// Flight Simulator 2002/4 A I a i r c r a f t configuration file // Aerospatiale/Eurocopter AS365N3 Dauphin // (C) Antti Pankkonen 12.01.2003 //cfg file updated by Greg D. Swagler, SpectroGrafx Productions, Inc. //www.sgpi.net - July 04, 2004 //Repaint by John Elliott Young (J.E.Young@bluestreamair.com) //AI cfg file modifications by The Rhythmosaur [fltsim.0] title=AI Aerospatiale HH65A Dolphin N975BS sim=Dauphin model= panel= sound= texture=N975BS atc_id_enable=1 atc_id=N975BS ui_manufacturer=Z AI //to make it show up at the very end of the List ui_type="Aerospatiale HH65A Dolphin" ui_variation="Bluestream Airlines - N975BS" atc_heavy=0 atc_airline=BLUESTREAM AIR atc_flight_number=401 prop_anim_ratio=1.41 description=----------- A I A i r c r a f t. Not configured for use! ---------------------------------- This particular hellicopter was obtained by Bluestream Airlines as a surplus purchase from the US Coast Guard.\nPaint by John Elliott Young of SpectroGrafx Productions, Inc. (www.sgpi.net) \ncopyright 2004, J.E.Young@bluestreamair.com\n\nThe HH65A Dolphin is the US military version of the civil AS365 Dauphin series, this version is different from the French made aircraft by the use of American made equipment. The HH65 is powered by 2 Honeywell LTS101-750B2 turbine engines which has had a bad reputation in the past. New engine components have made this helicopter perform better. This particular hellicopter was obtained by Bluestream Airlines as a surplus purchase from the US Coast Guard.\nPaint by John Elliott Young of SpectroGrafx Productions, Inc. (www.sgpi.net) \ncopyright 2004, J.E.Young@bluestreamair.com visual_damage=1 [General] atc_type=AEROSPATIALE atc_model=AS65 performance=Manufacturer: Aerospatiale\nRotor Diameter: 39 2"\nHeight: 13\nLength: 44 5"\nMax Gross Weight: 9,200 pounds\nEmpty Weight: 6,092 pounds\nNumber Engines: 2\nPropulsion Type: Lycoming LTS-101-750B-2 Gas Turbines\nFuel Capacity: 1,900 pounds\nMax Endurance: 3.5 hours\nMax Speed: 165 knots\nCruising Speed: 120 knots\nMax Range: 300 nautical miles\nRadius of Action: 150 nautical miles\nService Ceiling (Hover): 7,510 feet above sea level\nNumber of Pilots: 2\nNumber of Passengers: 6\n [turboprop_engine] power_scalar=1.0 maximum_torque=1865.000000 [propeller] thrust_scalar=1.0 thrust_scalar=1.0 propeller_type=1 propeller_diameter=6.883000 propeller_blades=2 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 [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=6184.000 empty_weight_roll_MOI=13200.000 empty_weight_pitch_MOI=15800.000 empty_weight_yaw_MOI=16800.000 empty_weight_coupled_MOI=0.000 max_gross_weight=9369.000 CG_forward_limit=0.000 CG_aft_limit=1.000 // //-----Fuel quantity is set to 1/3 of the real aircraft - //-----to get fuel flow and range to match those of real thing. - //-----Gauges are scaled to display correct values. - // [fuel] Center1=0.000, 0.000, 0.000, 100.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=2 electric_pump=0 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 10, 17.0 avionics=0, 5, 27.5 pitot_heat=0, 2, 17.0 max_battery_voltage=27.9 additional_system=0, 20, 17.0 marker_beacon=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_panel=0, 5 , 17.0 [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, 1 Adf.1=1 Transponder.1=1 Marker.1=1 [contact_points] //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) static_pitch=-5.000 static_cg_height=2.294 point.0=3.000, -21.200, 0.000, -0.400, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.1=1.000, 9.250, 0.000, -2.560, 1378.000, 0.000, 0.984, 38.000, 0.960, 1.250, 0.227, 1.000, 1.000, 0.000, 0.000, 0.000 point.2=1.000, -3.000, -3.330, -3.380, 1378.000, 1.000, 1.148, 0.000, 0.860, 1.350, 0.330, 1.500, 1.500, 2.000, 0.000, 0.000 point.3=1.000, -3.000, 3.330, -3.380, 