A turboshaft engine developed specifically for the Lynx Helicopter.

This is a really nice example sat in a correct transit frame with full blanks fitted and LOG CARD PRINTOUT.

Ideal for a myriad of potential uses – custom jet car, jet boat, jet bike, college instructional use or to fit in your Lynx Helicopter

Complete with log cards showing previously fitted to XZ195 (in 1998), ZD278 (in 2004), ZD280 (in 2006). Log card printout shows 3595.58 hours life consumed and 16404.02 hours life left remaining.

Comes in the lower half of the transit case.

Blanks are fitted.

Starter motor fitted.

Last installed in an aircraft in 2007.

Length: 109cm

Diameter: 59cm

Weight: 183 kg – all Dims approx.

Very much self-contained with on-board oil tank.

Small footprint with terrific power to weight ratio (1000SHP).

EPU – Electronic Protection Unit which shuts or slows the engine down in the event of problems.

Starter motor included.

Specification:

LP Compressor 4 Stage Axial with Bleed Valve

HP Compressor Centrifugal Impeller

Combustion Chamber Reverse Flow Annular with 17 Vaporising Burners

Compressor Turbines 1 Stage Axial each

Power Turbine 2 Stage Axial with reduction gearbox in the nose, output shaft speed 6164 rpm ratio 4.5:1

Starting Starter Generator

Ignition Two Torch Igniters with High Energy Plugs

Fuel System Gear pump with Hydro-mechanical or Electronic Fuel Controls, Electronic Protection System.

Oil System Return System with Pressure and Scavenge pumps, Engine Mounted Tank and Oil cooler

General characteristics

Type: Triple-shaft two-spool turboshaft

Length: 43.4 in (1090 mm)

Diameter: 23.5 in (590 mm)

Dry weight: 414 lb (187 kg)

Components

Compressor: 4-stage axial LP, single-stage centrifugal HP

Turbine: 2-stage power turbine, single-stage LP, single-stage HP

Performance

Maximum power output: 1,000 shp (746 kW)

Overall pressure ratio: 12:1

Air mass flow: 7 lb/sec

RPM: Nh= 43,400rpm Nl=37,600 rpm Npt= 27,738rpm