// BAE146-100 For FSX version 20
// FSDS model, panel design, XML gauge design by Jean-Pierre Brisard
// FD and Master Textures by Bob May
// Copyright 2010 - Premier Aircraft Design
[fltsim.0]
title=BAE1461_X20
sim=bae146-100
model=100
panel=BAE1461_x
sound=0
texture=BA
kb_checklists=bae146_check
kb_reference=bae146_ref
atc_id=G-MABR
atc_airline=speed bird
atc_flight_number=2413
atc_heavy=0
atc_parking_types=ramp, gate
ui_manufacturer=British Aerospace
ui_type=BAE146-100
ui_variation=British Airways G-MABR
description=The BAe 146 is a medium-sized commercial aircraft which was manufactured in the United Kingdom by British Aerospace (which later became part of BAE Systems). Production ran from 1983 until 2002. Manufacture of the improved version known as the Avro RJ began in 1992.The BAe 146/Avro RJ is a high-wing cantilever monoplane with a T-tail. It has four turbofan jet engines mounted on pylons underneath the wings, and has retractable tricycle landing gear. The aircraft has very quiet operation, and has been marketed under the name Whisperjet. It sees wide usage at small city-based airports. In its primary role it serves as a regional jet, short-haul airliner or regional airliner. The BAe 146/Avro RJ is in wide use among European airlines, such as Brussels Airlines, Swiss International Air Lines and Lufthansa. The freight-carrying version has the designation "QT" (Quiet Trader), while a convertible version is designated "QC".
The BAe 146 comes in -100, -200 and -300 models. The equivalent Avro RJ versions are designated RJ70, RJ85, and RJ100.
[fltsim.1]
title=BAE1461_CC2 20
sim=bae146-100
model=CC2
panel=BAE1461_x
sound=0
texture=cc2
kb_checklists=bae146_check
kb_reference=bae146_ref
atc_id=ZE700
atc_airline=air force
atc_flight_number=51
atc_heavy=0
atc_parking_types=ramp, gate
ui_manufacturer=British Aerospace
ui_type=BAE146-100
ui_variation=CC2 Royal Air Force
description=BAe CC2 is the designation given to the Bae 146-100 by the Royal Air Force. The CC2 is used to transport members of the royal family and heads of state. It is equiped with an executive interior and has various passive methods of defence against guided missiles.
[General]
atc_type=BRITISHAEROSPACE
atc_model=BA46
editable=1
performance="Cruise Speed \n432 kts TAS 520 mph 885 km\/h\n\nEngines \n4 x Textron Lycoming ALF 502R-5 Turbofans\n\nMaximum Range \n1808 nm \n\nService Ceiling \n33, 089 ft \
category=airplane
[Views]
eyepoint = 23.00,-1.76,-3.5 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[WEIGHT_AND_BALANCE]
max_gross_weight =93000.0
empty_weight =42684.00000
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -0.000, -0.000, -0.000
max_number_of_stations =3
;Moments of Inertia
empty_weight_roll_MOI =168818.64385
empty_weight_pitch_MOI =471587.58696
empty_weight_yaw_MOI =452011.91891
empty_weight_coupled_MOI =0.00000
station_load.0= 180, -0.000, -2.000, 8.000, Pilot
station_load.1= 180, -0.000, 2.000, 8.000, Co-pilot
station_load.2= 9000, -7.200, 0.000, -7.000, Pass/luggage
[fuel]
LeftMain = -0.000, -8.000, -4.000, 750.000, 0.000
RightMain = -0.000, 8.000, -4.000, 750.000, 0.000
Center1 = -0.000, 0.000, -7.000, 1500.000, 0.000
fuel_type =2
number_of_tank_selectors =1
electric_pump=1
fuel_dump_rate=0.02000
anemometer_pump=0
manual_pump=0
engine_driven_pump=0
[airplane_geometry]
wing_area =932.00000
wing_span =86.00000
wing_root_chord =11.37907
wing_dihedral =-3.00000
wing_incidence =3.00000
wing_twist =-0.30000
oswald_efficiency_factor=0.78600
wing_winglets_flag =0
wing_sweep =37.50000
wing_pos_apex_lon =18.93413
wing_pos_apex_vert =0.00000
htail_area =153.82000
htail_span =32.75000
htail_pos_lon =-45.29065
htail_pos_vert =0.00000
htail_incidence =0.00000
htail_sweep =30.00000
vtail_area =131.54000
vtail_span =15.26000
vtail_sweep =30.00000
vtail_pos_lon =-40.55640
vtail_pos_vert =2.42000
elevator_area =57.50000
aileron_area =59.90000
rudder_area =39.17000
elevator_up_limit =25.00000
elevator_down_limit =25.00000
aileron_up_limit =20.00000
aileron_down_limit =20.00000
rudder_limit =30.00000
elevator_trim_limit =20.00000
spoiler_limit =45.00000
spoilerons_available =0
aileron_to_spoileron_gain =3.00000
min_ailerons_for_spoilerons =10.00000
min_flaps_for_spoilerons =0.00000
spoiler_extension_time=3.00000
spoiler_handle_available=1
auto_spoiler_available=0
positive_g_limit_flaps_up=3.70000
negative_g_limit_flaps_up=-2.96000
positive_g_limit_flaps_down=2.59000
negative_g_limit_flaps_down=-2.22000
load_safety_factor=1.00000
[Reference Speeds]
flaps_up_stall_speed = 140.0 //Knots True (KTAS)
full_flaps_stall_speed = 112.0 //Knots True (KTAS)
cruise_speed =504.96229
max_mach =0.85000
max_indicated_speed =364.97016
[flaps.0]
type= 1
system_type=1
span-outboard= 0.800
extending-time= 10.0
