title=BoeX32
sim=BoeX32
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=Boeing
ui_type=X32
ui_variation=
description=FS2004\/FSX Boeing X-32\nby JRLucariny\nhttp:\/\/www.jrlucariny.com
atc_heavy=0
atc_id=
atc_airline=FAB
atc_flight_number=
ui_type=X32
ui_variation=
description=FS2004\/FSX Boeing X-32\nby JRLucariny\nhttp:\/\/www.jrlucariny.com
atc_heavy=0
atc_id=
atc_airline=FAB
atc_flight_number=
[General]
performance=Crew: 1 \nLength: 50.77 ft (15.47 m) \nWingspan: 36 ft (10.97 m) \nHeight: (5.28 m) \nWing area: 590 ft² (54.8 m²) \nMax takeoff weight: 38,000 lb (17,200 kg) \nPowerplant: 1× Pratt & Whitney F135 afterburning turbofan \nDry thrust: ~26,000 lbf (117 kN) \nThrust with afterburner: 35,000+ lbf (155.7+ kN) \nMaximum speed: Mach 1.6 (1,200 mph, 1,931 km\/h) at altitude \nRange on USAF mission profile: 850 NM (1,575 km) \nRange on United States Navy mission profile: 750 NM (1,390 km) \nRange on USMC\/RN mission profile: 594 NM (1,100 km)\n20 mm M61A2 cannon, or 27 mm Mauser BK-27 cannon \nInternal: 6 AMRAAM AAMs or 2 AMRAAM AAMs and 2 x 2,000 lb (900 kg) class guided bombs \nExternal: Approx. 15,000 lb (6,800 kg) of full range of external stores including guided weapons, anti-radiation missile, air-to-surface weapons, auxiliary fuel tanks
atc_type=BOEING AIRCRAFT
atc_model=BoeX32
performance=Crew: 1 \nLength: 50.77 ft (15.47 m) \nWingspan: 36 ft (10.97 m) \nHeight: (5.28 m) \nWing area: 590 ft² (54.8 m²) \nMax takeoff weight: 38,000 lb (17,200 kg) \nPowerplant: 1× Pratt & Whitney F135 afterburning turbofan \nDry thrust: ~26,000 lbf (117 kN) \nThrust with afterburner: 35,000+ lbf (155.7+ kN) \nMaximum speed: Mach 1.6 (1,200 mph, 1,931 km\/h) at altitude \nRange on USAF mission profile: 850 NM (1,575 km) \nRange on United States Navy mission profile: 750 NM (1,390 km) \nRange on USMC\/RN mission profile: 594 NM (1,100 km)\n20 mm M61A2 cannon, or 27 mm Mauser BK-27 cannon \nInternal: 6 AMRAAM AAMs or 2 AMRAAM AAMs and 2 x 2,000 lb (900 kg) class guided bombs \nExternal: Approx. 15,000 lb (6,800 kg) of full range of external stores including guided weapons, anti-radiation missile, air-to-surface weapons, auxiliary fuel tanks
atc_type=BOEING AIRCRAFT
atc_model=BoeX32
[WEIGHT_AND_BALANCE]
reference_datum_position=0,0,0
empty_weight_CG_position=0,0,0
max_number_of_stations=50
//Stayion-load-number = load, longitudinal, lateral, vertical, name
station_load.0= 300, 10, 0, 2, Pilot
station_load.1= 0, -5, -30, -6, LeftWing
station_load.2= 0, -5, 30, - 6, RightWing
empty_weight=15000
empty_weight_roll_MOI=135000
empty_weight_pitch_MOI=262662
empty_weight_yaw_MOI=373480
empty_weight_coupled_MOI=1300
max_gross_weight=31000 //Max weight for VTOL/Hover operation: 21000 lbs
reference_datum_position=0,0,0
empty_weight_CG_position=0,0,0
max_number_of_stations=50
//Stayion-load-number = load, longitudinal, lateral, vertical, name
station_load.0= 300, 10, 0, 2, Pilot
station_load.1= 0, -5, -30, -6, LeftWing
station_load.2= 0, -5, 30, - 6, RightWing
empty_weight=15000
empty_weight_roll_MOI=135000
empty_weight_pitch_MOI=262662
empty_weight_yaw_MOI=373480
empty_weight_coupled_MOI=1300
max_gross_weight=31000 //Max weight for VTOL/Hover operation: 21000 lbs
[contact_points]
point.0= 1.000, 13.700, 0.000, -9.500, 22252.774, 0.000, 0.676, 39.720, 0.313, 2.500, 1.996, 7.000, 7.000, 0.000, 0.000, 0.000
