[fltsim.0]
title=Northrop F-5E Tiger II (RSAF#1)
sim=F5 FDE
model=F-5T_1
panel=
sound=
texture=rsaf
panel_alias=
sound_alias=
kb_checklists=
kb_reference=
atc_id=
atc_id_color = 0xffffffff
atc_parking_types atc_parking_code = 1
atc_airline=Air Force
atc_flight_number=04
ui_manufacturer = Northrop
ui_type = R.S.A.F. F-5T Tiger II
ui_variation = Standard Load
description =© DSB Design 2004\n\nNorthrop-Grumman F-5F Tiger II\nRole: Light Attack Fighter\nCountry of Origin: United States
[fltsim.1]
title=Northrop F-5E Tiger II (RSAF#2)
sim=F5 FDE
model=F-5T_2
panel=
sound=
texture=rsaf
panel_alias=
sound_alias=
kb_checklists=
kb_reference=
atc_id=
atc_id_color = 0xffffffff
atc_parking_types atc_parking_code = 1
atc_airline=Air Force
atc_flight_number=04
ui_manufacturer = Northrop
ui_type = R.S.A.F. F-5T Tiger II
ui_variation = Air Interdiction Load
description =© DSB Design 2004\n\nNorthrop-Grumman F-5F Tiger II\nRole: Light Attack Fighter\nCountry of Origin: United States
[fltsim.2]
title=Northrop F-5E Tiger II (RSAF#3)
sim=F5 FDE
model=F-5T_3
panel=
sound=
texture=rsaf
panel_alias=
sound_alias=
kb_checklists=
kb_reference=
atc_id=
atc_id_color = 0xffffffff
atc_parking_types atc_parking_code = 1
atc_airline=Air Force
atc_flight_number=04
ui_manufacturer = Northrop
ui_type = R.S.A.F. F-5T Tiger II
ui_variation = Ferry Load
description =© DSB Design 2004\n\nNorthrop-Grumman F-5F Tiger II\nRole: Light Attack Fighter\nCountry of Origin: United States
[fltsim.3]
title=Northrop F-5E Tiger II (SWISS#2)
sim=F5 FDE
model=F-5F_1
panel=
sound=
texture=swiss
panel_alias=
sound_alias=
kb_checklists=
kb_reference=
atc_id=
atc_id_color = 0xffffffff
atc_parking_types atc_parking_code = 1
atc_airline=Air Force
atc_flight_number=04
ui_manufacturer = Northrop
ui_type = Swiss Air Force F-5F Tiger II
ui_variation = Standard Load
description =© DSB Design 2004\n\nNorthrop-Grumman F-5F Tiger II\nRole: Light Attack Fighter\nCountry of Origin: United States
[fltsim.4]
title=Northrop F-5E Tiger II (SWISS#3)
sim=F5 FDE
model=F-5F_2
panel=
sound=
texture=swiss
panel_alias=
sound_alias=
kb_checklists=
kb_reference=
atc_id=
atc_id_color = 0xffffffff
atc_parking_types atc_parking_code = 1
atc_airline=Air Force
atc_flight_number=04
ui_manufacturer = Northrop
ui_type = Swiss Air Force F-5F Tiger II
ui_variation = CAP Load
description =© DSB Design 2004\n\nNorthrop-Grumman F-5F Tiger II\nRole: Light Attack Fighter\nCountry of Origin: United States
//--------------------- END OF AIRCRAFT -------------------------
[General]
performance=
atc_type=NORTHRUP
atc_model=F5
---------------------------------------------------------------------------------------------------------
[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=12
station_load.0 = "180.0, 0.0, 15.0, -0.3, left wingtip" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "0.0, 0.0, 11.0, -0.5, left pylon 1" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "0.0, 0.5, 9.0, -0.5, left pylon 2" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "0.0, 0.5, -9.0, -1.0, right pylon 1" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "0.0, 0.5, -11.0, -0.5, right pylon 2" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "180.0, 0.0, -15.0, -0.3, right wingtip" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "200.0, 11.5, 0.0, 2.0, pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "200.0, 8.5, 0.0, 2.0, instructor" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight= 8085.000
empty_weight_roll_MOI= 24000.000
empty_weight_pitch_MOI= 48000.000
empty_weight_yaw_MOI= 25000.000
empty_weight_coupled_MOI= 4000.000
max_gross_weight= 20677.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
----------------------------------------------------------------------------------------------------
[fuel]
Center1= 0.000, 0.000, 0.000, 000.000, 0.000
LeftMain= 0.000, 0.000, 0.000, 250.000, 0.000
