[fltsim.0] title=JFAIC17A_RAF_99Sqn sim=JFAIC17A model= panel= sound= texture= atc_id=BLANK atc_flight_number=C17 atc_airline=AIR FORCE atc_parking_codes=C17 atc_parking_types=MIL_CARGO ui_manufacturer=Boeing ui_type=C-17 Globemaster ui_variation=99 Sqn RAF ui_typerole=Military Jet ui_createdby=Just Flight Ltd description=AI [fltsim.1] title=JFAIC17A_USAF_ALTUS sim=JFAIC17A model= panel= sound= texture=1 atc_id=BLANK atc_flight_number=C17 atc_airline=AIR FORCE atc_parking_codes=C17 atc_parking_types=MIL_CARGO ui_manufacturer=Boeing ui_type=C-17 Globemaster ui_variation=USAF Altus AFB ui_typerole=Military Jet ui_createdby=Just Flight Ltd description=AI [fltsim.2] title=JFAIC17A_USAF_CHARLESTON sim=JFAIC17A model= panel= sound= texture=2 atc_id=BLANK atc_flight_number=C17 atc_airline=AIR FORCE atc_parking_codes=C17 atc_parking_types=MIL_CARGO ui_manufacturer=Boeing ui_type=C-17 Globemaster ui_variation=USAF Charleston AFB ui_typerole=Military Jet ui_createdby=Just Flight Ltd description=AI [fltsim.3] title=JFAIC17A_USAF_HICKAM sim=JFAIC17A model= panel= sound= texture=3 atc_id=BLANK atc_flight_number=C17 atc_airline=AIR FORCE atc_parking_codes=C17 atc_parking_types=MIL_CARGO ui_manufacturer=Boeing ui_type=C-17 Globemaster ui_variation=USAF Hickam AFB ui_typerole=Military Jet ui_createdby=Just Flight Ltd description=AI [fltsim.4] title=JFAIC17A_USAF_McCHORD sim=JFAIC17A model= panel= sound= texture=4 atc_id=BLANK atc_flight_number=C17 atc_airline=AIR FORCE atc_parking_codes=C17 atc_parking_types=MIL_CARGO ui_manufacturer=Boeing ui_type=C-17 Globemaster ui_variation=USAF McChord AFB ui_typerole=Military Jet ui_createdby=Just Flight Ltd description=AI [fltsim.5] title=JFAIC17A_USAF_McGUIRE sim=JFAIC17A model= panel= sound= texture=5 atc_id=BLANK atc_flight_number=C17 atc_airline=AIR FORCE atc_parking_codes=C17 atc_parking_types=MIL_CARGO ui_manufacturer=Boeing ui_type=C-17 Globemaster ui_variation=USAF McGuire AFB ui_typerole=Military Jet ui_createdby=Just Flight Ltd description=AI [fltsim.6] title=JFAIC17A_USAF_MARCH sim=JFAIC17A model= panel= sound= texture=6 atc_id=BLANK atc_flight_number=C17 atc_airline=AIR FORCE atc_parking_codes=C17 atc_parking_types=MIL_CARGO ui_manufacturer=Boeing ui_type=C-17 Globemaster ui_variation=USAF March AFB ui_typerole=Military Jet ui_createdby=Just Flight Ltd description=AI [fltsim.7] title=JFAIC17A_USAF_JACKSON sim=JFAIC17A model= panel= sound= texture=7 atc_id=BLANK atc_flight_number=C17 atc_airline=AIR FORCE atc_parking_codes=C17 atc_parking_types=MIL_CARGO ui_manufacturer=Boeing ui_type=C-17 Globemaster ui_variation=USAF Jackson AFB ui_typerole=Military Jet ui_createdby=Just Flight Ltd description=AI [General] atc_type=C-17 atc_model=C17 editable=0 performance=AI Category=airplane [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [WEIGHT_AND_BALANCE] max_gross_weight = 150000 // (pounds) empty_weight = 44170 // (pounds) reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 20, 0, 0 //-5// 23.9(feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 ;Moments of Inertia empty_weight_pitch_MOI = 3172439 empty_weight_roll_MOI = 2262183 empty_weight_yaw_MOI = 3337024 empty_weight_coupled_MOI = 0 [jet_engine] thrust_scalar = 0.5 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 2.26, -47.17, 4.64 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = 8.57, -25.00, 5.80 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2 = 8.57, 25.00, 5.80 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3 = 2.26, 47.17, 4.64 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1 //Scalar for fuel flow efficiency min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear [TurbineEngineData] fuel_flow_gain = 0.002 //Gain on fuel flow inlet_area = 19.6 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 23500 //Lbs, max rated static thrust at Sea Level afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [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=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) [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 25.