point.1= 1.000, -5.250, -8.150, -8.250, 22252.774, 1.000, 0.676, 0.000, 0.499, 2.500, 0.623, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -5.250, 8.150, -8.250, 22252.774, 2.000, 0.676, 0.000, 0.499, 2.500, 0.623, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -2.583, -33.583, 0.833, 21574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -2.583, 33.583, 0.833, 21574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -19.167, 0.000, 4.750, 21574.803, 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, 13.583, 0.000, -1.917, 2163.065, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=3.000
static_cg_height=8.6000
gear_system_type=0
point.0= 1.000, 13.700, 0.000, -9.500, 22252.774, 0.000, 0.676, 39.720, 0.313, 2.500, 1.996, 7.000, 7.000, 0.000, 0.000, 0.000
point.1= 1.000, -5.250, -8.150, -8.250, 22252.774, 1.000, 0.676, 0.000, 0.499, 2.500, 0.623, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -5.250, 8.150, -8.250, 22252.774, 2.000, 0.676, 0.000, 0.499, 2.500, 0.623, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -2.583, -33.583, 0.833, 21574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -2.583, 33.583, 0.833, 21574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -19.167, 0.000, 4.750, 21574.803, 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, 13.583, 0.000, -1.917, 2163.065, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=3.000
static_cg_height=8.6000
gear_system_type=0
static_pitch = 6.235
static_cg_height = 5.4
gear_system_type=0
static_cg_height = 5.4
gear_system_type=0
[fuel]
// VTOL is ONLY possible when the max. VTOL-operation weight (21000 lbs) is not exceeded.
// Given empty weight and payload, this means max. 800 gal. of fuel !!
Center1= 0, 0, 0,400,0
LeftMain= 0, -5, 0,200,0
RightMain=0, 5, 0,200,0
External1=0,-30,-3,300,0
External2=0, 30,-3,300,0
fuel_type=2
number_of_tank_selectors=1
electric_pump=0
// VTOL is ONLY possible when the max. VTOL-operation weight (21000 lbs) is not exceeded.
// Given empty weight and payload, this means max. 800 gal. of fuel !!
Center1= 0, 0, 0,400,0
LeftMain= 0, -5, 0,200,0
RightMain=0, 5, 0,200,0
External1=0,-30,-3,300,0
External2=0, 30,-3,300,0
fuel_type=2
number_of_tank_selectors=1
electric_pump=0
[TailHook]
tailhook_length=8 ;(feet)
tailhook_position=-3.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0
tailhook_length=8 ;(feet)
tailhook_position=-3.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.12,0.11 ;Percent per second
wing_fold_system_type = 4 ;0=None
fold_rates = 0.12,0.11 ;Percent per second
[exits]
number_of_exits=1
exit_rate.0=1.0 ;Percent per second
number_of_exits=1
exit_rate.0=1.0 ;Percent per second
[ELECTRICAL]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=50.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 0.0
gear_motor=0, 5 , 0.0
autopilot=0, 5 , 0.0
avionics_bus=0, 10, 0.0
avionics=1, 5 , 0.0
pitot_heat=0, 2 , 0.0
additional_system=0, 20, 0.0
marker_beacon=1, 2 , 0.0
gear_warning=0, 2 , 0.0
fuel_pump=0, 5 , 0.0
starter1=0, 20, 0.0
light_nav=0, 5 , 0.0
light_beacon=0, 5 , 0.0
light_landing=0, 5 , 0.0
light_taxi=0, 5 , 0.0
light_strobe=0, 5 , 0.0
light_panel=0, 5 , 0.0
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=50.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 0.0
gear_motor=0, 5 , 0.0
autopilot=0, 5 , 0.0
avionics_bus=0, 10, 0.0
avionics=1, 5 , 0.0
pitot_heat=0, 2 , 0.0
additional_system=0, 20, 0.0
marker_beacon=1, 2 , 0.0
gear_warning=0, 2 , 0.0
fuel_pump=0, 5 , 0.0
