----------------------------------F-16 VIPER (By KIRK OLSSON) ----------------------------------

[fltsim.0]
title=F-16 Falcon RDAF E-177
sim=VIPER_NOR
model=
panel=
sound=
texture=e177
checklists=
description=Royal Danish Airforce F-16AM Fighting Falcon E - 177 Featuring Tailart at Aalborg AB 1999, shown at the roll out of the first MLU updated F-16A (E-177)  ---by Kirk Olsson---    \nTexture by Claus Vendelboe Holmberg   [email protected]                                          
ui_manufacturer=Lockheed Martin 
ui_type=F-16 FALCON (RDAF) 
ui_variation=E-177 MLU Roll Out
atc_heavy=0
atc_id=E-177
atc_airline=Air Force
atc_flight_number=
atc_type=LOCKHEED
atc_model=F16
atc_parking_codes=DAF
atc_parking_types=MIL_COMBAT

[fltsim.1]
title=F-16 Falcon RDAF E-199
sim=VIPER_NOR
model=
panel=
sound=
texture=e199
checklists=
description=Royal Danish Airforce F-16A Fighting Falcon E - 199 , Esk 730 Featureing Tailart shown at a Open House event held at Vaerlose AB   ---by Kirk Olsson---    \nTexture by Claus Vendelboe Holmberg   [email protected]                                          
ui_manufacturer=Lockheed Martin 
ui_type=F-16 FALCON (RDAF) 
ui_variation=E-199 Thor's Hammer
atc_heavy=0
atc_id=E-199
atc_airline=Air Force
atc_flight_number=
atc_type=LOCKHEED
atc_model=F16

[fltsim.2]
title=F-16 Falcon RDAF E-180
sim=VIPER_NOR
model=
panel=
sound=
texture=e180
checklists=
description=Royal Danish Airforce F-16A Fighting Falcon E - 180 Featureing Tailart celebrating NATO's 50 years  ---by Kirk Olsson---    \nTexture by Claus Vendelboe Holmberg   [email protected]                                      
ui_manufacturer=Lockheed Martin
ui_type=F-16 FALCON (RDAF) 
ui_variation=E-180 Holger Danske
atc_heavy=0
atc_id=E-180
atc_airline=Air Force
atc_flight_number=
atc_type=LOCKHEED
atc_model=F16

[fltsim.3]
title=F-16 Falcon RDAF E-008
sim=VIPER_NOR
model=
panel=
sound=
texture=e008
checklists=
description= F-16 Fighting Falcon Royal Danish Airforce, ESK730 Featureing Tailart  ---by Kirk Olsson---  \nTexture by Claus Vendelboe Holmberg   [email protected]                                         
ui_manufacturer=Lockheed Martin 
ui_type=F-16 FALCON (RDAF) 
ui_variation=SQN 730 - 50 Year
atc_heavy=0
atc_id=e-008
atc_airline=Air Force
atc_flight_number=
atc_type=LOCKHEED
atc_model=F16

[fltsim.4]
title=F-16 Falcon RDAF E-174
sim=Viper_NOR
model=
panel=
sound=
texture=clean
checklists=
description=The Royal Danish Air Force, signed on to the F-16 early in the NATO history of the aircraft. With an F-16 presence in Denmark, NATO increased its military might significantly in the Baltic Sea. Had conflict erupted during the Cold War years, Danish F-16s were positioned to thwart a massive Soviet fleet from gaining access to the North Sea. In those early years, Denmark operated F-16 Blocks 1 and 5. Blocks 10 and 15 followed later. Since then, Danish F-16s have passed through various modification programs, but none so extensive as the Mid-Life Update. With the MLU, the RDAF takes a major step in capability. \nmodel by Kirk Olsson. \nTexture by Claus Vendelboe Holmberg   [email protected]                                                                                                        
ui_manufacturer=Lockheed Martin
ui_type=F-16 Falcon (RDAF) 
ui_variation=E-174 Clean
atc_heavy=0
atc_id=E-174
atc_airline=Air Force
atc_flight_number=
atc_type=LOCKHEED
atc_model=F16

