[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=00181
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