S-55  V2.1
[fltsim.0]
title=Sikorsky S-55 RN
sim=s55
model=2
panel=
sound=
texture=RN
kb_checklists=S-55_Checklist
kb_reference=S-55_Reference
prop_anim_ratio=-1.30
ui_manufacturer=Sikorsky 
ui_type=Sikorsky S-55
ui_variation=1. Westland Whirlwind HAS Mk22, Royal Navy, 1955
atc_id=WV223
atc_heavy=0
atc_airline=NAVY
atc_flight_number=WV223
description=The S-55 started life as the venerable military version and first flew in 1949.  The S-55 served with the USN as the H04S, the Air Force as the H-19 and the Marines as the HRS.  Commercial certification was awarded in 1952 for the S-55.  Initial engines were P&W Wasp Radials, later variants had the P&W R-1300 and later still the P&W R-1340. UK versions were built under license and 400 examples were produced as the WS-55 Whirlwind, these later featured the Rolls Royce Bristol Gnome engine turbine, a replacement for the original Alvis radial engine.  France and Japan also had a license for S-55 construction.  Total production globally stands at 1281 airframes, the majority of which are for the US services.

[fltsim.1]
title=Sikorsky S-55 USMC
sim=s55
model=2
panel=
sound=
texture=usmc
kb_checklists=S-55_Checklist
kb_reference=S-55_Reference
prop_anim_ratio=-1.30
ui_manufacturer=Sikorsky 
ui_type=Sikorsky S-55
ui_variation=2. HRS-1, U.S. Marine Corps, Korea 1952
atc_id=HR13
atc_heavy=0
atc_airline=MARINE
atc_flight_number=HR13
description=The S-55 started life as the venerable military version and first flew in 1949.  The S-55 served with the USN as the H04S, the Air Force as the H-19 and the Marines as the HRS.  Commercial certification was awarded in 1952 for the S-55.  Initial engines were P&W Wasp Radials, later variants had the P&W R-1300 and later still the P&W R-1340. UK versions were built under license and 400 examples were produced as the WS-55 Whirlwind, these later featured the Rolls Royce Bristol Gnome engine turbine, a replacement for the original Alvis radial engine.  France and Japan also had a license for S-55 construction.  Total production globally stands at 1281 airframes, the majority of which are for the US services.

[fltsim.2]
title=Sikorsky S-55 ARMY
sim=s55
model=2
panel=
sound=
texture=army
kb_checklists=S-55_Checklist
kb_reference=S-55_Reference
prop_anim_ratio=-1.30
ui_manufacturer=Sikorsky 
ui_type=Sikorsky S-55
ui_variation=3. H-19 Chickasaw, U.S. Army, Korea 1953
atc_id=114269
atc_heavy=0
atc_airline=ARMY
atc_flight_number=269
description=The S-55 started life as the venerable military version and first flew in 1949.  The S-55 served with the USN as the H04S, the Air Force as the H-19 and the Marines as the HRS.  Commercial certification was awarded in 1952 for the S-55.  Initial engines were P&W Wasp Radials, later variants had the P&W R-1300 and later still the P&W R-1340. UK versions were built under license and 400 examples were produced as the WS-55 Whirlwind, these later featured the Rolls Royce Bristol Gnome engine turbine, a replacement for the original Alvis radial engine.  France and Japan also had a license for S-55 construction.  Total production globally stands at 1281 airframes, the majority of which are for the US services.

[fltsim.3]
title=Sikorsky S-55 RCN
sim=s55
model=
panel=
sound=
texture=rcn
kb_checklists=S-55_Checklist
kb_reference=S-55_Reference
prop_anim_ratio=-1.30
ui_manufacturer=Sikorsky 
ui_type=Sikorsky S-55
ui_variation=4. Sikorsky HO4-S, Royal Canadian Navy, 1956
atc_id=877
atc_heavy=0
atc_airline=NAVY
atc_flight_number=877
description=The S-55 started life as the venerable military version and first flew in 1949.  The S-55 served with the USN as the H04S, the Air Force as the H-19 and the Marines as the HRS.  Commercial certification was awarded in 1952 for the S-55.  Initial engines were P&W Wasp Radials, later variants had the P&W R-1300 and later still the P&W R-1340. UK versions were built under license and 400 examples were produced as the WS-55 Whirlwind, these later featured the Rolls Royce Bristol Gnome engine turbine, a replacement for the original Alvis radial engine.  France and Japan also had a license for S-55 construction.  Total production globally stands at 1281 airframes, the majority of which are for the US services.