starter1=0, 20, 0.0
light_nav=0, 5 , 0.0
light_beacon=0, 5 , 0.0
light_landing=0, 5 , 0.0
light_taxi=0, 5 , 0.0
light_strobe=0, 5 , 0.0
light_panel=0, 5 , 0.0
[LSO]
LSOAdjustSpeed=0.7
LSOAdjustSpeed=0.7
[forcefeedback]
gear_bump_nose_magnitude=3000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=3000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=3000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=950
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=550
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
gear_bump_nose_magnitude=3000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=3000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=3000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=950
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=550
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
[contact_points]
point.0= 1.000, 13.700, 0.000, -9.500, 2252.774, 0.000, 0.676, 39.720, 0.313, 2.500, 1.996, 7.000, 7.000, 0.000, 0.000, 0.000
point.1= 1.000, -5.250, -8.150, -8.250, 2252.774, 1.000, 0.676, 0.000, 0.499, 2.500, 0.623, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -5.250, 8.150, -8.250, 2252.774, 2.000, 0.676, 0.000, 0.499, 2.500, 0.623, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -2.583, -33.583, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -2.583, 33.583, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -19.167, 0.000, 4.750, 1574.803, 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, 13.583, 0.000, -1.917, 163.065, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=3.000
static_cg_height=8.6000
gear_system_type=0
point.0= 1.000, 13.700, 0.000, -9.500, 2252.774, 0.000, 0.676, 39.720, 0.313, 2.500, 1.996, 7.000, 7.000, 0.000, 0.000, 0.000
point.1= 1.000, -5.250, -8.150, -8.250, 2252.774, 1.000, 0.676, 0.000, 0.499, 2.500, 0.623, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -5.250, 8.150, -8.250, 2252.774, 2.000, 0.676, 0.000, 0.499, 2.500, 0.623, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -2.583, -33.583, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -2.583, 33.583, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -19.167, 0.000, 4.750, 1574.803, 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, 13.583, 0.000, -1.917, 163.065, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=3.000
static_cg_height=8.6000
gear_system_type=0
[Lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=4, 15.20, 0.00, 3.30, fx_vclight,
light.1=2, -19.54, 6.80, 7.40, fx_strobe,
light.2=2, -19.54, -6.80, 7.40, fx_strobe,
light.3=1, -3.69, 0.00, 2.40, fx_beacon ,
light.4=1, -3.77, 0.00, -4.90, fx_beacon ,
light.1=2, -19.54, 6.80, 7.40, fx_strobe,
light.2=2, -19.54, -6.80, 7.40, fx_strobe,
light.3=1, -3.69, 0.00, 2.40, fx_beacon ,
light.4=1, -3.77, 0.00, -4.90, fx_beacon ,
light.5= 5, -16.50,-17.80, -1.25, fx_contrail_s , // Left Wingtip contrail, when Gforce > 2
light.6= 5, -16.50, 17.80, -1.25, fx_contrail_s , // Right Wingtip contrail, when Gforce > 2
light.6= 5, -16.50, 17.80, -1.25, fx_contrail_s , // Right Wingtip contrail, when Gforce > 2
light.7= 4, -4.90, -14.00, -1.65, fx_smoke_y,
light.8= 4, -4.90, 14.00, -1.65, fx_smoke_b,
light.8= 4, -4.90, 14.00, -1.65, fx_smoke_b,
//afterburner effects
light.9= 6, -16.55, 0.00, -0.63, fx_afterburner_f3 , // Eng1 Afterburner Burn1
light.10= 6, -17.00, 0.00, -0.63, fx_F14_Burnerflame , // Eng1 Afterburner Flame
