[fltsim.0] title=Unitied States Air Force C-17 sim=Boeing C-17 model= panel= sound= texture= kb_checklists=Boeing_C17_check kb_reference=Boeing_C17_ref atc_id=40069 atc_airline=Air Force atc_heavy=1 atc_model=C17 ui_manufacturer=Boeing/MD ui_type=Boeing C17 Globemaster III ui_variation=U.S.A.F description=U.S.A.F Boeing C-17. Design : Owen Hewitt with assistance of Gary Carlson, Jim Goldman & Hiroshi Igami. Textures by Owen Hewitt & C. Vincent Cho. Animation : Mitsushi Yutaka\s Flight Dynamics (c) Steve Small\s Sounds : Default B747. Special thanks to Andrew Cozens - Official Boeing C-17 simulation test pilot.. November 2001 atc_flight_number=173 [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 [flight_tuning] cruise_lift_scalar=1.2 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 [WEIGHT_AND_BALANCE] max_gross_weight=585000 // (pounds) empty_weight=277000 // (pounds) reference_datum_position=0, 0, 0 empty_weight_CG_position=0, 0, 0 max_number_of_stations=50 //default: 45,000 lbs of payload station_load.0=2500, -25.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=10000, -15.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=15000, 0.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=10000, 15.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=2500, 25.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) // for full payload: //station_load.0= 2500, -25.0, 0.0, 0.0 //station_load.1= 10000, -15.0, 0.0, 0.0 //station_load.2=139000, 0.0, 0.0, 0.0 //station_load.3= 10000, 15.0, 0.0, 0.0 //station_load.4= 2500, 25.0, 0.0, 0.0 // for empty aircraft: //station_load.0= 0, -25.0, 0.0, 0.0 /station_load.1= 0, -15.0, 0.0, 0.0 //station_load.2= 0, 0.0, 0.0, 0.0 //station_load.3= 0, 15.0, 0.0, 0.0 //station_load.4= 0, 25.0, 0.0, 0.0 empty_weight_roll_MOI=29500000.000000 empty_weight_pitch_MOI=45000000.000000 empty_weight_yaw_MOI=59500000.000000 empty_weight_coupled_MOI=00000.000000 [ground_reaction] main_gear_damping_ratio=2.0 center_gear_damping_ratio=2.0 [pitot_static] vertical_speed_time_constant=100 [General] atc_type=Boeing atc_model=C17 performance=Cruise : Mach 0.76 at FL350 @ 65%N1. Dimensions (feet) : Span to winglet 169.8\s Length 174\s Height 55.1\s Ceiling 45000 ft\s MTOW 585,000 lbs\s Empty weight 277,000 lbs\s Range @ Payload 40,000 lbs = 4400 nm\s Normal Takeoff @ MTOW = 7740 ft\s STOL \/ tactical Takeoff : considerably less. Usable Fuel 181,054 lbs. Flight Dynamics COPYRIGHT © Steve Smal FSD 11\/2001.. [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 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 max_battery_voltage=28.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=400.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=100.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=98 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8 use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.; default_pitch_mode=0 default_bank_mode=0 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [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 [direction_indicators] direction_indicator.0=3,0 [fuel] LeftMain= 0.000000, -20.000000, 0.000000, 7320.000000, 3.000000 LeftAux= -8.000000, -33.000000, 0.000000, 6191.000000, 3.000000 RightMain=0.000000, 20.000000, 0.000000, 7320.000000, 3.000000 RightAux=-8.000000, 33.000000, 0.000000, 6191.000000, 3.