damaging-speed=300.0
blowout-speed=350.0
flaps-position.0=0.00
flaps-position.1=18.00
flaps-position.2=24.00
flaps-position.3=30.00
flaps-position.4=33.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=-1.00
[flight_tuning]
cruise_lift_scalar =1.20000
parasite_drag_scalar =1.00000
induced_drag_scalar =1.00000
elevator_effectiveness =1.0000
aileron_effectiveness =1.00000
rudder_effectiveness =1.00000
pitch_stability =1.55000
roll_stability =1.50000
yaw_stability =1.00000
elevator_trim_effectiveness =0.80000
aileron_trim_effectiveness =0.80000
rudder_trim_effectiveness =1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=0.00000
torque_on_roll=0.00000
gyro_precession_on_roll=0.00000
gyro_precession_on_yaw=0.00000
[GeneralEngineData]
engine_type =1
Engine.0 =2.000, -29.500, -2.000
Engine.1 =2.000, -18.900, -2.000
Engine.2 =2.000, 18.900, -2.000
Engine.3 =2.000, 29.500, -2.000
fuel_flow_scalar =0.70000
min_throttle_limit =0
[TurbineEngineData]
fuel_flow_gain =0.00200
inlet_area =5.48500
rated_N2_rpm =29920.00000
static_thrust =6970.00000
afterburner_available =0
reverser_available =0
afterburner_throttle_threshold=0.00000
ThrustSpecificFuelConsumption=0.40000
AfterBurnThrustSpecificFuelConsumption=0.00000
[jet_engine]
thrust_scalar =1.00000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm =90
autothrottle_takeoff_ga=1
pitch_takeoff_ga =8
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=12
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=25
gs_integrator_control=0.53
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain =1
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
[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)
static_pitch = -0.000
static_cg_height = 12.900
gear_system_type=0
max_number_of_points=10
tailwheel_lock=0
;point.0= 1, 28.950, 0.000, -12.970, 3000, 0, 2.000, 70.000, 0.296, 2.500, 0.952, 9.000, 8.000, 0, 219.9, 250.3
point.0 = 1, 28.95, 0, -12.76, 3000, 0, 2, 70, 0.1, 2.5, 0.952, 9, 8, 0, 219.9, 250.3
point.1= 1, -3.440, -8.700, -13.620, 4000, 1, 2.000, 0.000, 1.000, 2.500, 0.900, 11.000, 9.000, 2, 219.9, 250.3
point.2= 1, -3.440, 8.700, -13.620, 4000, 2, 2.000, 0.000, 1.000, 2.500, 0.900, 11.000, 9.000, 3, 219.9, 250.3
point.3= 2, 45.000, 0.000, 0.000, 2000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -15.000, 43.500, 0.000, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -15.000, -43.000, 0.000, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, -55.000, 0.000, 18.000, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.7= 2, 0.000, 0.000, 8.000, 0, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0
point.8= 2, 0.000, 0.000, -8.000, 0, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0
point.9= 5, -1.000, 0.000, -1.333, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
[gear_warning_system]
gear_warning_available =1
pct_throttle_limit =0.10000
flap_limit_idle =5.00000
flap_limit_power =25.50000
[brakes]
parking_brake =1
;toe_brakes_scale =1.24000
toe_brakes_scale =0.65
auto_brakes=1
hydraulic_system_scalar=1.00000
differential_braking_scale=0.20000
[hydraulic_system]
normal_pressure =3000.00000
electric_pumps = 0 //no electric pumps
engine_map = 1,1,1,1 //pumps on Eng1,2,3,4
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 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
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 7=recognition
light.0 =3, -8.250000, -43.700000, -2.600000, fx_navred
light.1 =3, -8.250000, 43.700000, -2.600000, fx_navgre
light.2 =3, -45.020000, 0.000000, -2.500000, fx_navwhi
light.3 =2, -8.800000, -43.800000, -2.600000, fx_strobeh
light.4 =2, -8.800000, 43.800000, -2.600000, fx_strobeh
light.5 =1, -43.500000, 0.000000, 13.500000, fx_beaconh
light.6=3, 5.750000, -3.260000, -0.750000, fx_navwhi
light.7=3, 5.750000, 3.260000, -0.750000, fx_navwhi
light.8=4, 27.694000, 0.000000, -4.77, fx_vclighth
light.9=4,20.80000, 0.000000, -4.77, fx_vclighth
light.10=4, 17.00, 0.000000, -4.77, fx_vclighth
light.11=4, 7.000000, 0.000000, -4.77, fx_vclighth
light.12=4,0.000000, 0.000000, -4.77, fx_vclighth
[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
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[TailHook]
tailhook_length= 4.000
tailhook_position = -15.000, 0.000, -1.000
cable_force_adjust = 1.0
[exits]
number_of_exits = 2
exit.0=0.2,17.786,-5.186,-6.745,0 ;Percent per second
exit.1=0.2,-17.374,2.586,-10.195,1 ;Percent per second
//MAIN EXIT; z=17.786, x=-5.186, y=-6.745
//REAR BAG; z=-17.374, x=2.586, y=-10.195
[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=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
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
[stall_warning]
type=2
stick_shaker=1
[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=0
