[fltsim.0]
title=B461BOT
sim=BAE146
model=
texture=BOT
ui_type=B461
ui_manufacturer=IVAO
ui_variation=Air Botswana (BOT)
description=IVAO Multiplayer Traffic Library\n(c) 2004-2006 International Virtual Aviation Organisation\n\nBAe 146-100\nmodel: Fernando MARTINEZ AIA\nfde: Koji TANAKA (Mr Hiro) & David CARTER & David FREED\npaint: Fernando MARTINEZ AIA\nLOD1 polygons: 115\nLOD9 polygons: 2737\n\nTHESE FILES MAY NOT BE UPLOADED TO ANY OTHER SITE WITHOUT THE AUTHOR'S WRITTEN PERMISSION. THESE REPAINTS AND MODELS ARE FREEWARE AND MAY NOT BE SOLD, OR PUT ON ANY SITE THAT CHARGES FOR DOWNLOADING FREE FILES. THE FILES FOUND IN THIS ARCHIVE MAY NOT BE DISTRIBUTED ON CD OR ANY MEDIUM FOR ANY KIND OF FEE, INCLUDING THE COST OF PRODUCTION, MATERIALS OR POSTAGE.

[General]
editable=0
performance=LOD1 polygons: 2737\nLOD9 polygons: 115\n

[WEIGHT_AND_BALANCE]
max_gross_weight = 110000.0
empty_weight = 55800.0
reference_datum_position     = 0.0, 0.0, 0.0
empty_weight_CG_position     = 1.5, 0.0, -1.0
max_number_of_stations =2
station_load.0 =30000.0, 2.5, 0.0, 1.0

;Moments of Inertia
empty_weight_pitch_MOI  = 2500000.0
empty_weight_roll_MOI   = 1800000.0
empty_weight_yaw_MOI    = 3700000.0
empty_weight_coupled_MOI        = 0.0
CG_forward_limit= 0.0
CG_aft_limit= 1.0

[flight_tuning]
cruise_lift_scalar=1.1
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness =2.4
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
Engine.0=1.000, -21.800, -6.500
Engine.1=1.000, 21.800, -6.500
Engine.2=2.000, -13.500, -6.000
Engine.3=2.000, 13.500, -6.000
fuel_flow_scalar = 1.0
min_throttle_limit = -0.12                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -30                  //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 15.7
rated_N2_rpm = 29920.0
static_thrust = 8500
afterburner_available = 0
reverser_available = 1

[jet_engine]
thrust_scalar =1.000

[contact_points]

        //0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
        //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
        //14 Airspeed limit for retraction     (KIAS)
        //15 Airspeed that gear gets damage at (KIAS)
        
point.0=1.0, 31.5, 0.0, -8.7, 1181.1, 0.0, 1.1, 40, 0.65, 1.6, 0.9, 4.8, 4.8, 0, 250, 250
point.1=1.0, -1.4,-7.4, -9.48, 1574.8, 1.0, 1.6, 0.0, 1.5, 1.2, 0.9, 5.1, 5.1, 2, 250, 250
point.2=1.0, -1.4, 7.4, -9.48, 1574.8, 2.0, 1.6, 0.0, 1.5, 1.2, 0.9, 5.1, 5.1, 3, 250, 250
point.3=2.0, -17.8,-46.5, 4.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 
point.4=2.0, -17.8, 46.5, 4.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 
point.5=2.0, -50.4,  0.0, 5.2, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 
point.6=2.0, 34.8,   0.0,-3.1, 787.4, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 

max_number_of_points=7
static_pitch=0.05
static_cg_height=8.5 
gear_system_type=1      //Hydraulic

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 10, 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 20, 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 17.0
light_nav          = 0, 5 , 17.0
light_beacon       = 0, 5 , 17.0
light_landing      = 0, 5 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 17.0

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, -3, -42.5, 2.65, fx_navredm
light.1 = 1, -3, 42.5, 2.65, fx_navgrem
light.2 = 2, -3.5, -42.6, 2.65, fx_strobeh
light.3 = 2, -3.5, 42.6, 2.65, fx_strobeh
light.4 = 1,  3.25, -2, -6.25, fx_beaconb
light.5 = 3, -39.8, 0, 3, fx_navwhi
light.6 = 3, -39.8, 0, 2.85, fx_strobe
light.7 = 1,  9, 0, 6.35, fx_beacon