light.9= 6, -16.55, 0.00, -0.63, fx_afterburner_f3 , // Eng1 Afterburner Burn1
light.10= 6, -17.00, 0.00, -0.63, fx_F14_Burnerflame , // Eng1 Afterburner Flame
[SmokeSystem]
smoke.0= 0.00, -18.00, 0.00, fx_smoke_f6
smoke.1= 0.00, -18.00, 0.00, fx_smoke_f6
smoke.0= 0.00, -18.00, 0.00, fx_smoke_f6
smoke.1= 0.00, -18.00, 0.00, fx_smoke_f6
[fuel]
Center1= 0.00, 0.00, 0.00, 400.00,0.00
LeftMain= -0.500,-3.00,-0.200,500.00,0.00
RightMain=-0.500, 3.00,-0.200,500.00,0.00
fuel_type=2
number_of_tank_selectors=1
electric_pump=0
Center1= 0.00, 0.00, 0.00, 400.00,0.00
LeftMain= -0.500,-3.00,-0.200,500.00,0.00
RightMain=-0.500, 3.00,-0.200,500.00,0.00
fuel_type=2
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=260.00
wing_span=27.500
wing_root_chord=9.416667
wing_dihedral=2.999268
wing_incidence=0.00
wing_twist=1.093140
oswald_efficiency_factor=0.78830
wing_winglets_flag=0
wing_sweep=0.00
wing_pos_apex_lon=0.019170
wing_pos_apex_vert=0.00
htail_area=49.000000
htail_span=11.333333
htail_pos_lon=-18.00
htail_pos_vert=0.00
htail_incidence=-0.1
htail_sweep=0.00
vtail_area=50.00
vtail_span=8.062258
vtail_sweep=30.000000
vtail_pos_lon=-18.00
vtail_pos_vert=8.333333
elevator_area=56.3900
aileron_area=19.9400
rudder_area=15.0400
elevator_up_limit=31.730403
elevator_down_limit=31.730403
aileron_up_limit=31.718944
aileron_down_limit=12.811336
rudder_limit=30.000070
elevator_trim_limit=31.512679
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.00
min_ailerons_for_spoilerons=0.00
min_flaps_for_spoilerons=0.00
wing_area=260.00
wing_span=27.500
wing_root_chord=9.416667
wing_dihedral=2.999268
wing_incidence=0.00
wing_twist=1.093140
oswald_efficiency_factor=0.78830
wing_winglets_flag=0
wing_sweep=0.00
wing_pos_apex_lon=0.019170
wing_pos_apex_vert=0.00
htail_area=49.000000
htail_span=11.333333
htail_pos_lon=-18.00
htail_pos_vert=0.00
htail_incidence=-0.1
htail_sweep=0.00
vtail_area=50.00
vtail_span=8.062258
vtail_sweep=30.000000
vtail_pos_lon=-18.00
vtail_pos_vert=8.333333
elevator_area=56.3900
aileron_area=19.9400
rudder_area=15.0400
elevator_up_limit=31.730403
elevator_down_limit=31.730403
aileron_up_limit=31.718944
aileron_down_limit=12.811336
rudder_limit=30.000070
elevator_trim_limit=31.512679
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.00
min_ailerons_for_spoilerons=0.00
min_flaps_for_spoilerons=0.00
[Flaps.0] // Animation only
type=1
span-outboard=0.5
extending-time=10
system_type=0
damaging-speed=0
blowout-speed=0
lift_scalar=0
drag_scalar=0
pitch_scalar=0
flaps-position.0=0 //Flaps 0 degrees, Nozzles 0 degrees
flaps-position.1=10 //Flaps 10 degrees, Nozzles 0 degrees
flaps-position.2=20 //Flaps 20 degrees, Nozzles 0 degrees
flaps-position.3=40 //Flaps 40 degrees, Nozzles 0 degrees
flaps-position.4=55 //Flaps 40 degrees, Nozzles 50 degrees
flaps-position.5=80 //Flaps 40 degrees, Nozzles 82 degrees
flaps-position.6=85 //Flaps 40 degrees, Nozzles 86 degrees
flaps-position.7=90 //Flaps 40 degrees, Nozzles 90 degrees
flaps-position.8=95 //Flaps 40 degrees, Nozzles 94 degrees
flaps-position.9=100 //Flaps 40 degrees, Nozzles 98 degrees
type=1
span-outboard=0.5
extending-time=10
system_type=0
damaging-speed=0
blowout-speed=0
lift_scalar=0
drag_scalar=0
pitch_scalar=0
flaps-position.0=0 //Flaps 0 degrees, Nozzles 0 degrees
flaps-position.1=10 //Flaps 10 degrees, Nozzles 0 degrees
flaps-position.2=20 //Flaps 20 degrees, Nozzles 0 degrees
flaps-position.3=40 //Flaps 40 degrees, Nozzles 0 degrees
