[fltsim.0]
title =F-86F Sabre CR1
sim = F-86f
model =
panel =
sound =
texture =cr
kb_checklists=F86F_check
kb_reference=F86F_ref
atc_id=SAAF 607
ui_manufacturer=North American
ui_type="F86F Sabre"
ui_variation="F-86F Sabre 32nd sqn"
description="F-86F 32nd sqn Soesterberg Netherlands 1956"
description=F-86F Sabre\n
visual_damage=1
atc_parking_types=MIL_COMBAT
atc_parking_codes=M001,F86
atc_airline=Mil- F-86 Sabre -Fighter


[fltsim.1]
title =F-86F Sabre CR2
sim = F-86f
model =
panel =
sound =
texture =512
kb_checklists=F86F_check
kb_reference=F86F_ref
atc_id=SAAF 607
ui_manufacturer=North American
ui_type="F86F Sabre"
ui_variation="F-86F Sabre 512th sqn"
description="F-86F 512th sqn Soesterberg Netherlands 1954"
description=F-86F Sabre\n
visual_damage=1
atc_parking_types=MIL_COMBAT
atc_parking_codes=M001,F86
atc_airline=Mil- F-86 Sabre -Fighter

[General]
atc_type =
atc_model =
editable = 1
performance = + Weight: 12049 lbs    Max 20000 lbs + Power: 5910 lbs thrust + 8.0g Corner speed: 362 mph + Max speed @ SL: 688 mph + Max speed: 604 mph @ 35000 ft + Climb rate: 9850 ft/min @ 439 mph Flight Dynamics By: Jerry Beckwith Mudpond Virtual Aircraft FD Build 51 - 12/29/03 12:33 AM Flight Dynamics Workbook V2.84.52

[Views]
eyepoint= 12.05, 0.06,  0.26 


[pitot_static]
vertical_speed_time_constant = 2

[WEIGHT_AND_BALANCE]
max_gross_weight = 20000
empty_weight = 11849

reference_datum_position = 0, 0, 0
empty_weight_CG_position  = 3.5, 0, -2.5
CG_forward_limit = 0
CG_aft_limit = 1

max_number_of_stations = 13
station_load.0 = 200, 10, 0, -1, Pilot
station_load.1 = 0, 0, 0, 0
station_load.2 = 0, 0, 0, 0
station_load.3 = 0, 0, 0, 0
station_load.4 = 0, 0, 0, 0
station_load.5 = 0, 0, 0, 0
station_load.6 = 0, 0, 0, 0
station_load.7 = 0, 0, 0, 0
station_load.8 = 0, 0, 0, 0
station_load.9 = 0, 0, 0, 0
station_load.10 = 0, 0, 0, 0
station_load.11 = 0, 0, 0, 0
station_load.12 = 0, 0, 0, 0

empty_weight_pitch_MOI = 15201
empty_weight_roll_MOI = 7966
empty_weight_yaw_MOI = 19029
empty_weight_coupled_MOI = 0

[flight_tuning]
cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
elevator_effectiveness = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
pitch_stability = 1
roll_stability = 1
yaw_stability = 1
elevator_trim_effectiveness = 1
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1
hi_alpha_on_roll = 1
hi_alpha_on_yaw = 1
p_factor_on_yaw = 1
torque_on_roll = 1
gyro_precession_on_roll = 1
gyro_precession_on_yaw = 1

[GeneralEngineData]
engine_type = 1
Engine.0 = -9, 0, -3
fuel_flow_scalar = 1
min_throttle_limit = 0

[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 1.74697014484186
rated_N2_rpm = 7950
static_thrust = 5910
afterburner_available = 0
reverser_available = 0

[jet_engine]
thrust_scalar = 1

[folding_wings]
wing_fold_system_type =  4
fold_rates =  0.12, 0.11

[TailHook]
tailhook_length = 4
tailhook_position = -15, 0, -1
cable_force_adjust = 1

