[fltsim.0]
title=ARNZ BAE 146-300 'White'
sim=bae1463
model=
panel=
sound=
texture=white
checklists=
ui_manufacturer=British Aerospace
ui_type=146 300
ui_variation=Plain White
description=Aircraft by Jon Murchison - www.flightsim.co.nz, Panel by Matthias Lieberecht - www.baepanelproject.com, Distribution - Historic Jetliner Group - http://www.simviation.com/hjg/main.htm
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
atc_type=BAe
atc_model=BA46
visual_damage=0
atc_id_color=0x00000000
atc_parking_types=GATE,RAMP
atc_id_font=Verdana,-11,1,600,0

[fltsim.1]
title=ARNZ BAE 146-300
sim=bae1463
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=British Aerospace
ui_type=146 300
ui_variation= Flight Test
description=Aircraft by Jon Murchison - www.flightsim.co.nz, Panel by Matthias Lieberecht - www.baepanelproject.com, Distribution - Historic Jetliner Group - http://www.simviation.com/hjg/main.htm
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
atc_type=BAe
atc_model=BA46
visual_damage=0
atc_id_color=0x00000000
atc_parking_types=GATE,RAMP
atc_id_font=Verdana,-11,1,600,0
[General]
performance=Cruise Speed: 432 Knots TAS or Mach 0,7\nMaximum Range: 1,138 nm\nService Ceiling: 29,000 ft\nMax Takeoff Wgt: 44,225 kgn\n\n\n\n\n 
atc_type=BRITISHAEROSPACE 
atc_model=BA46 
editable=1


[General]
performance=Cruise Speed: 432 Knots TAS or Mach 0,7\nMaximum Range: 1,138 nm\nService Ceiling: 29,000 ft\nMax Takeoff Wgt: 44,225 kgn\n\n\n\n\n 
atc_type=BRITISHAEROSPACE 
atc_model=BA46 
editable=1 

[flight_tuning]
cruise_lift_scalar=1.360 
pitch_stability=1.1
roll_stability=1.0
yaw_stability=1.1
parasite_drag_scalar=1.05 
induced_drag_scalar=1.0
elevator_effectiveness=0.9 
aileron_effectiveness=1.0
rudder_effectiveness=1.100 
elevator_trim_effectiveness=0.8
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.000 

[weight_and_balance]

// ACM V2.0
max_gross_weight = 97516
empty_weight = 54500
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 1157891
empty_weight_roll_MOI = 560372
empty_weight_yaw_MOI = 1575881
empty_weight_coupled_MOI = 0

max_number_of_stations = 7

station_load.0 = "340.0, 37.5, 0.0, 0.0, Pilots"
station_load.1 = "5100.0,  27.50,  0.00, 0.00, 30 Pax forward"
station_load.2 = "5900.0, 5.0,  0.00, 0.00, 35 Pax center"
station_load.3 = "5900.0, -12.5.0,  0.00, 0.00, 35 Pax aft"
station_load.4 = "2500, 22.5, 0.0, 0.0, Cargo forward"
station_load.5 = "2500, -12.5, 0.0, 0.0, Cargo aft"


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 1, -43,  2.5, fx_navredh ,
light.1 = 3,  1,  43,   2.5, fx_navgreh ,
light.2 = 2, -44.5,    0.00,   3.4, fx_strobeh ,
light.3 = 2, 0, -43,   2.5, fx_strobeh ,
light.4 = 2, 0,  43,   2.5, fx_strobeh ,
light.5 = 1, 13.5,    0.00,  7, fx_beaconh ,
light.6 = 1,  8.8,    -2.3, -6.5, fx_beaconb ,
light.7 = 4,  42.0,    0.00,   1.102, fx_vclighth,


[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop

engine_type = 1
fuel_flow_scalar = 1.150
engine.0 = 3.000, -21.000, -0.667
engine.1 = 6.000, -13.000, -0.500
engine.2 = 6.000, 13.000, -0.500
engine.3 = 3.000, 21.000, -0.667
min_throttle_limit=0.000000