[fltsim.5]
title=F-16 Falcon RDAF E-195
sim=VIPER_NOR
model=
panel=
sound=
texture=e195
checklists=
description=Royal Danish Airforce F-16AM Fighting Falcon E-195, ESK726 Featureing Tailart    ---by Kirk Olsson---       \nTexture by Claus Vendelboe Holmberg   [email protected]                                       
ui_manufacturer=Lockheed Martin 
ui_type=F-16 FALCON (RDAF) 
ui_variation=E-195 Red tail 
atc_heavy=0
atc_id=E-195
atc_airline=RDAF
atc_flight_number=
atc_type=LOCKHEED
atc_model=F16
--------------------------------------------------





[General]
performance= maximum level speed Mach 2.0 at 12190 m (40,000ft) > service ceiling above 15240 m (50,000 feet) > operational radius 925 km (575 miles) > empty 7070 kg (15,586 lb) > maximum take-off 16,057 kg (35,400 lb)
atc_type=LOCKHEED
atc_model=F16
Category=airplane



---------------------------------------------------------------------------------------------------------
---------------------------------------------------------------------------------------------------------
[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 =   "220.0,  0.0, 15.0,	-0.3, left wingtip"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)        
station_load.1 =   "190.0,  0.0,  13.0,	-0.5, left pylon 1"           //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2 =   "600.0,   0.5,  11.0,	-0.5, left pylon2"               //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3 =  "0.0,  0.5,  9.0,	-1.0, left pylon3"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

station_load.4 =  "00.0,  5.0,  1.0,	-1.5, left lantirn pylon  "         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5 =  "750.0,  3.0,  0.0,	-2.5, center pylon "         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.6 =  "500.0,  5.0,  -1.0,	-1.5, right lantirn pylon "         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

station_load.7 =  "0.0, 0.5,  -9.0,	-1.0, right pylon 4"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.8 =  "600.0, 0.5,  -11.0,	-0.5, right pylon 5"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.9 = "190.0,  0.0,  -13.0,	-0.5, right pylon 6"    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.10 =  "220.0, 0.0,  -15.0,	-0.3, right wingtip"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.11 =  "200.0, 8.5,  0.0,	2.0, pilot"        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

empty_weight= 11000.000
empty_weight_roll_MOI= 40000.000
empty_weight_pitch_MOI= 48000.000
empty_weight_yaw_MOI= 24000.000
empty_weight_coupled_MOI= 4000.000
max_gross_weight= 32211.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
----------------------------------------------------------------------------------------------------
[fuel]
Center1= 0.000, 0.000, 0.000, 150.000, 0.000
LeftMain= 0.000, 0.000, 0.000, 350.000, 0.000
LeftAux= 0.000, -5.000, 0.000, 100.000, 0.000
LeftTip= 0.000, -10.000, 0.000, 0.000, 0.000
RightMain= 0.000, 0.000, 0.000, 350.000, 0.000
RightAux= 0.000, 5.000, 0.000, 100.000, 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= 9.762
aileron_down_limit= 9.762
rudder_limit= 35.918
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
auto_spoiler_available=0
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=29.914530
positive_g_limit_flaps_down=29.914530
negative_g_limit_flaps_up=-29.914530
negative_g_limit_flaps_down=-30.651709
-----------------------------------------------------------------------------------------------------------------------
[contact_points]

            1        2        3         4         5          6         7    8        9         10      
point.0= 1.000,   10.583,   0.000,   -6.180,   1574.803,   0.000,   0.978, 37.620,  0.220,   1.700,   1.0,   6.300,  6.200,  0.000, 400.000, 0.000
point.1= 1.000,   -2.500,  -4.167,   -6.430,    1574.803,  1.000,   1.000, 0.000,   0.605,   1.300,   1.2,   5.5,    5.600,  2.000, 400.000, 0.000
point.2= 1.000,   -2.500,   4.167,   -6.430,   1574.803,   2.000,   1.000, 0.000,   0.605,   1.300,   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= -6.667, 0.000, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit=0.000000

-------------------------------------------------------------------------------------------------------

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 3.617
rated_N2_rpm= 29920.000
static_thrust= 12300.000
afterburner_available= 1
reverser_available= 0
-------------------------------------------------------------------------------------------------------
[Reference Speeds]
flaps_up_stall_speed= 79.000
full_flaps_stall_speed= 63.200
cruise_speed= 622.662
max_indicated_speed=1400.000000
max_mach=2.000000
------------------------------------------------------------------------------------------------------