[contact_points]
max_number_of_points = 12
point.0 = 1, 16.35, 0,    -8.11, 3000, 0, 1, 30, 0.075, 2.5, 1.5, 5, 5, 0, 330, 352
point.1 = 1,  2.8, -4.2,  -8.35, 2600, 1, 1,  0, 0.36,  2.5, 0.9, 5, 5, 2, 330, 352
point.2 = 1,  2.8,  4.2,  -8.35, 2600, 2, 1,  0, 0.36,  2.5, 0.9, 5, 5, 3, 330, 352
//point.3 = 2, -4.5,-18.8,  -3.8,  1574, 0, 0,  0, 0,     0,   0,   0, 0, 5
//point.4 = 2, -4.5, 18.8,  -3.8,  1574, 0, 0,  0, 0,     0,   0,   0, 0, 6
//point.5 = 2,-15.4,  0,    -3,    1574, 0, 0,  0, 0,     0,   0,   0, 0, 9
//point.6 = 2, 18.8,  0,    -2.08, 1574, 0, 0,  0, 0,     0,   0,   0, 0, 4
//point.7 = 2,-18.2,  0,     6.5,   700, 0, 0,  0, 0,     0,   0,   0, 0, 9
//point.8 = 2,  3.8,  0,    -5.5,  3750, 0, 0,  0, 0,     0,   0,   0, 0, 4
//point.9 = 2,-17.3,  0,    -1,    3100, 0, 0,  0, 0,     0,   0,   0, 0, 4
//point.10 = 2,-5.5, -9.25, -6.4,  2000, 0, 0,  0, 0,     0,   0,   0, 0, 5
//point.11 = 2,-5.5,  9.25, -6.4,  2000, 0, 0,  0, 0,     0,   0,   0, 0, 6

point.3 = 2,  -4.56, 18.65, -3.80,  150, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0, 0, 5, 0,   0
point.4 = 2,  -4.56,-18.65, -3.80,  150, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0, 0, 6, 0,   0
point.5 = 2, -16.85,  0.00,  6.75,  250, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0, 0, 9, 0,   0
point.6 = 2,  18.61, -0.00, -2.00,  150, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0, 0, 4, 0,   0
point.7 = 2, -15.30,  0.00, -3.00,  250, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0, 0, 9, 0,   0
point.8 = 2,  17.80, -0.00, -4.30,  150, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0, 0, 4, 0,   0
point.9 = 2, -17.20,  0.00, -1.00,  250, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0, 0, 4, 0,   0
point.10 = 2,  1.42, -9.16, -6.70,  250, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0, 0, 5, 0,   0
point.11 = 2,  1.42,  9.16, -6.70,  250, 0, 0.00,  0.0, 0.00, 0.0, 0.0, 0, 0, 6, 0,   0


static_pitch= 0
static_cg_height= 7.9
gear_system_type = 1


[flaps.0]       //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 = 11, 361
flaps-position.2 = 22, 345
flaps-position.3 = 33, 329
flaps-position.4 = 45, 314
damaging-speed = 361
blowout-speed = 392
system_type = 1
lift_scalar = 0
drag_scalar = 0
pitch_scalar = 1

[flaps.1]       //Leading Edge Flaps - Lift
type = 2
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 = 15
flaps-position.2 = 30
flaps-position.3 = 45
flaps-position.4 = 30
damaging-speed = 361
blowout-speed = 392
system_type = 1
lift_scalar = 1
drag_scalar = 0
pitch_scalar = 0

[flaps.2]       //Leading Edge Flaps - Drag
type = 2
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 = 4
flaps-position.2 = 5
flaps-position.3 = 6
flaps-position.4 = 45
damaging-speed = 361
blowout-speed = 392
system_type = 1
lift_scalar = 0
drag_scalar = 1
pitch_scalar = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
electric_always_available = 1

flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17

[LIGHTS]
light.0 = 3,   -4.56, -18.64,  -3.80, fx_navred ,
light.1 = 3,   -4.56,  18.61,  -3.80, fx_navgre ,
light.2 = 3,  -16.85,   0.00,   6.75, fx_navwhi ,
light.3 = 2,   -4.69, -18.64,  -3.80, fx_strobe ,
light.4 = 2,   -4.69,  18.61,  -3.80, fx_strobe ,
light.5 = 1,  -16.75,   0.00,   6.75, fx_beacon ,
light.6 = 2,   -0.55,   0.00,  -5.10, fx_strobe ,
light.7 = 4,   14.5,    0.00,  -1.60, fx_vclight,
light.8=6, -11.2,  0.0, 1.47, fx_efaburner,
light.9=6, -22.2,  0.0, 0.97, efall.fx,


