M120 datasheet

The working engine. 120 hp, honest numbers, published prices.

DRY MASS 62.4 KGTBO 2 000 HPOWER 120 HPFUEL MOGAS 91E10
Document
DS-M120-2026
Revision
C
Issued
2026-07-01
Sheets
1 of 1
M120 flat-four, three-quarter view: sand-cast crankcase, finned barrels, black crinkle cam covers and the offset reduction drive
General arrangement
Type dataM120 · 2026
Configuration
Flat-four, horizontally opposed
Displacement
1,340 cc
Max power
120 hp @ 5,500 rpm
Cruise power (75%)
90 hp @ 4,900 rpm
Reduction drive
2.43 : 1 helical, torsional damper
Dry mass
62.4 kg
TBO
2,000 h
Fuel
91E10 mogas / UL91 / 100LL
Fuel burn (75%)
17.1 L/h
Cooling
Liquid-cooled heads, air-cooled barrels
Ignition & injection
Dual-channel FADEC, auto altitude compensation
Alternator
600 W integrated PM, dual regulators
Propeller flange
SAE-1 / hydraulic governor pad optional

Performance and installation

Power and torque, measured on the cellCELL DATA
035701051400501001502002,0002,5003,0003,5004,0004,5005,0005,500Crank rpmhpN·m
PowerTorque
Power
Installation envelopeFWF
612 mm overall542 mmMartlet AeroM120 FWFSide elevSheet 1 of 1Scale NTSRev E

Commercial terms

CommercialEX-WORKS FILTON
Firewall-forward price
$24,800
Deposit to hold a build slot
$2,500 (refundable)
Warranty
3 yr / 1,000 h, whichever comes later
Documentation
Free — manuals, ICD, parts catalog

Martlet Aero Ltd, Filton, Bristol. Specifications subject to service-letter revision; data taken from published test-cell records.

Close on the crankcase top deck: the riveted identification plate reading M160T, serial and works
Parting line