LeftAux= 0.000, -5.000, 0.000, 00.000, 0.000
LeftTip= 0.000, -10.000, 0.000, 0.000, 0.000
RightMain= 0.000, 0.000, 0.000, 250.000, 0.000
RightAux= 0.000, 5.000, 0.000, 00.000, 0.000
RightTip= 0.000, 10.000, 0.000, 0.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=3
electric_pump=0
--------------------------------------------------------------------------------------------------------------
[airplane_geometry]
wing_area= 245.000
wing_span= 30.500
wing_root_chord= 7.333
wing_dihedral= 0.000
wing_incidence= -0.494
wing_twist= -1.000
oswald_efficiency_factor= 1.071
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 47.000
htail_span= 14.167
htail_pos_lon= -16.333
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 40.000
vtail_span= 7.211
vtail_sweep= 0.000
vtail_pos_lon= -16.333
vtail_pos_vert= 5.833
elevator_area= 10.000
aileron_area= 6.880
rudder_area= 3.400
elevator_up_limit= 21.064
elevator_down_limit= 15.772
aileron_up_limit= 20.762
aileron_down_limit= 15.762
rudder_limit= 20.918
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
-----------------------------------------------------------------------------------------------------------------------
[contact_points]
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16
point.0= 1.000, 14.670, 0.000, -6.200, 1574.803, 0.000, 0.578, 37.620, 0.300, 1.700, 1.0, 6.300, 6.200, 0.000, 400.000, 0.00
point.1= 1.000, -3.700, -6.500, -6.400, 1574.803, 1.000, 0.578, 0.000, 0.605, 1.200, 1.2, 5.5, 5.600, 2.000, 400.000, 0.000
point.2= 1.000, -3.700, 6.500, -6.400, 1574.803, 2.000, 0.578, 0.000, 0.605, 1.200, 1.2, 5.5, 5.600, 3.000, 400.000, 0.000
point.3= 2.000, -6.417, -16.333, -0.167, 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, -6.417, 16.333, -0.167, 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, -19.750, 0.000, -1.833, 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, 22.667, 0.000, -1.250, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 6.265
gear_system_type=0
--------------------------------------------------------------------------------------------------------
[jet_engine]
thrust_scalar=1.0
-------------------------------------------------------------------------------------------------------
[GeneralEngineData]
engine_type=1
Engine.0=-8.000000,1.000000,0.000000
Engine.1=-8.000000,-1.000000,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=-0.30
-------------------------------------------------------------------------------------------------------
[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=6.247200
rated_N2_rpm=29920.000000
static_thrust=4500.000000
afterburner_available=1
reverser_available=0
-------------------------------------------------------------------------------------------------------
[Reference Speeds]
flaps_up_stall_speed= 79.000
full_flaps_stall_speed= 63.200
cruise_speed= 680.662
max_indicated_speed=850.000000
max_mach=1.400000
------------------------------------------------------------------------------------------------------
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
-------------------------------------------------------------------------------------------------------
[folding_wings]
wing_fold_system_type = 4
fold_rates = 5.0, 5.0
[Views]
//eyepoint= 10, 0, 2.7 - F-5E
eyepoint=13, 0.0, 2.5 - F-5F
----------------------------------------------------------------------------------------------------------
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
----------------------------------------------------------------------------------------------------------------
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -7, -13.3, -1.0, fx_navred
light.1 = 3, -7, 13.3, -1.0, fx_navgre
light.2 = 1, -15.8, 0.01, 7.2, fx_beacon
light.3 = 2, -10, -14.2, 0, fx_Vortices
light.4 = 2, -10, 14.2, 0, fx_Vortices
light.5 = 3, -17.2, -0.0, 7.8, fx_navwhih
light.6= 6, -21.0, 1.0, 3.8, fx_dsb_f5burner
light.7= 6, -21.0, -1.0, 3.8, fx_dsb_f5burner