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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
// Total fuel equivalent 20600 lb

Center1 = 0, 0, 0, 659, 0
LeftMain = -1, -19, 0, 1216, 0
RightMain = -1, 19, 0, 1216, 0
electric_pump=0


[contact_points]
static_pitch = -1.2
static_cg_height = 9
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7

point.0 = 1, 42.800, 0, -8.57, 1574.809, 0, 0.9, 35, 0.3, 2.5, 0.987, 5, 5, 0, 0, 0
point.1 = 1, -3.5058, -15.00, -10.4, 1574.803, 1, 1.5, 0, 1.5, 2.5, 0.642, 5, 5, 2, 0, 0
point.2 = 1, -3.5057, 15.00, -10.4, 1574.803, 2, 1.5, 0, 1.5, 2.5, 0.642, 5, 5, 3, 0, 0
point.3 = 2, -10.2253, -42.8538, 2.3935, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -10.225, 42.5124, 2.2342, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -53.5457, 0, 3.4065, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 42.9256, 0, -2.8684, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0

[keyboard_response]
elevator = 110.000, 250.000
aileron = 110.000, 250.000
rudder = 110.000, 250.000


[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 = 1500
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 1000
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

[airplane_geometry]
//ACM_AREAW1// 0,0,0,3.2766,1.4562,1.4562,0,3.1127,2.9125,2.9125
//ACM_AREAW2// 0,2.9489,4.3688,4.3688,0,2.7851,5.8250,5.8250,0,2.6212
//ACM_AREAW3// 7.2813,7.2813,0,2.4574,8.7376,8.7376,0,2.2936,10.1938,10.1938
//ACM_AREAW4// 0,2.1297,11.6501,11.6501,0,1.9659,13.1064,13.1064,0,1.8021
//ACM_AREAH1// 0,0,0,2.8871,0.4811,0.4811,0,2.7428,0.9623,0.9623
//ACM_AREAH2// 0,2.5984,1.4435,1.4435,0,2.4540,1.9247,1.9247,0,2.3097
//ACM_AREAH3// 2.4059,2.4059,0,2.1653,2.8871,2.8871,0,2.0210,3.3683,3.3683
//ACM_AREAH4// 0,1.8766,3.8495,3.8495,0,1.7323,4.3307,4.3307,0,1.5879
//ACM_AREAV1// 0,0,0,4.9514,0.5501,0.5501,0,4.5553,1.1003,1.1003
//ACM_AREAV2// 0,4.1592,1.6504,1.6504,0,3.7631,2.2006,2.2006,0,3.3670
//ACM_AREAV3// 2.7508,2.7508,0,2.9708,3.3009,3.3009,0,2.5747,3.8511,3.8511
//ACM_AREAV4// 0,2.1786,4.4013,4.4013,0,1.7825,4.9514,4.9514,0,1.3864
//ACM_CAREAW1// 6.5532,6.5532,1.6383,2.2936,7.2813,7.2813,1.6383,2.2608,8.0094,8.0094
//ACM_CAREAW2// 1.6383,2.2280,8.7376,8.7376,1.6383,2.1953,9.4657,9.4657,1.6383,2.1625
//ACM_CAREAW3// 10.1938,10.1938,1.6383,2.1297,10.9220,10.9220,1.6383,2.0970,11.6501,11.6501
//ACM_CAREAW4// 1.6383,2.0642,12.3782,12.3782,1.6383,2.0314,13.1064,13.1064,1.6383,1.9987
//ACM_CAREAH1// 0,0,1.4435,2.8871,0.4811,0.4811,1.4435,2.8149,0.9623,0.9623
//ACM_CAREAH2// 1.4435,2.7428,1.4435,1.4435,1.4435,2.6706,1.9247,1.9247,1.4435,2.5984
//ACM_CAREAH3// 2.4059,2.4059,1.4435,2.5262,2.8871,2.8871,1.4435,2.4540,3.3683,3.3683
//ACM_CAREAH4// 1.4435,2.3819,3.8495,3.8495,1.4435,2.3097,4.3307,4.3307,1.4435,2.2375
//ACM_CAREAV1// 0,0,1.2378,3.7136,0.5501,0.5501,1.2378,3.5155,1.1003,1.1003
//ACM_CAREAV2// 1.2378,3.3174,1.6504,1.6504,1.2378,3.1194,2.2006,2.2006,1.2378,2.9213
//ACM_CAREAV3// 2.7508,2.7508,1.2378,2.7233,3.3009,3.3009,1.2378,2.5252,3.8511,3.8511
//ACM_CAREAV4// 1.2378,2.3271,4.4013,4.4013,1.2378,2.1291,4.9514,4.9514,1.2378,1.9310
wing_area = 894.000
wing_span = 86.000
wing_root_chord = 9.850
wing_dihedral = -1.000
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor = 0.800
wing_winglets_flag = 0
wing_sweep = 15.000
wing_pos_apex_lon = 8.500
wing_pos_apex_vert = 0.000
htail_area = 304.000
htail_span = 28.417
htail_pos_lon = -41.000
htail_pos_vert = 0.000
htail_incidence = -1.800
htail_sweep = 0.000
vtail_area = 203.000
vtail_span = 16.245
vtail_sweep = 0.000
vtail_pos_lon = -40.000
vtail_pos_vert = 5.833
elevator_area = 87.000
aileron_area = 36.960
rudder_area = 34.5
elevator_up_limit = 25.5
elevator_down_limit = 21.5
aileron_up_limit = 19.5
aileron_down_limit = 14.5
rudder_limit = 23.5
elevator_trim_limit = 8.5
spoiler_limit = 60.0
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 9.969
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 0, 2 , 17.0
electric_always_available = 1