[Views]
eyepoint=15.4,-0.02000,3.68
VIEW_FORWARD_ZOOM=0.00

----------------------------------------------------------------------------------------------------------
[exits]
number_of_exits=2
exit_rate.0=0.2                               ;Percent per second
----------------------------------------------------------------------------------------------------------------
[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.52,0.22                          ;Percent per second
----------------------------------------------------------------------------------------------------------------
[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

----------------------------------------------------------------------------------------------------------------
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_ktchdwn, 1
-----------------------------------------------------------------------------------------------------------------


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing



light.7=3, 12.2, 2.48,  -1.4, fx_knavgre ,
light.5=3, 12.2, -2.48,  -1.4, fx_knavred ,
light.6=3, -5.9, 16.7,  0.7, fx_knavgre 
light.4=3, -5.9, -16.7,  0.7, fx_knavred 

light.2=3, 12.2, 2.48,  -1.4, fx_kbeacongreen ,
light.1=3, 12.2, -2.48,  -1.4, fx_kbeaconred ,

light.8=5, 15.0, 1.9,  -7.9, fx_kLVIPER ,

light.10=5, 25.0, 1.9,  -5.9, fx_kLVIPER ,


light.11=4, -12.6, 3.4,  1.1, fx_knavwhi ,
light.12=4, -12.6, -3.4,  1.1, fx_knavwhi ,
light.13=4, -14.6, -0.6,  3.1, fx_kLVIPER ,
light.14=4, -14.6, 5.6,  3.1, fx_kLviper ,

light.3=1, -20.217,  0.0,  11.987, fx_kVbeacon ,
light.15= 4,  15.56,   0.00,  3.5, fx_kvclight ,

light.16=3, -21.4, 0.0,  4.5, fx_kbeaconwhite ,

light.20=4, 17.0, 2.9,  -5.9, fx_kLVIPER ,
light.=21=4, 17.0, 2.9,  -5.9, fx_kLVIPER 




light.9=2, -18.2,  0.0, 0.3, fx_f1light.fx
light.xx=2, -20.8,  0.0, 0.3, fx_f1light.fx
light.xx=2, -23.2,  0.0, 0.3, fx_f1light.fx
light.xx=2, -25.2,  0.0, 0.3, fx_f1light.fx

light.xx= 4,  9.5,   0.00,  3.5, fx_kvclight ,

light.17=2, -15.2, 0.0, 0.531,  fx_f1light.fx
light.18=2, -15.2, 0.0, 0.531,  fx_f1lighta.fx
light.19=2, -15.2,  0.0, 0.531, fx_f1light.fx



-------------------------------------------------------------------------------------------------------


[SMOKESYSTEM]
smoke.9=0.0, -5.9, 16.7,   fx_kcontrail.fx
smoke.10= 0.0, -5.9, -16.7,   fx_kcontrail.fx

smoke.0= 50, 1.0, -4.0,   fx_kvapor.fx
smoke.1= 50, 1.0, -6.0,  fx_kvapor.fx   
smoke.2= 50., 1., 4.0, fx_kvapor.fx
smoke.3= 50., 1., 6.0, fx_kvapor.fx

smoke.4= 10., 1., 6.0, fx_kvapor_alt.fx
smoke.5= 10., 1., 7.0, fx_kvapor_alt.fx
smoke.6= 10., 1., -6.0, fx_kvapor_alt.fx
smoke.7= 10., 1., -7.0, fx_kvapor_alt.fx




smoke.8= -50.0, 0.0, 0.0,   fx_kf16exhaust.fx


-------------------------------------------------------------------------------------------------

[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 
pitot_heat=1.000000

-----------------------------------------------------------------------------------------------

[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= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.200
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.996, 0.000
flaps-position.2= 15.996, 0.000
flaps-position.3= 22.992, 0.000

----------------------------------------------------------------------------------------
[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 2.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.700
drag_scalar= 0.100
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 18.000, 0.000
---------------------------------------------------------------------------------------------------------------
[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     = 1.1
parasite_drag_scalar   = 1.63
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.4
aileron_effectiveness  = 1.3
rudder_effectiveness   = 1.0
pitch_stability        = 1.5
roll_stability         = 1.2
yaw_stability          = 1.2
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
----------------------------------------------------------------------------------------------------------
[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
[brakes]
toe_brakes_scale=0.671407
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[General]
performance=0\n\n\n\n\n
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0