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=3800.000000 wing_span=183.333333 wing_root_chord=30.000000 wing_dihedral=-5.498657 wing_incidence=1.850000 wing_twist=-0.5 oswald_efficiency_factor=0.680000 wing_winglets_flag=1 wing_sweep=25.000000 wing_pos_apex_lon=2.292665 wing_pos_apex_vert=0.000000 htail_area=845.000000 htail_span=72.000000 htail_pos_lon=-95.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=28.000000 vtail_area=1310.000000 vtail_span=26.000000 vtail_sweep=40.000000 vtail_pos_lon=-105.000000 vtail_pos_vert=55.000000 elevator_area=260.000000 aileron_area=222.000000 rudder_area=200.000000 elevator_up_limit=28.000000 elevator_down_limit=28.000000 aileron_up_limit=22.000000 aileron_down_limit=18.000000 rudder_limit=26.500000 elevator_trim_limit=20.000000 spoiler_limit=59.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [Flaps.0] type=1 span-outboard=0.900000 extending-time=20.000000 system_type=0 flaps-position.0=0 // degrees flaps-position.1=10 // degrees flaps-position.2=22 // degrees flaps-position.3=30 // degrees flaps-position.4=42 // degrees damaging-speed=200 // KIAS blowout-speed=250 // KIAS lift_scalar=1.4 drag_scalar=0.9 pitch_scalar=0.0 system_type=1 //Hydraulic [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard=0.7 // 0.0 .. 1.0 extending-time=10 // seconds flaps-position.0=0 // degrees flaps-position.1=1.0 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=1.25 drag_scalar=0.1 pitch_scalar=0.0 system_type=1 //Hydraulic [GeneralEngineData] engine_type=1 Engine.0=-23.333333,-45.750000,0.000000 Engine.1=0.000000,-24.416667,0.000000 Engine.2=0.000000,24.416667,0.000000 Engine.3=-23.333333,45.750000,0.000000 fuel_flow_scalar=2.050 //1.300 min_throttle_limit=-0.500000 [TurbineEngineData] fuel_flow_gain=0.001650 inlet_area=65.500000 rated_N2_rpm=29920.000000 static_thrust=40400.000000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=135.000000 full_flaps_stall_speed=108.000000 cruise_speed=540.000 max_indicated_speed=475.000000 max_mach=0.900000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3,-16.02,-83.1,2.8,fx_navredm, light.1=3,-16.02,83.1,2.8 ,fx_navgrem, light.2=3,-16.02,-83.1,2.79,fx_navredh, light.3=3,-16.02,83.1 ,2.79, fx_navgreh, light.4=2,-25.5,83.2,2.8,fx_strobeh, light.5=2,-25.5,-83.2,2.8 ,fx_strobeh, light.6=2,-16.1,-83.2,2.8,fx_strobeh, light.7=2,-16.1,83.2,2. 8,fx_strobeh, light.8=1,-78.2,0.0,44.05,fx_beaconh, light.9=1,29.3,0.0,-10 .1,fx_beaconh, light.10=1,-78.2,0.0,44.05,fx_beaconh, light.11=1,29.3,0.0, -10.1,fx_beaconh, [Views] eyepoint=63.104905,-1.653236,5.100681 [contact_points] point.0=1.000000,62.916667,0.000000,-13.250000,2360.907127,0.000000,4.393823,75.300000,0.898048,2.500000,2.000000,15.000000,15.000000,0.000000,0.000000,0.000000 point.1=1.000000,-8.333333,-12.416667,-14.833333,3147.876169,1.000000,4.393823,0.000000,2.667645,2.500000,2.000000,15.000000,15.000000,2.000000,0.000000,0.000000 point.2=1.000000,-8.333333,12.416667,-14.833333,3147.876169,2.000000,4.393823,0.000000,2.667645,2.500000,2.000000,15.000000,15.000000,3.000000,0.000000,0.000000 point.3=2.000000,-20.833333,-82.916667,2.083333,1180.453563,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-20.833333,82.916667,2.083333,1180.453563,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-25.166667,0.000000,-8.583333,1180.453563,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,69.083333,0.000000,-4.000000,1180.453563,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.373535 static_cg_height=11.864791 gear_system_type=0 [brakes] toe_brakes_scale=0.976592 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0