// Contact Point Location Testing Lights for F-86
//light.0 = 3, 16.35, 0,    -8.11, fx_navgre , // nlg
//light.1 = 3,  2.8, -4.2,  -8.35, fx_navgre , // lt mlg
//light.2 = 3,  2.8,  4.2,  -8.35, fx_navgre , // rt mlg
//light.3 = 3, -4.56, 18.65, -3.80, fx_navred , // rt wingtip
//light.4 = 3, -4.56,-18.65, -3.80, fx_navred , // lt wingtip
//light.5 = 3,-16.85,  0.00,  6.75, fx_navred , // v stab
//light.6 = 3, 18.61, -0.00, -2.00, fx_navred , // inlet high
//light.7 = 3,-15.30,  0.00, -3.00, fx_navred , // exh low
//light.8 = 3,  1.42, -9.16, -6.70, fx_navred , // lt ext tank
//light.9 = 3,  1.42,  9.16, -6.70, fx_navred , // rt ext tank
//light.10= 3, 17.80, -0.00, -4.30, fx_navred , // inlet low
//light.11= 3,-17.20,  0.00, -1.00, fx_navred , // exh high


[SMOKESYSTEM] // (feet) vertical, longitudinal, lateral,
smoke.1= -4.47,  -4.89,  -18.61, fx_contrail_320  // fore/aft, up/dwn/ prt/strbrd
smoke.2= -4.47,  -4.89,   18.61, fx_contrail_320
smoke.3= -3.47,  -20.47,   0.0, fx_f4eng_exhaust_gry  // engine 

[keyboard_response]
elevator = 350, 500
aileron  = 450, 1000
rudder   = 200, 1000

[direction_indicators]
direction_indicator.0 = 1, 0

[exits]
number_of_exits = 1
exit_rate.0 = 0.4

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

[autopilot]
autopilot_available = 1
flight_director_available = 0
default_vertical_speed = 1000
autothrottle_available = 0
autothrottle_arming_required = 0
autothrottle_max_rpm =  90
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8
max_pitch_velocity_hi_alt = 1.5
max_pitch_velocity_lo_alt_breakpoint = 20000
max_pitch_velocity_hi_alt_breakpoint = 28000
max_pitch = 10
max_pitch_acceleration = 1
max_pitch_velocity_lo_alt = 2
max_bank= 25
max_bank_acceleration = 1.8
max_bank_velocity = 3
max_throttle_rate = 0.1
nav_proportional_control = 9
nav_integrator_control = 0.25
nav_derivative_control = 0
nav_integrator_boundary = 2.5
nav_derivative_boundary = 0
gs_proportional_control = 9.52
gs_integrator_control = 0.26
gs_derivative_control = 0
gs_integrator_boundary = 0.7
gs_derivative_boundary = 0
yaw_damper_gain = 0

[fuel]
Center1 = 3.5, 0, -0.5, 505,  0
fuel_type =  2
number_of_tank_selectors = 1
electric_pump=0

[airplane_geometry]
wing_area = 287.9
wing_span = 37.12
wing_root_chord = 7.75592672413793
wing_dihedral = 6.2
wing_incidence = 0
wing_twist = 0
oswald_efficiency_factor = 0.895869052794581
wing_winglets_flag = 0
wing_sweep  = 0
wing_pos_apex_lon = 5.54898168103448
wing_pos_apex_vert = -2.5
htail_area = 35.9
htail_span = 14.9
htail_pos_lon = -22.4
htail_pos_vert = 0
htail_incidence = 0
htail_sweep = 0
vtail_area = 21.3
vtail_span = 6.9
vtail_sweep = 0
vtail_pos_lon  = -22.9
vtail_pos_vert = 0
elevator_area = 19.9
aileron_area = 20.7
rudder_area = 13.6
elevator_up_limit = 30
elevator_down_limit = 20
aileron_up_limit = 15
aileron_down_limit = 15
rudder_limit = 30
elevator_trim_limit = 18
spoiler_limit = 30
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0

[Reference Speeds]
flaps_up_stall_speed    = 122.5
full_flaps_stall_speed  = 93
cruise_speed            = 348
max_indicated_speed = 652
max_mach = 0.9857

[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
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[gear_warning_system]
gear_warning_available = 0
pct_throttle_limit = 0.1
flap_limit_idle = 33.75
flap_limit_power = 16.875

[brakes]
toe_brakes_scale = 0.640888698995941
parking_brake = 1

[stall_warning]
type = 1

[hydraulic_system]
electric_pumps = 0
engine_map = 1, 0, 0, 0
normal_pressure = 1250

[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0