; Localized	07/07/2003 12:46  (GMT)	4:4.2.169 	aircraft.cfg
[fltsim.0]
title=HONDA V4
sim=hondajet_v4
model=v4
panel=v4
sound=""
texture=v4
kb_checklists=Lear45_check
kb_reference=Lear45_ref
atc_id=N420
ui_manufacturer=HONDA
ui_type=Learjet
ui_variation=V4
description=HONDA JET V4\n\nCabin Door   [Shift+E]\nWindow Curtain  [Shift+E]  then [2]\nCargo Doo       Wing Fold/ExtendAr

[General]
atc_type=Learjet
atc_model=""
editable=0
performance=Engines     GE-HONDA / HF-120\n\nMaximum Cruise Speed  FL300        \n420 Knot        483mph   778 km\/h\n\nVFR Range    \n1400 nm          2592 km\nIFR Range (Cruise@FL410)   \n1180 nm          2185 km

[WEIGHT_AND_BALANCE]
max_gross_weight=12300.0                      // (pounds)
empty_weight=8800.0                          // (pounds)

reference_datum_position=34.5,  0, 0    // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-35.79, 0, 0    // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0="170, -25.0, -1.2, 0.0, "           // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="170, -25.0,  1.2, 0.0, 1"        // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="170, -32.5, -1.2, 0.0, 2"     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="170, -32.5,  1.2, 0.0, 3"     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="170, -36.7, -1.2, 0.0, 4"     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5="170, -36.7,  1.2, 0.0, 5"     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10="100, -42.0,  0.0, 0.0,  1"        // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11="50, -45.0,  0.0, 0.0,  2"        // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)


;Moments of Inertia
empty_weight_pitch_MOI=50000
empty_weight_roll_MOI=45000
empty_weight_yaw_MOI=70000
empty_weight_coupled_MOI=0.0

[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, 5 , 9.5
avionics=1, 5 , 9.5
additional_system=0, 2 , 9.5
marker_beacon=1, 2 , 9.0
fuel_pump=0, 5 , 9.0

[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=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[GeneralEngineData]
engine_type=1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-38.8, -4.8, 0.8                     //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-38.8,  4.8, 0.8                     //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.60                  //Scalar for fuel flow efficiency
min_throttle_limit=-0.28                      //Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain=0.0025                //Gain on fuel flow
inlet_area=2.5000                //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                 //RPM, second stage compressor rated value
static_thrust=2400                  //Lbs, max rated static thrust at Sea Level
afterburner_available=0                     //Afterburner available?
reverser_available=1                     //Thrust reverser available?

[jet_engine]
thrust_scalar=1.0


;/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, -20.30,   0.00, -4.77, 1181.1, 0, 0.6349, 46.8, 0.3000, 2.5, 2.9100, 10.0, 10.0, 0, 260.0, 260.0
point.1=1, -37.25,  -4.75, -4.80, 1574.8, 1, 0.6349,  0.0, 0.4798, 2.5, 0.5456,  9.0,  9.0, 2, 260.0, 260.0
point.2=1, -37.25,   4.75, -4.80, 1574.8, 2, 0.6349,  0.0, 0.4798, 2.5, 0.5456,  9.0,  9.0, 3, 260.0, 260.0
point.3=2, -37.83, -23.92, -3.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 5, 0.0, 0.0
point.4=2, -37.83,  23.92, -3.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 6, 0.0, 0.0
point.5=2, -57.17,   0.00,  0.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 9, 0.0, 0.0
point.6=2, -11.47,   0.00, -1.50,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 4, 0.0, 0.0

static_pitch=-0.14
static_cg_height=4.75
gear_system_type=1           //Hydraulic

[gear_warning_system]
gear_warning_available=1    //Normal
pct_throttle_limit=0.1     //Percent throttle that activates warning
flap_limit_idle=15.0     //Flap angle that activates warning at idle
flap_limit_power=30.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake=1       //Parking brake available
toe_brakes_scale=1.0  //Brake scalar

[hydraulic_system]
normal_pressure=3000.0    //PSI
electric_pumps=0         //no electric pumps
engine_map=1,1,0,0   //pumps on Eng1,2

[Views]
//eyepoint=-35.50,  1.23, 2.35   //Cabin Right Seat
//eyepoint=-35.50, -1.23, 2.35   //Cabin Left Seat
eyepoint=-26.38, -1.20, 2.46   //CockPit

[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,  -35.60, -19.20,  -1.50, fx_navred ,
light.1=3,  -35.60,  19.20,  -1.50, fx_navgre ,
light.2=3,  -52.52,   0.00,  2.70, fx_navwhi ,
light.3=1,  -36.20,   0.00, -2.70, fx_beacon ,
light.4=2,  -36.20,   0.00, -2.70, fx_strobe ,
light.5=1,  -53.75,   0.00,  9.79, fx_beacon ,

[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=5                                    // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=10                                    // degrees
flaps-position.2=20                                   // degrees
flaps-position.3=40                                   // degrees
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS

[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

[attitude_indicators]
;/Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=2
attitude_indicator.1=1

[turn_indicators]
;/Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s

[fuel]
Center1=-33.4,   0.0, -1.5, 150.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=-35.3, -10.0, -1.5, 105.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-35.3,  10.0, -1.5, 105.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area=200.0                 //Square feet
wing_span=40.0                  //Feet
wing_root_chord=9.9                   //Feet
wing_dihedral=2.5                   //Degrees
wing_incidence=0.5                   //Degrees
wing_twist=-1.5                  //Degrees
oswald_efficiency_factor=0.8                   //Measure of lift effeciency of wing
wing_winglets_flag=1                     //Are winglets available?
wing_sweep=13.4                  //Degrees, wing leading edge
wing_pos_apex_lon=-31.5                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_area=67.0                  //Square feet
htail_span=17.2                  //Feet
htail_pos_lon=-59.1                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence=2.0                   //Degrees
htail_sweep=25.0                  //Degrees, horizontal tail leading edge
vtail_area=42.0                  //Square feet
vtail_span=7.4                   //Feet, tip to body
vtail_sweep=30.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-55.0                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=4.1                   //Feet, vertical distance from reference point, positive going up
elevator_area=17.0                  //Square feet
aileron_area=13.5                  //Square feet
rudder_area=7.3                   //Square feet
elevator_up_limit=17.0                  //Degrees
elevator_down_limit=15.5                  //Degrees
aileron_up_limit=18.0                  //Degrees
aileron_down_limit=18.0                  //Degrees
rudder_limit=30.0                  //Degrees
elevator_trim_limit=15.0                  //Degrees
spoiler_limit=60.0                  //Degrees
spoilerons_available=1                     //Spoilerons Available?
aileron_to_spoileron_gain=4.6                 //Aileron to spoileron gain
min_ailerons_for_spoilerons=5                 //Degrees
min_flaps_for_spoilerons=0.0                   //Minimum flap handle position when spoilerons activate
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000

[Reference Speeds]
flaps_up_stall_speed=112.0                 //Knots True (KTAS)
full_flaps_stall_speed=102.0                 //Knots True (KTAS)
cruise_speed=420.0                 //Knots True (KTAS)
max_mach=0.80
max_indicated_speed=320                   //Red line (KIAS)

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=100
autothrottle_takeoff_ga=0
pitch_takeoff_ga=8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=1.0
use_no_default_pitch =1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
default_pitch_mode=0
default_bank_mode=0

[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

[stall_warning]
type=2
stick_shaker=1

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.2,0.2	                          ;Percent per second