LOM M132

Type	Aircraft engine
National origin	Czech Republic
Manufacturer	LOM Praha s.p.

The LOM M132 is a Czech aircraft engine, designed and produced by LOM Praha (Letecke Opravny Malesice, Praha) of Prague for use in light aircraft.^[1]

Design and development edit

The engine is a four-cylinder four-stroke, in-line, 3,980 cc (242.9 cu in) displacement, air-cooled, direct drive gasoline engine design. It employs dual magneto ignition and produces 90 kW (121 hp) for take-off at 2700 rpm, with a compression ratio of 6.3.^[1]^[2]

Variants edit

M132A: Model for limited aerobatics, to a maximum of 5 seconds inverted flight.^[1]^[2]
M132AK: Model for advanced aerobatics, including inverted flight.^[1]^[2]

Applications edit

Fisher R-80 Tiger Moth

Specifications (M132A) edit

Data from Tacke and manufacturer^[1]^[2]

General characteristics

Type: Four cylinder, four stroke aircraft engine
Bore: 105 mm (4.1 in)
Stroke: 115 mm (4.5 in)
Displacement: 3,980 cc (242.9 cu in)
Length: 1,052 mm (41.4 in)
Width: 425 mm (16.7 in)
Height: 688 mm (27.1 in)
Dry weight: 105 kg (231.5 lb)

Components

Fuel type: gasoline
Cooling system: air
Reduction gear: none

Performance

Power output: 90 kW (121 hp) for takeoff, 80 kW (107 hp) continuous
Compression ratio: 6.3:1

References edit

^ ^a ^b ^c ^d ^e Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 258-259. Flying Pages Europe SARL, 2015. ISSN 1368-485X
^ ^a ^b ^c ^d LOM Praha. "M132A / M132AK". www.pistovemotory.cz. Retrieved 19 March 2018.

External links edit

Official website

[WDLA15-1] Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 258-259. Flying Pages Europe SARL, 2015. ISSN 1368-485X

[M132-2] LOM Praha. "M132A / M132AK". www.pistovemotory.cz. Retrieved 19 March 2018.

[1]

[2]