1378.000, 2.000, 1.148, 0.000, 0.860, 1.350, 0.330, 1.500, 1.500, 3.000, 0.000, 0.000 point.4=2.000, 11.000, 0.000, 1.000, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.5=2.000, -22.000, 0.000, 1.500, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.000, 0.000, -19.000, 7.300, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.7=2.000, 0.000, 19.000, 7.300, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 gear_system_type=0 [exits] number_of_exits=1 exit_rate.0=0.4 [GeneralEngineData] engine_type=5 Engine.0=-2.4, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.12 //Scalar for fuel flow efficiency min_throttle_limit=-0.25 //Minimum percent throttle. Generally negative for turbine reverser [Reference Speeds] flaps_up_stall_speed=54.000000 full_flaps_stall_speed=43.200000 cruise_speed=141.000000 max_indicated_speed=182.000 max_mach=1.000000 [smokesystem] smoke.0=2.00, -7.00, -1.70, fx_helismAS365 smoke.1=2.00, -7.00, 1.70, fx_helismAS365 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=-0.72,1.4,3.2 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks landrotorwash=fx_rtr_lnd waterrotorwash=fx_rtr_wtr [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -16.6, -5.30, 0.90, fx_navred , light.1=3, -16.6, 5.30, 0.90, fx_navgre , light.2=3, -25.4, 0.00, 0.90, fx_navwhi , light.3=2, -24.2, -0.20, 9.30, fx_as365 , light.4=4, 1.00, -1.00, 1.50, fx_vclight , light.5=4, -4.50, 0.00, 1.30, fx_vclight , light.6=4, 1.00, 1.00, 1.50, fx_vclight , [direction_indicators] direction_indicator.0=3,0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=0.001 autothrottle_available=1 pitch_takeoff_ga=0.000000 autothrottle_arming_required=1 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 max_pitch=10.000 max_pitch_acceleration=1.000 max_pitch_velocity_lo_alt=2.000 max_pitch_velocity_hi_alt=1.500 max_pitch_velocity_lo_alt_breakpoint=20000.000 max_pitch_velocity_hi_alt_breakpoint=28000.000 max_bank=25.000 max_bank_acceleration=1.800 max_bank_velocity=3.000 max_throttle_rate=0.100 nav_proportional_control=9.000 nav_integrator_control=0.250 nav_derivative_control=0.000 nav_integrator_boundary=2.500 nav_derivative_boundary=0.000 gs_proportional_control=9.520 gs_integrator_control=0.260 gs_derivative_control=0.000 gs_integrator_boundary=0.700 gs_derivative_boundary=0.000 yaw_damper_gain=1 use_no_default_bank=1 default_bank_mode=0 [brakes] toe_brakes_scale=1.916 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000 flap_limit_power=0.000 flap_limit_idle=0.000 [hydraulic_system] normal_pressure=0.000 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1, 0 [airplane_geometry] wing_area=279.000000 wing_span=52.083333 wing_root_chord=6.360000 wing_dihedral=3.900146 wing_incidence=2.521362 wing_twist=-1.697388 oswald_efficiency_factor=0.699101 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.590000 wing_pos_apex_vert=0.000000 htail_area=39.000000 htail_span=11.666667 htail_pos_lon=-14.666667 htail_pos_vert=0.000000 htail_incidence=1.999512 htail_sweep=0.000000 vtail_area=18.000000 vtail_span=4.837355 vtail_sweep=0.000000 vtail_pos_lon=-12.583333 vtail_pos_vert=1.500000 elevator_area=16.610000 aileron_area=18.300000 rudder_area=6.650000 elevator_up_limit=28.000447 elevator_down_limit=20.998903 aileron_up_limit=19.996227 aileron_down_limit=15.000035 rudder_limit=23.995472 elevator_trim_limit=19.497754 spoiler_limit=19.996227 spoilerons_available=1 aileron_to_spoileron_gain=1.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=7.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=12.666187,0.000000 flaps-position.2=25.332374,0.000000 flaps-position.3=37.998561,0.000000 [TurbineEngineData] fuel_flow_gain=0.011000 inlet_area=1.000000 rated_N2_rpm=33000.000000 static_thrust=158.000000 afterburner_available=0 [stall_warning] type=1