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.885 //Brake scalar auto_brakes=4 [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=43.7, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 20 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 1 // degrees flaps-position.2 = 2 // degrees flaps-position.3 = 5 // degrees flaps-position.4 = 10 // degrees flaps-position.5 = 15 // degrees flaps-position.6 = 25 // degrees flaps-position.7 = 30 // degrees flaps-position.8 = 40 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.1] //Inboard Leading Edge Flaps type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 2 // seconds flaps-position.0 = 0 // flaps-position.1 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.2] //Outboard Leading Edge Slat type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 3 // seconds flaps-position.0 = 0 // flaps-position.1 = 0.5 // flaps-position.4 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [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. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [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 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga=1 pitch_takeoff_ga = 8; max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=12.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [fuel] Center1 = 0, 0, 0, 2313, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -3, -19, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -3, 19, 0, 1500, 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 [airplane_geometry] wing_area = 1137.0 //Square feet wing_span = 94.75 //Feet wing_root_chord = 18.0 //Feet wing_dihedral = 6.2 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -0.5 //Degrees oswald_efficiency_factor= 0.75 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 25.0 //Degrees, wing leading edge wing_pos_apex_lon = 8.0 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_area = 338.0 //Square feet htail_span = 41.7 //Feet htail_pos_lon = -35.0 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.0 //Degrees htail_sweep = 30.0 //Degrees, horizontal tail leading edge vtail_area = 224.0 //Square feet vtail_span = 20.0 //Feet, tip to body vtail_sweep = 35.0 //Degrees, vertical tail leading edge vtail_pos_lon = -35.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 5.8 //Feet, vertical distance from reference point, positive going up elevator_area = 70.5 //Square feet aileron_area = 26.9 //Square feet rudder_area = 56.2 //Square feet elevator_up_limit = 22.5 //Degrees elevator_down_limit = 19.5 //Degrees aileron_up_limit = 20.0 //Degrees aileron_down_limit = 20.0 //Degrees rudder_limit = 26.0 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit = 60.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 3 //Aileron to spoileron gain min_ailerons_for_spoilerons = 10 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate auto_spoiler_available=1 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed = 140.0 //Knots True (KTAS) full_flaps_stall_speed = 112.0 //Knots True (KTAS) cruise_speed=506.0 //Knots True (KTAS) max_mach = 0.92 max_indicated_speed = 365.0 //Red line (KIAS) [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [stall_warning] type=2 stick_shaker=1 [contact_points] point.0=1, 59.78, 0.0, -8.13,1181.1, 0, 1.442, 55.92, 0.8, 2.5, 0.9, 4.0, 4.0, 0, 0.0, 0.0 point.1=1, -22.51, -10.06, -8.4, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 0.0, 0.0 point.2=1, -22.51, 10.06, -8.4, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.9, 7.1, 7.1, 3, 0.0, 0.0 point.3=2, -48.33, -65.46, 9.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -48.33, 65.46, 9.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -96.61, 0.00, 9.12, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 25.41, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 max_number_of_points=21 static_pitch=-1.0 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=9.3 //feet, altitude of CG when at rest on the ground gear_system_type=0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -17.74, -82.79, 6.93, fx_navredm , light.1=3, -17.74, 82.79, 6.93, fx_navgrem , light.2=3, -90.00, 0.00, 13.77, fx_navwhih , light.3=2, -17.74, -82.79, 6.93, fx_strobeh , light.4=2, -17.74, 82.79, 6.93, fx_strobeh , light.5=1, 31.53, 0.00, 16.01, fx_beaconh , [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0