[fltsim.4]
title=Sikorsky S-55 RAF
sim=s55
model=2
panel=
sound=
texture=raf
kb_checklists=S-55_Checklist
kb_reference=S-55_Reference
prop_anim_ratio=-1.30
ui_manufacturer=Sikorsky 
ui_type=Sikorsky S-55
ui_variation=5. Westland Whirlwind HAR.4, RAF 155 Sqn. Malaya
atc_id=XJ421
atc_heavy=0
atc_airline=AIR FORCE
atc_flight_number=XJ421
description=The S-55 started life as the venerable military version and first flew in 1949.  The S-55 served with the USN as the H04S, the Air Force as the H-19 and the Marines as the HRS.  Commercial certification was awarded in 1952 for the S-55.  Initial engines were P&W Wasp Radials, later variants had the P&W R-1300 and later still the P&W R-1340. UK versions were built under license and 400 examples were produced as the WS-55 Whirlwind, these later featured the Rolls Royce Bristol Gnome engine turbine, a replacement for the original Alvis radial engine.  France and Japan also had a license for S-55 construction.  Total production globally stands at 1281 airframes, the majority of which are for the US services.

[General]
atc_type=Sikorsky
atc_model=S_55P
performance=Cruise Speed  79 kts\nMax Speed   97 Kts\nEngine 1 P&W R-1340 9 Cyl @ 700shp\nService Ceiling  10,600 ft  3,231 m\nRate of Climb 700'per min\nFuel Capacity  Internal 195 U.S. gal\nRange Internal  405 nm\nEmpty Weight  5,250 lb\nMaximum Gross Weight  7,540 lb\nSeating 2 Crew & 8-12 Passengers
editable=1 
Category=helicopter

[WEIGHT_AND_BALANCE]
max_gross_weight 	= 7540    // (pounds)
empty_weight 	= 5250    // (pounds)

reference_datum_position =  0.33,  0.0, 0.0   // (feet) distance from FlightSim Reference position
empty_weight_CG_position = -0.73,  0.0, 0.0   // (feet) longitudinal, lateral, vertical 

max_number_of_stations = 8
station_load.0 = "210, 2.6,  2.20, 0.0, Pilot"          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "210, 2.6, -2.20, 0.0, Passenger"      // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI   = 13000
empty_weight_roll_MOI    = 11000
empty_weight_yaw_MOI     = 18000
empty_weight_coupled_MOI =     0

[electrical]
;BusType, MaxAmpLoad, MinVoltage       
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 28
generator_alternator_voltage = 28
max_generator_alternator_amps = 180
electric_always_available = 1
gear_motor        = 0, 5, 17
autopilot         = 0, 5, 17
avionics_bus      = 0, 10, 17
avionics          = 1, 5, 17
pitot_heat        = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon     = 0, 2, 17
gear_warning      = 0, 2, 17
fuel_pump         = 0, 5, 17
starter1          = 0, 20, 17
light_nav         = 0, 3, 17
light_beacon      = 0, 3, 17
light_landing     = 0, 5, 17
light_taxi        = 0, 5, 17
light_strobe      = 0, 3, 17
light_panel       = 0, 2, 17

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=  3,  -8.15,  -3.30,  3.15,  fx_navred_AS  ; Nav left
light.1=  3,  -8.15,   3.30,  3.15,  fx_navgre_AS  ; Nav right
light.2=  3, -33.75,   0.00,  6.35,  fx_navwhi_AS  ; Nav tail
light.3 = 1,  -3.71,   0.00,  7.98,  fx_beacon     ; Beacon top
light.4 = 4,   2.95,   0.00,  7.00,  fx_vclight    ; Pilots
light.5 = 4,   1.25,   0.00,  3.00,  fx_vclight    ; Cargo hold fore
light.6 = 4,  -6.25,   0.00,  3.00,  fx_vclight    ; Cargo hold aft
light.7 = 2,  -3.71,   0.00,  7.98,  fx_strobe     ; Strobe top

[TailHook]
tailhook_length=5				;(feet)
tailhook_position=-8.35, 0.0, -1.0  ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0

[contact_points]

