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113:, 5,970 cc (364.3 cu in) displacement, air-cooled, direct drive, gasoline engine design. It employs dual
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Model for advanced aerobatics, including inverted flight. This model can mount an air filter.
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ignition and produces 132.4 kW (178 hp) for take-off at 2750 rpm, with a
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132.9 kW (178 hp) for takeoff, 117.6 kW (158 hp) continuous
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Model for limited aerobatics, to a maximum of 5 seconds inverted flight.
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343:, pages 258-259. Flying Pages Europe SARL, 2015.
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341:World Directory of Light Aviation 2015-16
175:Six cylinder, four stroke aircraft engine
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202:5,970 cc (364.3 cu in)
89:(Letecke Opravny Malesice, Praha) of
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339:Tacke, Willi; Marino Boric; et al:
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421:Air-cooled aircraft piston engines
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426:2000s aircraft piston engines
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229:146.5 kg (323.0 lb)
105:The engine is a six-cylinder
208:1,344 mm (52.9 in)
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85:, designed and produced by
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416:LOM Praha aircraft engines
220:688 mm (27.1 in)
214:468 mm (18.4 in)
193:115 mm (4.5 in)
184:105 mm (4.1 in)
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312:List of aircraft engines
167:General characteristics
163:Tacke and manufacturer
156:Specifications (M132A)
101:Design and development
16:Czech aircraft engine
373:www.pistovemotory.cz
289:Related development
275:Compression ratio
119:compression ratio
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399:Official website
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369:"M137A / M137AZ"
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83:aircraft engine
58:Czech Republic
54:National origin
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47:Aircraft engine
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95:light aircraft
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144:Applications
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38:Avia M-137A
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367:LOM Praha.
262:Performance
107:four-stroke
93:for use in
410:Categories
318:References
240:Fuel type:
234:Components
225:Dry weight
349:1368-485X
161:Data from
150:Zlín Z-50
87:LOM Praha
24:LOM M137
378:19 March
300:LOM M132
295:LOM M337
284:See also
242:gasoline
125:Variants
121:of 6.3.
76:LOM M137
218:Height:
206:Length:
115:magneto
111:in-line
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212:Width:
189:Stroke
136:M137AZ
91:Prague
279:6.3:1
173:Type:
130:M137A
80:Czech
78:is a
43:Type
380:2018
345:ISSN
257:none
180:Bore
74:The
248:air
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355:^
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