[TurbineEngineData]
fuel_flow_gain=0.003 
inlet_area=5.500 
rated_N2_rpm=29920 
static_thrust=7600
afterburner_available=0 
reverser_available=0 

[jet_engine]
thrust_scalar=1.100 

[Reference Speeds]
flaps_up_stall_speed    = 102.0
full_flaps_stall_speed  = 92.11
cruise_speed            = 350.0
max_mach                = 0.72
max_indicated_speed     = 300

[exits]
number_of_exits = 3
exit_rate.0 = 0.1
exit_rate.1 = 0.4
exit_rate.2 = 0.4

[folding_wings]
wing_fold_system_type=4
fold_rates=0.075,0.075

[Views]
eyepoint=41.28, -1.98, 3.00 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1500.000 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=96.500
pitch_takeoff_ga=8.000 
default_pitch_mode=0
default_bank_mode=0  
max_pitch=10.000000
max_pitch_acceleration=1.4
max_pitch_velocity_lo_alt=2.8
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=18000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.000000
max_bank_acceleration=2.20 
max_bank_velocity=4.000000
max_throttle_rate=0.100000
nav_proportional_control=12.000000
nav_integrator_control=0.200000
nav_derivative_control=1.200000
nav_integrator_boundary=1.000000
nav_derivative_boundary=0.700000
gs_proportional_control=15.000000
gs_integrator_control=0.300000
gs_derivative_control=0.900000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.300000
yaw_damper_gain=0.450000

[pitot_static]
vertical_speed_time_constant=10

[direction_indicators]
direction_indicator.0=3,0 

[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 1, 1 
Nav.2=1, 1, 1 
Adf.1=1 
Transponder.1=1 
Marker.1=1 


[Flaps.0]
type=1
span-outboard=0.800
extending-time=4.000
system_type=1
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.250
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000000,0.000000
flaps-position.1=18.000000,0.000000
flaps-position.2=24.000000,0.000000
flaps-position.3=30.000000,0.000000
flaps-position.4=33.000000,0.000000

[brakes]
toe_brakes_scale=1.0
parking_brake=1
differential_braking_scale =0.5

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.06
flap_limit_power=24.0
flap_limit_idle=18.0

[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3100.000000

[stall_warning]
type=2

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0