[fltsim.0]
title=Avro Arrow
sim=arrow
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N456LJ
ui_manufacturer=ALPHA
ui_type=Arrow
ui_variation=RCAF
description=The first all-new Learjet since Bill Lear rolled the model 23 off the line in the 1960s, this computer-designed airplane is a fast, high altitude flyer. Certified up to 51,000 ft (15,545 m), the Learjet 45 often cruises above standard airliner altitudes. After transitioning in Flight Simulator from the complex single-engine airplanes to the King Air, move into piloting jets with the Lear. See the Aircraft Information section of Help for tips on flying this aircraft.  
atc_heavy=0
atc_airline=
atc_flight_number=

[fltsim.1]
title=Avro Arrow RL203
sim=arrow
model=
panel=
sound=
texture=203
kb_checklists=
kb_reference=
atc_id=RL203
ui_manufacturer=ALPHA
ui_type=Arrow
ui_variation=RL203
description=The third prototype for the Avro Arrow
atc_heavy=0
atc_airline=Canforce
atc_flight_number=203
atc_parking_types=MIL_COMBAT
atc_parking_codes=M002


[General]
atc_type=Avro
atc_model=Arrow
editable=1
performance=Cruise Speed\t\nMach 0.81            464 kts          859 kmh\n\nEngines\t\nAllied Signal TFE731-20     3,500 lb thrust\n\nMaximum Range\t\n2,200 nm            2,532 sm \t     4,074 km\n\nService Ceiling\t\n51,000 ft             15,545 m\n\nFuel Capacity\t\n6,062 lb              2,722 kg\n905 U.S. gal         3,424 L \n\nMaximum Gross Weight\t\n20,450 lb             9,276 kg\n\nMaximum Takeoff Weight - HGW\t\n20,200 lb \t9,163 kg\n\nUseful Load\t\n8,750 lb  \t3,969 kg\n\nLength\t\n58.4 ft\t               17.7 m\n\nWingspan\t\n47.8 ft\t               14.6 m\n\nHeight\t\n14.3 ft\t               4.3 m\n\nSeating\t\nUp to 9

[WEIGHT_AND_BALANCE]
max_gross_weight = 62430.000
empty_weight = 43960.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations = 50

;Moments of Inertia
empty_weight_pitch_MOI   = 3000000.000
empty_weight_roll_MOI    = 300000.000
empty_weight_yaw_MOI     = 2400000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[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     =0.500
parasite_drag_scalar   =2.001
induced_drag_scalar    =2.000
elevator_effectiveness =2.001
aileron_effectiveness  =4.000
rudder_effectiveness   =1.000
pitch_stability        =2.002
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =0.502
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type = 1
Engine.0 = -26.000, -2.800, 0.000
Engine.1 = -26.000, 2.800, 0.000
fuel_flow_scalar        = 1.000
min_throttle_limit = 0.00                      //Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain          = 0.003
inlet_area              = 1.000
rated_N2_rpm            = 29920.000
static_thrust           = 23400.000
afterburner_available   = 1
reverser_available      = 0.000

[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, 27.000, 0.000, -9.500, 1500.000, 0.000, 0.700, 45.000, 0.150, 2.500, 0.950, 4.000, 4.000, 0.000, 260.000, 260.000
point.1= 1.000, -4.000, -12.000, -8.000, 2000.000, 1.000, 1.100, 0.000, 0.300, 2.500, 0.500, 5.000, 5.000, 2.000, 260.000, 260.000
point.2= 1.000, -4.000, 12.000, -8.000, 2000.000, 2.000, 1.100, 0.000, 0.300, 2.500, 0.500, 5.100, 5.100, 3.000, 260.000, 260.000
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 = 3.000
static_cg_height = 8.000
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 = 2  //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 = 31.51, 0.00, 3.31

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3,  -21.57, -25.10,  0.97, fx_navredm,
light.1 = 3,  -21.57,  25.10,  0.97, fx_navgrem,
light.2 = 3,  -31.49,   0.00, 14.47, fx_navwhi,
light.3 = 2,  -21.82, -25.10,  0.97, fx_strobeh,
light.4 = 2,  -21.82,  25.10,  0.97, fx_strobeh,
light.5 = 2,  -31.17,   0.00, 13.97, fx_strobeh,
light.6 = 4,   31.71,   0.00,  3.83, fx_vclighth,


[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, 1

[fuel]
Center1   = 0.000, 0.000, 0.000, 0.000, 0.000
LeftMain  = 0.000, 0.000, 0.000, 1250.000, 0.000
RightMain = 0.000, 0.000, 0.000, 1250.000, 0.000
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1

[airplane_geometry]
wing_area               = 1225.000
wing_span               = 50.000
wing_root_chord         = 45.000
wing_dihedral           = -3.000
wing_incidence          = 0.000
wing_twist              = 0.000
oswald_efficiency_factor= 1.000
wing_winglets_flag      = 0
wing_sweep              = 55.000
wing_pos_apex_lon       = 15.000
wing_pos_apex_vert      = 1.000
htail_area              = 600.000
htail_span              = 24.000
htail_pos_lon           = -60.000
htail_pos_vert          = 0.000
htail_incidence         = 0.000
htail_sweep             = 45.000
vtail_area              = 132.000
vtail_span              = 12.000
vtail_sweep             = 50.000
vtail_pos_lon           = -50.000
vtail_pos_vert          = 4.100
elevator_area           = 45.000
aileron_area            = 40.000
rudder_area             = 40.000
elevator_up_limit       = 17.000
elevator_down_limit     = 15.500
aileron_up_limit        = 18.000
aileron_down_limit      = 18.000
rudder_limit            = 20.000
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    = 150.000
full_flaps_stall_speed  = 150.000
cruise_speed            = 700.000
max_mach                = 1.98
max_indicated_speed     = 1312                //Red line (KIAS)

[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;
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

[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


[TailHook]
tailhook_length=1
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=1
[Flaps.0]
type= 0
span-outboard= 0.000
extending-time= 0.100
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 0.000