[fltsim.0]
title=AGUSTA_HH-3F
sim=AGUSTA_HH-3F
model=
panel=
sound=
texture=
atc_heavy=0
atc_airline=Air Force
atc_flight_number=S21
ui_manufacturer=AGUSTA
ui_type=HH-3F
ui_typerole="Rotorcraft"
ui_createdby="I. D'Attomo & G. Quai"
ui_variation=''S.A.R.''
description=After the experience aquired in building (under licence) the ''Sikorsky H-3/S-61R sea king'', Agusta started the production of this more versatile '' Agusta HH-3F pelican'' for Italian Air Force as replacements of the Grumman HU-16 Albatross used for S.A.R. (Search and Rescue).The 5 bladed Agusta HH-3F helicopters perform S.A.R. missions on land and sea in time of peace and C/SAR (Combat SAR) during military assignement. Here is modeled the Long-range search and rescue helicopter ''Agusta HH-3F Pelican'' based in Pratica di Mare AB.
[General]
atc_type= s.a.r.
performance=Cruise Speed 115 kts \nEngine 2GE-T58-GE-5 1521shp\nMaximum Range 435 nm \nService Ceiling 10,500 ft \nHovering Ceiling 10,500 \nEmpty Weight 6200kg\nMaximum Gross Weight 10000kg \nLength 66.2 ft \nRotor Span 62.3 ftm\nHeight 15.7 ft \nSeating Up to 6
Category=helicopter
[WEIGHT_AND_BALANCE]
max_gross_weight =10200 (pounds)
empty_weight = 1760 // (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 = "170, 0.0, -1.17, 0.0, Co-Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, 0.0, 1.17, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "0, 0.0, -1.42, 0.0, Passenger 1" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "0, 0.0, 0.00, 0.0, Passenger 2" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "0, 0.0, 1.42, 0.0, Passenger 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "0, 0.0, 0.00, 0.0, Baggage" // 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
[turboprop_engine]
power_scalar = 1.0
[propeller]
thrust_scalar = 1.0
[Helicopter]
low_realism_stability_scale =2.2, 2.7, 2.7 //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, 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
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
//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=1, 4.83, 3.33, -4.66, 1574.8, 1, 0.5187, 50.0, 0.286975, 2.5, 0.605067, 5.0, 4.0, 2.0, 0.0, 0.0
point.1=1, -3.50, -3.33, -4.66, 1574.8, 0, 0.5187, 0.00, 0.396299, 2.5, 0.728164, 4.0, 3.0, 0.0, 0.0, 0.0
point.2=1, -3.50, 3.33, -4.66, 1574.8, 0, 0.5187, 0.00, 0.396299, 2.5, 0.728164, 6.0, 5.0, 0.0, 0.0, 0.0
point.3=1, 4.83, -3.33, -4.66, 1574.8, 2, 0.5187, 50.0, 0.286975, 2.5, 0.605067, 7.0, 5.0, 3.0, 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
//Float
point.8= 4, 19.1, -1.8, -1.90, 2500, 0,0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
point.9= 4, 19.1, 1.8, -1.90, 2500, 0,0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
point.10=4, -2.3, -1.8, -1.90, 2500, 0,0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
point.11=4, -2.3, 1.8, -1.90, 2500, 0,0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
static_pitch = 0.198
static_cg_height =4.294
gear_system_type=0
[brakes]
parking_brake =1 //Parking brake available
toe_brakes_scale =0.7 //Brake scalar
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint =19.8, 1.1, 4.7
[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=1,0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 6.50, -8.90, 0.60, fx_navred ,
light.1 = 3, 6.50, 8.90, 0.60, fx_navgre ,
light.2 = 3, -30.80, 0.00, 11.46, fx_navwhi ,
light.3 = 1, -29.70, 0.00, 11.58, fx_beacon ,
light.4 = 2, -29.80, 0.00, 11.58, fx_strobe ,
light.5 = 4, 23.80, 0.00, 2.10, fx_vclighth ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
[fuel]
Center1 = 0.0, 0.0, 0.0, 91.0, 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=1
[GeneralEngineData]
engine_type = 3 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 8.3, 0.0, 0.4 //(feet) longitudinal, lateral, vertical distance from reference datum
//Engine.1 = 8.3, 0.0, 0.4 //(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
[Reference Speeds]
flaps_up_stall_speed = 0.0 //Knots True (KTAS)
full_flaps_stall_speed = 0.0 //Knots True (KTAS)
cruise_speed = 115.0 //Knots True (KTAS)
max_indicated_speed = 130 //Red line (KIAS)
[autopilot]
autopilot_available= 0
flight_director_available= 0
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.10,0.50 ;Percent per second
[yaw_string]
yaw_string_available=1
[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=0
