[fltsim.0]
title=CH34A
sim=SikorskyCH34A
model=
panel=
sound=
texture=
kb_checklists=CH34A_check
kb_reference=CH34A_ref
prop_anim_ratio=-1.65
atc_id_color=0xc6eff7ff
atc_id=34493

atc_model=
ui_manufacturer=Sikorsky
ui_type=S-58T
ui_variation=Screaming Mimi
description=FS2002 aircraft by Paul Bradshaw. The Sikorsky H-34 was developed in 1950's in order to replace the H-19 for the Armed Services. The H-34 had many different roles throughout all branches of service. Some of them including troop and equipment delivery, aerial mine delivery, medical evacuation and presidential transport just to name a few. The Army's version of the H-34 was called the CH-34A "Choctaw". The CH-34A Choctaw saw most of it's combat action during the VietNam War.  Although first created by Sikorsky, the H-34 soon became used world-wide and being produced by Westland Aircraft and Sud Est of France. This version of the CH-34A "Choctaw", is one of the earlier versions with the old style main landing gear configuration and the flat, side cockpit style windows.


[General]
atc_type=Sikorsky
performance=Cruise Speed \t\n   107 mph          172 km\/h\n\nEngine\nWright R 1820 84 Cyclone   1,525 shp\n\nMaximum Range\n318 m            511 km\n\nService Ceiling\n9,500 ft        2,895 m\n\nHovering Ceiling\n8,900 ft     \n\nFuel Capacity\n160 U.S. gal total      \n\nEmpty Weight\n7,675 lb          3,481 kg\n\nMaximum Gross Weight\n13,300 lb          3,481 kg\n\nMaximum Gross Weight (Sling Load)\n5,000 lb       \n\nLength\t\n46.9 ft\t        14.17 m\n\nRotor Span\n56 ft\t         17.06 m\n\nHeight\n15.11 ft\t         4.8 m\n\nSeating \t\nUp to 18 \n\nUseful Load\t\n10,487 lb\t          \n
editable=1

//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)
Category=helicopter
//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)


[turboprop_engine]
power_scalar=1.0

[propeller]
thrust_scalar=1.0
propeller_type=1
propeller_diameter=56.0
propeller_blades=4
propeller_moi=5.706520
beta_max=0.000000
beta_min=15.000000
min_gov_rpm=0.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000


[Helicopter]
low_realism_stability_scale=1.0, 1.0, 1.0             //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 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.0=3,  -3.56, -3.44, 2.64,  fx_navred ,
light.1=3,  -3.56,  3.44, 2.64,  fx_navgre ,
light.2=1, -34.95,  0.00, 6.54,  fx_beacon ,
light.3=2,  -2.00,  0.00, 6.90,  fx_strobe ,
light.4=4,   2.00,  0.00, 1.50,  fx_vclight ,

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks

[fuel]
Center1   =  0.0, 0.0, -5.0,  30.0, 0.0 
Center2   =  2.0, 0.0,  0.0,  30.0, 0.0
Center3   =  0.0, 0.0,  0.0, 100.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                  
electric_pump=0

[GeneralEngineData]
engine_type=5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=0.0, 0.0, 3.5                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[Reference Speeds]
flaps_up_stall_speed=0.0                   //Knots True (KTAS)
full_flaps_stall_speed=0.0                   //Knots True (KTAS)
cruise_speed=107.0                 //Knots True (KTAS)
max_indicated_speed=1000.000000

[autopilot]
autopilot_available=0
flight_director_available=0

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[WEIGHT_AND_BALANCE]
max_gross_weight=13300                         // (pounds)
empty_weight=7675                             // (pounds)

reference_datum_position=0.0, 0.0, 0.0   // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0.0, 0.0   // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=0.000000,0.000000,0.000000,0.000000
station_load.1=0,  0.0, 0.0, 0.0              //Co-Pilot        Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)


;Moments of Inertia
empty_weight_pitch_MOI=6000
empty_weight_roll_MOI=4000
empty_weight_yaw_MOI=10000
empty_weight_coupled_MOI=0

[contact_points]
point.0=1.000000,-25.754281,0.000000,-5.203224,2000.661648,0.000000,0.574146,60.000000,0.750000,1.000000,0.600000,3.000000,3.000000,0.000000,0.000000,0.000000

point.1=1.000000,2.289998,-5.684776,-5.567264,1574.803150,1.0,1.322178,0.000000,0.700000,2.500000,1.000000,3.000000,3.000000,2.000000,0.000000,0.000000

point.2=1.000000,2.289998,5.684776,-5.567264,1574.803150,2.0,1.322178,0.000000,0.700000,2.500000,1.000000,3.000000,3.000000,3.000000,0.000000,0.000000


static_pitch=0.298
static_cg_height=5.167264
gear_system_type=0

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
elevator=100,  180
aileron=200, 1000
rudder=200, 1000

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[Views]
eyepoint=6.4, 2.0, 6.4

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type=4
direction_indicator.0=3,0
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[brakes]
toe_brakes_scale=1.000031
parking_brake=1
[pitot_static]
pitot_heat=1.000000
[hydraulic_system]
normal_pressure=0.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=5.150000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[deice_system]
structural_deice_type=0