M160T datasheet

The flagship. 160 hp held flat to 15,000 ft.

DRY MASS 73.1 KGTBO 1 800 HPOWER 160 HP → FL150BOOST 1.42 BAR ABS
Document
DS-M160T-2026
Revision
C
Issued
2026-07-01
Sheets
1 of 1
M160T turbocharged flat-four, three-quarter view with the turbocharger and intercooler slung below the crankcase
General arrangement
Type dataM160T · 2026
Configuration
Flat-four, turbocharged + intercooled
Displacement
1,340 cc
Max power
160 hp @ 5,800 rpm, held to 15,000 ft
Critical altitude
15,000 ft ISA
Reduction drive
2.43 : 1 helical, torsional damper
Dry mass
73.1 kg
TBO
1,800 h
Fuel
UL91 / 100LL (mogas STC in test)
Fuel burn (75%)
23.4 L/h
Cooling
Liquid-cooled heads, air-cooled barrels, air-air intercooler
Boost control
FADEC-governed electric wastegate, dual channel
Turbocharger
Single fixed-geometry, 1.42 bar absolute max
Propeller flange
SAE-1, governor pad standard

Performance and installation

Power and torque, measured on the cellCELL DATA
045901351800651301952602,0002,5003,0003,5004,0004,5005,0005,500Crank rpmhpN·m
PowerTorque
Power
Installation envelopeFWF
668 mm overall574 mmMartlet AeroM160T FWFSide elevSheet 1 of 1Scale NTSRev E

Commercial terms

CommercialEX-WORKS FILTON
Firewall-forward price
$32,400
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