///*** CFG FILE/claudio sanchez
_____________________________________________________________________________
[fltsim.0]
title=North American F-86F-30 fav2
sim=f86f30
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=9477
ui_manufacturer=North American
ui_type=F-86F-30 Sabre
ui_variation=FAV9477
description=Veintidós (22) de estos cazas fueron adquiridos en 1955, para reemplazar a los P-47D Thunderbolt del Escuadrón de Caza C-36 Los Diablos y bautizados a su llegada como los Jaguares del C-36. Comenzando así una época de gloria en la aviación de caza, para el momento la más moderna y mejor equipada de Latinoamérica. El 24 de noviembre de 1955 el comandante del escuadrón el Tcnel. Juan A. Delgado, rompe por primera vez la barrera del sonido sobre los cielos aragueños, el 10 de Diciembre del mismo año lo hace oficialmente. Posteriormente los Sabre conforman el equipo acrobático Los Jaguares de la FAV, entre 1961 a 1969 siempre operando desde la base aérea El Libertador en Palo Negro. En 1972 fueron transferidos a la base Tte. Vicente Landaeta Gil en Barquisimeto. Finalizando su operación en 1975, cuando aún los disponibles fueron vendidos a la Fuerza Aérea Boliviana. visita -->> www.fav-club.com
[fltsim.1]
title=North American F-86F-30 fav1
sim=f86f30
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=9479
ui_manufacturer=North American
ui_type=F-86F-30 Sabre
ui_variation=FAV9479
description= Veintidós (22) de estos cazas fueron adquiridos en 1955, para reemplazar a los P-47D Thunderbolt del Escuadrón de Caza C-36 Los Diablos y bautizados a su llegada como los Jaguares del C-36. Comenzando así una época de gloria en la aviación de caza, para el momento la más moderna y mejor equipada de Latinoamérica. El 24 de noviembre de 1955 el comandante del escuadrón el Tcnel. Juan A. Delgado, rompe por primera vez la barrera del sonido sobre los cielos aragueños, el 10 de Diciembre del mismo año lo hace oficialmente. Posteriormente los Sabre conforman el equipo acrobático Los Jaguares de la FAV, entre 1961 a 1969 siempre operando desde la base aérea El Libertador en Palo Negro. En 1972 fueron transferidos a la base Tte. Vicente Landaeta Gil en Barquisimeto. Finalizando su operación en 1975, cuando aún los disponibles fueron vendidos a la Fuerza Aérea Boliviana. visita -->> www.fav-club.com
___________________________________________________________________________________
[General]
atc_type=F86
atc_model=F86
editable=0
performance=fabricante:North American (USA)_LONGITUD:11,45 m._ENVERGADURA:11,3 m._ALTURA:4,27 m._PLANTA MOTRIZ:General Electric J47-GE-27 de 5.790 lbs de empuje._VELOCIDAD:MÁXIMA: 1.072 km/h._PESOS:VACÍO: 1.823 Kg._MÁXIMO DESPEGUE: 2.381 Kg._TECHO:16.170 m._ALCANCE:2.000 km._ARMAMENTO:6 ametralladoras de 12,7mm. 10 cohetes de "5 ó 2 bombas de 454 kg._REPAINT y aircraft.cfg: Claudio_Sanchez(Design Machine) -->claudiosanchez@icnet.com.ve Modelo:Mike Stone
[WEIGHT_AND_BALANCE]
max_gross_weight = 20315.000
empty_weight = 10868.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, -1.000
max_number_of_stations =50
;Moments of Inertia
empty_weight_pitch_MOI = 320000.000
empty_weight_roll_MOI = 50000.000
empty_weight_yaw_MOI = 120000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=0.000000,0.000000,0.000000,0.000000
[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 10, 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 20, 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =2.002
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =2.002
rudder_effectiveness =1.000
pitch_stability =2.002
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.512
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 1
Engine.0 = -19.000, 0.000, 0.000
fuel_flow_scalar = 0.200
[TurbineEngineData]
fuel_flow_gain = 0.003
inlet_area = 3.000
rated_N2_rpm = 30000.000
static_thrust = 5970.000
afterburner_available = 0
reverser_available = 0
[jet_engine]
thrust_scalar =1.000
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
[contact_points]
point.0= 1.000, 13.500, 0.000, -5.600, 1200.000, 0.000, 0.800, 45.000, 0.200, 2.500, 0.900, 3.000, 3.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.000, -4.000, -5.700, 1600.000, 1.000, 1.000, 0.000, 0.500, 2.500, 0.900, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -2.000, 4.000, -5.700, 1600.000, 2.000, 1.000, 0.000, 0.500, 2.500, 0.900, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -3.330, -23.920, -3.000, 787.400, 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, -3.330, 23.920, -3.000, 787.400, 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, -22.670, 0.000, 0.000, 787.400, 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, 23.030, 0.000, -1.500, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = -0.750
static_cg_height = 5.200
[$Views]
eyepoint = -17.11, -1.31, 1.64
[Views]
eyepoint=8.330258,0.000000,6.497232
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -7.61, -18.29, -1.48, fx_navred ,
light.1 = 3, -7.61, 18.29, -1.48, fx_navgre ,
light.2 = 3, -20.83, 0.10, 1.52, fx_navwhi ,
light.3 = 2, -20.83, -0.10, 1.52, fx_strobe ,
light.4 = 2, -7.61, -18.29, -1.48, fx_strobe ,
light.5 = 2, -7.61, 18.29, -1.48, fx_strobe ,
light.6 = 2, -20.83, -0.10, 1.52, fx_strobe ,
light.7 = 2, -7.61, -18.29, -1.48, fx_strobe ,
light.8 = 2, -7.61, 18.29, -1.48, fx_strobe ,
[SMOKESYSTEM]
smoke.0=-3.50,-12.00,0.00,fx_smoke_rx
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1 = 0.000, 0.000, 0.000, 300.000, 0.000
LeftMain = 0.000, -5.000, 0.000, 135.000, 0.000
RightMain = 0.000, 5.000, 0.000, 135.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area = 280.000
wing_span = 39.000
wing_root_chord = 9.500
wing_dihedral = 3.000
wing_incidence = -0.500
wing_twist = -1.000
oswald_efficiency_factor= 0.800
wing_winglets_flag = 0
wing_sweep = 37.000
wing_pos_apex_lon = 5.300
wing_pos_apex_vert = -2.000
htail_area = 70.000
htail_span = 12.800
htail_pos_lon = -25.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 35.000
vtail_area = 60.000
vtail_span = 7.000
vtail_sweep = 35.000
vtail_pos_lon = -25.000
vtail_pos_vert = 2.000
elevator_area = 25.000
aileron_area = 26.000
rudder_area = 6.500
elevator_up_limit = 17.000
elevator_down_limit = 15.000
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 15.000
spoiler_limit = 60.000
spoilerons_available = 0
aileron_to_spoileron_gain = 4.600
min_ailerons_for_spoilerons = 5.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed = 120.000
full_flaps_stall_speed = 100.000
cruise_speed = 597.000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
