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Avia M 337

inverted six-cylinder air-cooled inline engine

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General referenceInterpretive dossier study · Crown Archives visual atlas
Record originEnglish Wikipedia
Text licenseCC BY-SA 4.0
Source revisionApr 15, 2026
Entity authorityQ4828506
Source-derived summary

The Avia M 337 (originally designated the Walter M337) is an inverted six-cylinder air-cooled inline engine. It was developed by the Czechoslovak company as a six-cylinder derivative of the four-cylinder M 332 engine, going into production in 1960. An unsupercharged version of the M 337 is designated as the LOM M137. Production transferred to Avia in 1964, and to Letecke Opravny Malesice (LOM) in 1992.

Variants

M 337A

Basic supercharged engine - not rated for aerobatics

M 337R

Modified for pusher installation

M 337AK

modified oil system for unlimited inverted flying. "Snap" aerobatics permitted.

M 337AK1

AK fitted with alternator instead of generator

M 337B

Increased max running speed (3000 rpm) - increased power - 175 kW (235 hp).

M 337BK

Aerobatic version of B.

M 337C

Increased compression ratio - 188 kW (252 hp)

M 137A

Unsupercharged version of M 337 130 kW (180 hp) take-off power. Aerobatics allowed.

M 137AZ

As M 137A, with filtered air feed

M 437

Gear ratio 0.7:1 180 kW (240 hp)

Applications

AeroVolga LA-8C

Falconar SAL Mustang

Let L-200 Morava

Zlín Z 526, Z 726

Zlín 142

Zlín Z 43

Specifications (M 337)

Data from Jane's All The World's Aircraft 1980-81

General characteristics

Type: 6-cylinder inverted air-cooled supercharged inline engine

Bore: 105 mm (4.13 in)

Stroke: 115mm (4.53 in)

Displacement: 5.97 L (364.3 in3)

Length: 1,410 mm (55.51 in)

Width: 472 mm (18.58 in)

Height: 628 mm (24.72

Dry weight: 148 kg (326.3 lb)

Components

Valvetrain: OHC two camshaft operated valves per cylinder, sodium filled exhaust valve

Supercharger: Centrifugal

Fuel system: Low-pressure fuel injection

Fuel type: Min 72-78 Octane

Oil system: Dry sump pressure feed system

Cooling system: Air-cooled

Performance

Power output: 157 kW (210 hp) at 2,750 rpm (take-off)

Power-to-weight ratio: 1.06 kW/kg (0.64 hp/lb)

References

Taylor, John W R, ed.

Editorial summary

This brief starts where responsible research should: with the source description of “Avia M 337” as inverted six-cylinder air-cooled inline engine. Everything that follows is an evidence route, not borrowed authority.

Editorial reviewA concise reference frame for defining the subject, testing terminology and identifying the institution closest to the evidence. The current lead gives the account dated anchors—1960, 1964, 1992, 1980—that can be checked directly. The selected authority fields contribute no independent date. The account is most persuasive where Avia, inverted and six-cylinder can be independently traced.
Editorial analysis

Why this record matters

The subject matters to the general reference register because the source frames it as inverted six-cylinder air-cooled inline engine. Its deeper value depends on whether names, dates, institutions and citations support that framing.

Evidence profile

The citation trail is more important than the brevity of the summary: it shows where individual claims can be examined in context. The source revision retrieved here is dated Apr 15, 2026. The linked authority identifier is Q4828506. None of the 0 selected statements returned an explicit reference. The first chronological checks are 1960, 1964, 1992 and 1980.

Critical limits

Overview language is designed for orientation and should not be treated as a substitute for the evidence cited beneath it. The lead is largely declarative, so disagreement and counter-evidence require a deliberate search beyond the opening account. Authority statements aid reconciliation but still require their own references, qualifiers and ranks to be checked.

How to read it

Use the entry as an orientation point, then follow its citations and revision history. Names, dates and institutional relationships should be checked against the original record.

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  2. Expand the search: follow Avia M 337 primary sources, Avia M 337 archive and Avia research across catalogues and specialist indexes.
  3. Test the account: compare the strongest cited source with the responsible institution’s current record and note any disagreement.

Questions for further research

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Source & attribution

This entry incorporates text from Avia M 337” on English Wikipedia. Contributors are listed in the page history. Text is available under the Creative Commons Attribution-ShareAlike 4.0 License. Selected authority identifiers and statements are retrieved from Wikidata under CC0; their references and qualifiers remain part of the verification path.