Aircraft Turbine Engine Trainer

Engine ignition and starting system is included, as well as the oil, fuel and electrical system are representative of typical aircraft systems. The runnable engine stand is mounted on casters which hallows mobility for easy positioning of the engine. However, the stand must be securely attached to anchoring points prior to operation. The runn able engine can be operated like it is operated on the aircraft during the ground runs over its operating range of rpm as specified by the engine manufacturer for ground operations.
The trainer consists of:
Runnable Aircraft Turbine Engine
Engine Instrument Panel
Oil System
Fuel System
Engine Stand
Engine Electrical System
Safety Barrier with Interlocks.

Fan/Compressor Stages: 1/8
Length(Inches): 75.5
Dry Weight(Lbs.): 725 - 737
Core / Power Turbine Stages: 2/1
Max Diameter(Inches): 33
Max. Power at Sea Level (Lbs.): 4,200 - 4,500
Bypass Ratio:2.0
Specific Fuel Consumption at Maximum power: 0.643 - 0.652.