[fltsim.0]
title=F-86L SABRE (95th FIS)
sim=F86DRDAF
model=
panel=
sound=
texture=
checklists=
atc_id=AL-T
atc_airline=RDAF
atc_flight_number=16026
ui_manufacturer=North American
ui_type=F-86D Sabre
ui_variation=RDAF F-86D Sabre
editable=0
visual_damage=1

description=Morth American F86\nArtwork by Angelo Moneta 1995\/2000\nvf@intercity.it\nRepaint by Povl Skudstrup


[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


[General]
performance=Royal Danish Air Force \nNorth American F-86D\n maxspeed 1114 km/h\n Lenght 12.47 m\n WingSpan 11.30m\n Weight 8227 kg\n Range 438 km\n ClimpSpeed 61 m/s\n Power GEJ-47-GE-17B


[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=7496.000000
empty_weight_roll_MOI=19118.000000
empty_weight_pitch_MOI=14298.000000
empty_weight_yaw_MOI=27893.000000
empty_weight_coupled_MOI=1300.000000

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.9
aileron_effectiveness=1.0
rudder_effectiveness=0.9
pitch_stability=1.5
roll_stability=1.5
yaw_stability=1.5
elevator_trim_effectiveness=0.5
aileron_trim_effectiveness=0.5
rudder_trim_effectiveness=0.5


[fuel]
LeftMain=0.000000,0.000000,0.000000,180.000000,0.000000
LeftAux=0.000000,-14.750000,0.000000,86.000000,0.000000
RightMain=0.000000,0.000000,0.000000,180.000000,0.000000
RightAux=0.000000,14.750000,0.000000,86.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=215.000000
wing_span=37.083333
wing_root_chord=5.833333
wing_dihedral=3.499146
wing_incidence=-0.494385
wing_twist=-0.999756
oswald_efficiency_factor=1.072141
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=32.000000
htail_span=12.833333
htail_pos_lon=-17.500000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=32.000000
vtail_span=6.449806
vtail_sweep=0.000000
vtail_pos_lon=-18.333333
vtail_pos_vert=5.833333
elevator_area=8.000000
aileron_area=8.600000
rudder_area=5.440000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000,19.166667,0.000000,-6.250000,1574.803150,0.000000,0.576675,43.800000,0.140806,2.500000,0.944761,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,-0.500000,-9.166667,-5.916667,1574.803150,1.000000,0.576675,0.000000,0.196445,2.500000,0.799821,5.000000,5.000000,2.000000,0.000000,0.000000
point.2=1.000000,-0.500000,9.166667,-5.916667,1574.803150,2.000000,0.576675,0.000000,0.196445,2.500000,0.799821,5.000000,5.000000,3.000000,0.000000,0.000000
point.3=2.000000,-1.583333,-15.916667,0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-1.583333,15.916667,0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-27.500000,0.000000,-0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,11.916667,0.000000,-0.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.000000
static_cg_height=5.918128

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=13.330818,0.000000
flaps-position.2=26.661636,0.000000
flaps-position.3=39.992454,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=0.000000,0.000000,0.000000
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=5.655360
rated_N2_rpm=29920.000000
static_thrust=4712.800000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=110.000000
full_flaps_stall_speed=88.000000
cruise_speed=428.687234

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=8.330258,0.000000,7.497232

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
use_no_default_pitch=1 	
use_no_default_bank=1

[direction_indicators]
direction_indicator.0=3,0


[SMOKESYSTEM]
smoke.0=0.00, -20.00, 0.00, fx_smoke_white
smoke.1=0.00, 2.00, 20.00, fx_smoke_red
smoke.2=0.00, 2.00, -20.00, fx_smoke_blue

[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5#
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1#
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000