[fltsim.0]
title=Cessna CH-1C Skyhook
sim=CH-1C Skyhook
model=
panel=
sound=
texture=
checklists=
kb_reference=
ui_manufacturer=Cessna
ui_type=CH-1C Skyhook
ui_variation="White and green"
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
prop_anim_ratio=-1.32
description=Number of seats: 4\nEngine: 1 x Continental FSO-470-A rated 260hp\nRotor diameter: 35 ft\nFuselage length: 32 ft\nFuselage width: 5.3 ft\nHeight: 8.3 ft\nGross weight: 3100 lbs\nEmpty weight: 2050lbs\n
[General]
performance= Max. speed: 105 kts,\nCruising speed: 86 kts\nRate of climb: 1151 fpm\nRange: 268 nm
atc_type=HELICOPTER
atc_model=CH-1C
[autopilot]
autopilot_available=0
flight_director_available=0
autothrottle_available=0
[direction_indicators]
direction_indicator.0=3,0
[Helicopter]
low_realism_stability_scale=1.0, 1.0, 1.0 //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings
[WEIGHT_AND_BALANCE]
reference_datum_position=0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=340.000, 0.000, 0.000, 0.000
empty_weight=2050
empty_weight_roll_MOI= 10000.000
empty_weight_pitch_MOI= 10000.000
empty_weight_yaw_MOI= 15000.000
empty_weight_coupled_MOI= 000.000
max_gross_weight=3100
CG_forward_limit=0.000
CG_aft_limit=1.000
[fuel]
Center1= 0.000, 0.000, 0.000, 60.000, 0.000
fuel_type=1.000
number_of_tank_selectors=1
electric_pump=0
//0 Class <0=none,1=wheel, 2=scrape, 3=skid>
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0=3, 4.83, 3.33, -4.99, 1574.8, 0, 0.5187, 0.0, 0.286975, 2.5, 0.605067, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=3, -3.50, -3.33, -4.89, 1574.8, 0, 0.5187, 0.0, 0.396299, 2.5, 0.728164, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=3, -3.50, 3.33, -4.89, 1574.8, 0, 0.5187, 0.0, 0.396299, 2.5, 0.728164, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=3, 4.83, -3.33, -4.99, 1574.8, 0, 0.5187, 0.0, 0.286975, 2.5, 0.605067, 0.0, 0.0, 1.0, 0.0, 0.0
point.4=2, 0.00, -16.67, 9.00, 0.0, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 5.0, 0.0, 0.0
point.5=2, 0.00, 16.67, 9.00, 0.0, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 6.0, 0.0, 0.0
point.6=2, -20.50, 0.00, 1.67, 787.4, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 9.0, 0.0, 0.0
point.7=2, 0.00, 9.08, 2.58, 787.4, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch = 0.190
static_cg_height = 4.99
[GeneralEngineData]
engine_type=3
Engine.0=2.4, 0.0, 0.0
fuel_flow_scalar=1.000
rotation=2,1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW
min_throttle_limit=0.000000
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 86.66 //Cubic inches per cylinder
compression_ratio= 8.5 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 3200 //Max rated RPM
max_rated_hp= 270 //Max rated HP
fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 38.50 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 1 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[Helicopter]
reference_length = 42.75
reference_frontal_area = 17.7
reference_side_area = 44.5
side_aero_center = -12.5
right_trim_scalar = 1.0
correlator_available = 1
governed_pct_rpm_ref = 1.04
governor_pid = 0.4, 0, 0.1, 0, 0.2
rotor_brake_scalar = 1.0
torque_scalar = 1.0
cyclic_roll_control_scalar =1.0
cyclic_pitch_control_scalar =1.0
pedal_control_scalar =1.0
collective_on_rotor_torque_scalar = 1.0
[fuselage_aerodynamics]
drag_force_cf = 0.55
side_drag_force_cf = 10.0
pitch_damp_cf = -2.0
roll_damp_cf = -2.0
yaw_damp_cf = -0.1
yaw_stability_cf = 0.27
[MainRotor]
Position = -8.5, 0, 4.91 //Longitudinal, Lateral, Vertical feet from datum
Radius = 12.583 //feet
max_disc_angle = 5.0
RatedRpm = 415
Number_of_blades = 2
Weight_per_blade = 26.0
Weight_to_moi_factor = 0.58
inflow_vel_reference = 34.0
[SecondaryRotor]
Position = -22.8, -0.74, 1.8 //Longitudinal, Lateral, Vertical feet from datum
TailRotor = 1
Radius = 1.75
[hydraulic_system]
normal_pressure = 600 //PSI
engine_map=1,0,0,0
[Reference Speeds]
flaps_up_stall_speed=0.000
full_flaps_stall_speed=0.0
cruise_speed=100.000
max_indicated_speed=1000.000000
[keyboard_response]
elevator=100.000, 180.000
aileron=200.000, 1000.000
rudder=200.000, 1000.000
spoiler_limit=1.000
spoilerons_available=1
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=10.000
min_flaps_for_spoilerons=0.000
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.5=4,0.0,0.00,0.00,fx_vclight,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
[Radios]
// Radio Type=available, standby frequency, has glide slope
Audio.1=1
Com.1=1,
Com.2=1,
Nav.1=1,
Nav.2=1,
Adf.1=1
Transponder.1=1
Marker.1=1
[exits]
number_of_exits=2
exit_rate.0=0.25 ;Percent per second
exit_rate.1=0.25 ;Percent per second
[Views]
eyepoint= -3.95, -0.85, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum
[brakes]
toe_brakes_scale=0.000000
parking_brake=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
