This has never been in an airplane just bench run it has an 1 hr 11 mins on it. This is the E start version.

Olympus HP E-start with 23,5 Kg (230N / 51,7Lbf) thrust

Olympus HP gas-turbine.
E-start system Air-start system
-------------------------------------------------------------------------------------------------------
Diameter 131 mm 131 mm
Length 384 mm 273 mm
Turbine weight 2850 gram 2475 gram
System weight * 3795 gram 3150 gram
Thrust @ max. rpm 230 N 230 N
Thrust @ min. rpm 13 N 13 N
Maximum RPM 108,500 108,500
Idle RPM 36,000 36,000
Pressure ratio @ max. rpm 3,8 :1 3,8 :1
Mass flow @ max. rpm 450 gr/sec. 450 gr/sec.
Normal EGT 700 C 700 C
Maximum EGT 750 C 750 C
Fuel consumption @ max. rpm 640 gr/min. 640 gr/min.
Fuel JP-4/petroleum/Jet A1
Oil 4,5% aeroshell 500 mixed with fuel.
-------------------------------------------------------------------------------------------------------