flaps-position.4=55 //Flaps 40 degrees, Nozzles 50 degrees
flaps-position.5=80 //Flaps 40 degrees, Nozzles 82 degrees
flaps-position.6=85 //Flaps 40 degrees, Nozzles 86 degrees
flaps-position.7=90 //Flaps 40 degrees, Nozzles 90 degrees
flaps-position.8=95 //Flaps 40 degrees, Nozzles 94 degrees
flaps-position.9=100 //Flaps 40 degrees, Nozzles 98 degrees
[Flaps.1] // Drag/Lift modelling
type= 2
span-outboard= 0
extending-time= 5
system_type= 0
damaging-speed= 250
blowout-speed= 300
lift_scalar= 1
drag_scalar= 1
pitch_scalar= 1
flaps-position.0= 0
flaps-position.1= 10
flaps-position.2= 20
flaps-position.3= 40
flaps-position.4= 150 // Nozzles 50 (high drag/lift)
flaps-position.5= 150
flaps-position.6= 150
flaps-position.7= 150
flaps-position.8= 150
flaps-position.9= 150
type= 2
span-outboard= 0
extending-time= 5
system_type= 0
damaging-speed= 250
blowout-speed= 300
lift_scalar= 1
drag_scalar= 1
pitch_scalar= 1
flaps-position.0= 0
flaps-position.1= 10
flaps-position.2= 20
flaps-position.3= 40
flaps-position.4= 150 // Nozzles 50 (high drag/lift)
flaps-position.5= 150
flaps-position.6= 150
flaps-position.7= 150
flaps-position.8= 150
flaps-position.9= 150
[GeneralEngineData]
engine_type=1
Engine.0=-3.00,0.00,0.00
fuel_flow_scalar=1.00
min_throttle_limit=0.00
engine_type=1
Engine.0=-3.00,0.00,0.00
fuel_flow_scalar=1.00
min_throttle_limit=0.00
[TurbineEngineData]
fuel_flow_gain=0.002500
inlet_area=6.500
rated_N2_rpm=29920.00
static_thrust=11200.00
afterburner_available=0
reverser_available=0
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
fuel_flow_gain=0.002500
inlet_area=6.500
rated_N2_rpm=29920.00
static_thrust=11200.00
afterburner_available=0
reverser_available=0
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
[Reference Speeds]
flaps_up_stall_speed=125.00
full_flaps_stall_speed=100.00
cruise_speed=513.055208
max_indicated_speed=745.00
max_mach=1.200
flaps_up_stall_speed=125.00
full_flaps_stall_speed=100.00
cruise_speed=513.055208
max_indicated_speed=745.00
max_mach=1.200
[keyboard_response]
elevator=150.00,250.00
aileron=150.00,250.00
rudder=150.00,250.00
elevator=150.00,250.00
aileron=150.00,250.00
rudder=150.00,250.00
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
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
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
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
[direction_indicators]
direction_indicator.0=3,0
direction_indicator.0=3,0
[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
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
[brakes]
toe_brakes_scale=3
parking_brake=2
toe_brakes_scale=3
parking_brake=2
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
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=1,0,0,0
normal_pressure=3000.000000
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
type=1
[attitude_indicators]
attitude_indicator.0=1
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
turn_indicator.0=1,0
[Views]
eyepoint=12.30,0.0, 2.78
eyepoint=12.30,0.0, 2.78
[Effects]
concrete=fx_sparks
contrail=fx_RCB_Contrail
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
touchdown=fx_tchdwn_s, 1
concrete=fx_sparks
contrail=fx_RCB_Contrail
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
touchdown=fx_tchdwn_s, 1
[tailhook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=1.0
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=1.0
