GA.140
Type
4-cyl. horizontally opposed air-cooled piston engine
National origin
Italy
Manufacturer
Agusta
The Agusta GA.140/V is a 4-cylinder, air-cooled, horizontally opposed engine mounted vertically, developed in Italy for helicopter use and produced from 1962 to 1969.
Specifications (G.A.140/V)[ edit ] Data from Jane's All the World's Aircraft 1962–63[1]
General characteristics Type: 4-cylinder air-cooled horizontally opposed helicopter piston engine
Bore : 114.3 mm (4.50 in)
Stroke : 88.9 mm (3.50 in)
Displacement : 3.653 L (222.92 cu in)
Length: 580 mm (22.83 in)
Width: 800 mm (31.50 in)
Height: 690 mm (27.17 in)
Dry weight : 116 kg (256 lb) dry
Designer: M. Ginnini
Components Valvetrain : pushrod operated overhead valve, 2x inlet + 2x exhaust per cylinder
Fuel system: Marvel-Schebler MA 4.5 carburettor
Fuel type: 91 octane minimum
Oil system: Pressure lubrication with a gear driven pump
Cooling system: Air-cooled
^ Taylor, John W.R. FRHistS. ARAeS (1962). Jane's All the World's Aircraft 1962–63 . London: Sampson, Low, Marston & Co Ltd.
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