COCKPIT AND SIMULATION.

Panel and cockpit can be quickly reconfigured to simulate:
– Schweizer 300 for basic training.
– Bell 206 for advanced training, turbine and IFR SE training.

Other cockpit configurations and panels are also available, on customer demand.

Flight Deck equipment:
– Robust dual flight controls with realistic ergonomy.
– Full functional instrument set.
– Sounds and vibration system.
– Intercom with co-pilot.
– Simulated radiocom with instructor.
– Actual seats and seatbelts.

Example in H-300 configuration.

GENERAL DATA

WHAT IS DIFFERENT ?

COCKPIT

VISUAL SYSTEM

DATABASE

INSTRUCTOR STATION

TRAINING

VIDEOS

Instruments:
– 2 Altimeters.
– Airspeed indicator.
– Attitude gyro.
– Horizontal situation indicator.
– Vertical speed indicator.
– Turn/bank indicator.
– Engine and rotor RPM.
– Compass.
– Carburator temperature.(*)
– Manifold pressure.(*)
– Fuel mixture and cut off. (*)
– Carburettor heating.(*)
– magneto selector.(*)
– Fuel quantity.
– Cylinder temperature.(*)
– Oil pressure.
– Oil temperature.
– Amp meter.
– Stop watch.

– Warnings: main gearbox, tailrotor gearbox, voltage, fuel, clutch.
– Breakers, switches : Alternator, Battery, Clutch, etc.
– Turbine output temperature (T4). (**)
– Gas producer RPM. (**)
– Torquemeter. (**)
– Radio-Altimeter.
– Aircraft Lights and instruments brightness.
– Audio panel.
– ADF.
– HSI.
– 2 NAV-COM.
– Transponder.
– DME.
– Intercom with 2 headsets.
– GPS (optional).

(*) pistons engine specific
(**) turbine engine specific

Examples of Simulated Failures:
– Engine failure.
– Engine fire.
– Turbine hot start.
– Turbine wet start.
– Progressive loss of power.
– Carburettor freezing.
– Tail rotor breakdown.
– Tail rotor chips.
– Tail rotor loss of control.
– Main gearbox chips.
– Main gearbox oil leak.
– Main gearbox overheat.
– Tail rotor gearbox oil leak.
– Fuel leak.
– Hydraulic failure.
– Engine oil leak.
– Electrical failure.
– Instrument failure.
– Generator Failure.
– and many more...

Flight dynamics simulated effects:
– All flight conditions: Hover, climb, descent, autorotation, etc.
– Vortex.
– Retreating blade stall.
– Mast bumping.
– Ground turbulences.
– Ground interaction.
– Dynamic rollover.
– Induced Speed.
– Flight controls primary effects.
– Flight controls induced effects.
– Realistic engine procedures, from startup to shutdown.
– Ground effect.
– Mass and inertia.
– Fuselage drag.
– Balance and Loading.
– Atmosphere (temperature, pressure, wind, ground height ,etc).
– Blade number and blade characteristics.
– Clockwise or anticlockwise rotor.
– Blade cross section characteristics.
– Clutch characteristics.
– Engine power ,torque, consumption.
– Power transmission characteristics.

COPYRIGHT H-SIM 2009