        //0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
        //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)

static_pitch = 1.5
static_cg_height = 4.60
max_number_of_points = 8

//--------0-----1------2-------3-----4---5---6-----7----8------9---10----11-12-13-14--15
	     	
point.0 = 1,   6.22, -2.70, -4.96, 2500, 0, 0.45, 140, 0.17, 2.52, 0.8,  0, 0, 2, 00, 300 ; nose wheel left
point.1 = 1,   6.22,  2.70, -4.96, 2500, 0, 0.45, 140, 0.17, 2.52, 0.8,  0, 0, 2, 00, 300 ; nose wheel right
point.2 = 1,  -5.42, -5.90, -5.30, 2500, 1, 1.20,  0,  0.79, 1.25, 0.8,  0, 0, 3, 00, 300 ; aft wheel left
point.3 = 1,  -5.42,  5.90, -5.30, 2500, 2, 1.20,  0,  0.79, 1.25, 0.8,  0, 0, 3, 00, 300 ; aft wheel right
point.4 = 2,   6.60,  0.00, -2.47, 2500, 0, 0.00,  0,  0.0,   0.0, 0.0,  0, 0, 5, 0,  0   ; scrape fuse front
point.5 = 2,  -8.50,  0.00, -2.28, 2500, 0, 0.00,  0,  0.0,   0.0, 0.0,  0, 0, 6, 0,  0   ; scrape fuse aft
point.6 = 2, -31.40,  0.00,  4.43, 2500, 0, 0.00,  0,  0.0,   0.0, 0.0,  0, 0, 9, 0,  0   ; scrape boom
point.7 = 5,   0.00,  0.00,  0.00,    0, 0, 0.00,  0., 0.0,   0.0, 0.0,  1, 1, 0, 0,  0   ; Water rudder

gear_system_type=0

[Views]
eyepoint= 2.4, 1.4, 7.0 

[exits]
number_of_exits=2
exit_rate.0=0.3
exit_rate.0=0.7

[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

[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

[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

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

[Reference Speeds]
cruise_speed            = 79     //Knots True (KTAS)
max_indicated_speed     = 117    //Red line (KIAS)

[autopilot]
autopilot_available= 0
flight_director_available= 0

[yaw_string]
yaw_string_available=1

[brakes]
parking_brake = 1       	    //Parking brake available
toe_brakes_scale = 1.0  	    //Brake scalar

[hydraulic_system]
normal_pressure = 0.0    	    //PSI

[pitot_static]
pitot_heat=1.000000

[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

[deice_system]
structural_deice_type=2

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
startup = fx_ALPHA_S55_engstrt
touchdown=fx_tchdwn_s, 1

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
Center1 =   0.0, 0,  -5, 110, 6
Center2 =  -1.0, 0,  -5,  85, 4
electric_pump=0

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -0.5, 0.0, 0.0                       //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0                           //Fuel flow scalar
min_throttle_limit =  0.0;                      //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 90.0                     //Cubic inches per cylinder
compression_ratio= 8.5                          //Compression ratio
number_of_cylinders=9                           //Number of cylinders
max_rated_rpm= 2700                             //Max rated RPM
max_rated_hp= 700                               //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= 0                                //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= 0                        //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       			=  21.58   
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  	      	=   1.0
governor_pid 				=   0.4, 0, 0.1, 0, 0.2
rotor_brake_scalar     			=   2.5
torque_scalar          			=   3.0
cyclic_roll_control_scalar 		=   1.8
cyclic_pitch_control_scalar 		=   0.6
pedal_control_scalar        		=   1.2
collective_on_rotor_torque_scalar 	=   1.0

[fuselage_aerodynamics]
drag_force_cf      = 4.25
side_drag_force_cf = 10.0
pitch_damp_cf      = -5.0
roll_damp_cf       = -5.0
yaw_damp_cf        = -3.1
yaw_stability_cf   =  0.27

[MainRotor]
Position 			= -0.5, 0.0, 4.91       //Longitudinal, Lateral, Vertical feet from datum
Radius   			= 12.583                  //feet
max_disc_angle 		= 5.0
RatedRpm 			= 510
Number_of_blades 		= 2
Weight_per_blade 		= 26.0
Weight_to_moi_factor 	= 0.58
inflow_vel_reference 	= 59.0

[SecondaryRotor]
Position 		= -28.8, -0.74, 1.8           //Longitudinal, Lateral, Vertical feet from datum
TailRotor 		= 1					//feet
Radius   		= 2.25