inwards. [1] Dalotel was assisted by Société Poulet in the construction of the prototype, registered F-PPZE, which was first flown in April 1969. [1]
With a bore and stroke of 4.25 inches and a compression ratio of 5.2:1, the Scarab developed 125 hp (93 kW) at 2,050 rpm from 422 cu in (7 L) with a dry weight of 285 lb (129 kg). Scarab Junior A 5-cyl. version introduced in 1930 developing 90 hp (67 kW) at 2,125 rpm from 301 cu in (5 L) with a dry weight of 230 lb (104 kg).
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