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1         //Parking brake available
toe_brakes_scale = 0.18  //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=39.9, -1.31, 4.7   //(feet) longitudinal, lateral, vertical distance from reference datum

[Radios]
// Radio Type = availiable, standby frequency, has glide slope.
Audio.1       = 1
Com.1         = 1, 1
Com.2         = 1, 1
Nav.1         = 1, 1, 1
Nav.2         = 1, 1, 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 = 1 

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

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

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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2500
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 93
autothrottle_takeoff_ga=1
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=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[fuel]
Center1 = 0.0, 0.0, -1.0, 1980.0, 0.0
LeftMain  = -4.7, -9.4, 0.0, 1400.0, 0.0
RightMain = -4.7, 9.4, 0.0, 1400.0, 0.0
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=0

[airplane_geometry]
wing_area               = 980.0
wing_span               = 93.0
wing_root_chord         = 19.9
wing_dihedral           = 5.2
wing_incidence          = 1.5
wing_twist              = -0.2
oswald_efficiency_factor= 0.73
wing_winglets_flag      = 0
wing_sweep              = 27.0
wing_pos_apex_lon       = 9.5
wing_pos_apex_vert      = 0.0
htail_area              = 264.6
htail_span              = 36.0
htail_pos_lon           = -39.9
htail_pos_vert          = 8.9
htail_incidence         = 0.0
htail_sweep             = 39.0
vtail_area              = 219.9
vtail_span              = 19.9
vtail_sweep             = 40.0
vtail_pos_lon           = -31.5
vtail_pos_vert          = 11.0
elevator_area           = 228.2
aileron_area            = 29.8
rudder_area             = 62.8
elevator_up_limit       = 22.5
elevator_down_limit     = 21.5
aileron_up_limit        = 20.0
aileron_down_limit      = 20.0
rudder_limit            = 26.0
elevator_trim_limit     = 20.0
spoiler_limit           = 60.0
spoilerons_available    = 1
aileron_to_spoileron_gain = 3.0
min_ailerons_for_spoilerons = 10.0
min_flaps_for_spoilerons = 0.0

[Reference Speeds] 
flaps_up_stall_speed=122.0
full_flaps_stall_speed=132.0
cruise_speed=435.0
max_indicated_speed=300.0
max_mach= 0.78

[forcefeedback]
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=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 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

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI

[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 20                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 1                                    // degrees
flaps-position.2 = 2                                    // degrees
flaps-position.3 = 5                                    // degrees
flaps-position.4 = 10                                   // degrees
flaps-position.5 = 20                                   // degrees
flaps-position.6 = 30                                   // degrees
flaps-position.7 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.1]       //Outboard Leading Edge Slat
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 3                                    // seconds
flaps-position.0 = 0                                    // 
flaps-position.1 = 0.5                                  // 
flaps-position.4 = 1.0                                  // 
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic


[fltsim.1]
title=PAUKNAIR EC-GEO
sim=BAE146
model=
texture=1
ui_type=B461
ui_manufacturer=IVAO
ui_variation=PAUKNAIR EC-GEO
description=IVAO Multiplayer Traffic Library\n(c) 2004-2006 International Virtual Aviation Organisation\n\nBAe 146-100\nmodel: Fernando MARTINEZ AIA\nfde: Koji TANAKA (Mr Hiro) & David CARTER & David FREED\npaint: Fernando MARTINEZ AIA\nLOD1 polygons: 115\nLOD9 polygons: 2737\n\nTHESE FILES MAY NOT BE UPLOADED TO ANY OTHER SITE WITHOUT THE AUTHOR'S WRITTEN PERMISSION. THESE REPAINTS AND MODELS ARE FREEWARE AND MAY NOT BE SOLD, OR PUT ON ANY SITE THAT CHARGES FOR DOWNLOADING FREE FILES. THE FILES FOUND IN THIS ARCHIVE MAY NOT BE DISTRIBUTED ON CD OR ANY MEDIUM FOR ANY KIND OF FEE, INCLUDING THE COST OF PRODUCTION, MATERIALS OR POSTAGE.

atc_id=4101
atc_airline=4101
atc_flight_number=4101