light.8= 6, -21.0, 1.0, 3.8, fx_dsb_f5burner
light.9= 6, -21.0, -1.0, 3.8, fx_dsb_f5burner
light.10 = 4, 13.0, 0.0, 2.5, fx_dsb_vclight_red
light.11= 5, 12, -5, -9.3, fx_f5_llight
light.12= 5, 12, 5, -9.3, fx_f5_llight
light.13 = 3, 4.8, -3.7, -0.3, fx_navred
light.14 = 3, 4.8, 3.7, -0.3, fx_navgre
light.15 = 4, 8.5, 0.0, 2.7, fx_dsb_vclight_red
light.16= 6, -21.0, 1.0, 3.8, fx_dsb_f5burner
light.17= 6, -21.0, -1.0, 3.8, fx_dsb_f5burner
-------------------------------------------------------------------------------------------------------
[SMOKESYSTEM]
smoke.0 = 0, 5, -0, fx_dsb_hawk_smoke
smoke.1 = 0, -5, -0, fx_dsb_hawk_smoke
-------------------------------------------------------------------------------------------------
[forcefeedback]
stick_shaker_magnitude=15000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1500 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
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
---------------------------------------------------------------------------------------------
[pitot_static]
vertical_speed_time_constant = 100
-----------------------------------------------------------------------------------------------
[autopilot]
autopilot_available=1
flight_director_available= 1
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
--------------------------------------------------------------------------------------------------
[Flaps.0]
type=1
span-outboard=0.500
extending-time=3.000
system_type=1
damaging-speed= 240.000
blowout-speed= 280.000
lift_scalar= 0.350
drag_scalar= 0.450
pitch_scalar= 1.000
flaps-position.0=0.0
flaps-position.1=30.0
flaps-position.2=60.0
flaps-position.3=90.0
flaps-position.4=90.0
[Flaps.1]
type=1
span-outboard=0.500
extending-time=3.000
system_type=1
damaging-speed= 240.000
blowout-speed= 280.000
lift_scalar= 0.350
drag_scalar= 0.450
pitch_scalar= 1.000
flaps-position.0=0.0
flaps-position.1=30.0
flaps-position.2=60.0
flaps-position.3=90.0
flaps-position.4=90.0
[Flaps.2]
type=2
span-outboard=0
extending-time=1
system_type=1
damaging-speed= 0
blowout-speed= 0
lift_scalar= 0
drag_scalar= 1
pitch_scalar= 0
flaps-position.0=0,0
flaps-position.1=0,0
flaps-position.2=0,0
flaps-position.3=0,0
flaps-position.4=600,0
---------------------------------------------------------------------------------------------------------------
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.9
-------------------------------------------------------------------------------------------------------------------------------------------
[electrical]
;BusType, MaxAmpLoad, MinVoltage ;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage=24.0
min_battery_voltage=24.0
max_generator_alternator_amps=400.0
generator_alternator_voltage=28.0
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 20, 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
---------------------------------------------------------------------------------------------------------
[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 = 1.3
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
---------------------------------------------------------------------------------------------------------
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 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
----------------------------------------------------------------------------------------------------------
[gear_warning_system]
gear_warning_available = 0
pct_throttle_limit = 0.1
flap_limit_idle = 30
flap_limit_power = 15
[brakes]
toe_brakes_scale = 0.625
parking_brake = 1
differential_braking_scale = 1.0
[stall_warning]
type = 1
[hydraulic_system]
electric_pumps = 0
engine_map = 1, 0, 0, 0
normal_pressure = 3000
[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=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1 //Turn AND Bank
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup=fx_dsb_heat