[fltsim.0]
title=Paint2
sim=CRJ-200ER
model=
panel=
sound=
texture=
atc_heavy=0
atc_airline=JERSEY
atc_flight_number=1336
ui_manufacturer=Bombardier
ui_type=CRJ-200ER
ui_variation=Flybe
visual_damage=1
description=Project Opensky \nBombardier Canadair Regional Jet -- CRJ-200ER\nVersion 2002.1.5\n\nFS2002 Only\n\nEngine Type: General Electric CF34-3B1\n\nModel Designer\n Mitsushi Yutaka\n\nFlight Dynamics Designer\n Warren C. Daniel\n\nTexture Designer\n C. Vincent Cho\n\nTechnical Resource\n Nick Peterson\n Simon Ng\n\nTest Pilots\n Project Opensky Members
[General]
atc_type=BOMBARDIER
atc_model=CARJ
performance=Refer to the kneeboard reference sheet\n\nFlight Dynamics modified by Peter Beddig
[WEIGHT_AND_BALANCE]
max_gross_weight= 51250.000
empty_weight= 30500.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 2.000, 0.000, 0.000
max_number_of_stations= 8
station_load.0 =340.000000, 32.400000, 0.000000, 1.500000, Pilots
station_load.1 =4420.000000, 17.600000, 0.000000, 1.500000, PAX front
station_load.2 =4420.000000, -6.600000, 0.000000, 1.500000, PAX rear
station_load.3 =2000.000000, -16.400000, 0.000000, 1.500000, Baggage
empty_weight_roll_MOI= 150774.000
empty_weight_pitch_MOI= 242040.000
empty_weight_yaw_MOI= 416940.000
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 =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 1
Engine.0 = -15.200, -7.500, 4.200
Engine.1 = -15.200, 7.500, 4.200
fuel_flow_scalar = 0.800
min_throttle_limit = -0.30 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
//bypass_ratio=6.2
fuel_flow_gain= 0.002
inlet_area= 7.900
rated_N2_rpm= 29920.000
static_thrust= 9220.000
afterburner_available= 0
reverser_available= 1.000
[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, 34.800, 0.000, -6.000, 1181.100, 0.000, 0.635, 54.000, 0.250, 2.000, 0.950, 10.000, 10.000, 0.000, 260.000, 260.000
point.1= 1.000, 0.000, -6.000, -6.200, 1574.800, 1.000, 1.080, 0.000, 0.600, 2.000, 0.850, 9.000, 9.000, 2.000, 260.000, 260.000
point.2= 1.000, 0.000, 6.000, -6.200, 1574.800, 2.000, 1.080, 0.000, 0.600, 2.000, 0.850, 9.000, 9.000, 3.000, 260.000, 260.000
point.3= 2.000, 0.000, -35.000, 0.000, 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, 0.000, 35.000, 0.000, 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, -35.000, 0.000, 1.000, 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, 42.400, 0.000, -2.000, 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 = 0.000
static_cg_height = 5.700
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 = 33.0 //Flap angle that activates warning at idle
flap_limit_power = 25.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.2 //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 = 35.400, -1.250, 4.000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, -5.20, -33.20, -0.25, fx_navredm ,
light.1=3, -5.20, 33.20, -0.25, fx_navgrem ,
light.2=3, -36.29, 0.00, 4.45, fx_navwhi ,
light.3=2, -5.37, -33.30, -0.25, fx_strobeh ,
light.4=2, -5.37, 33.30, -0.25, fx_strobeh ,
light.5=1, 19.00, 0.00, 7.02, fx_beaconh ,
light.6=1, 19.00, 0.00, -2.15, fx_beaconb ,
light.7=4, 23.70, 0.00, 2.20, fx_vclighth,
light.8=1, 34.85, 1.65, 5.4, fx_vclight ,
light.9=1, 34.85, -1.65, 5.4, fx_vclight ,
light.10=1, 28.00, 0.00, 4.5, fx_vclighth ,
light.11=1, 10.00, 0.00, 4.5, fx_vclighth ,
light.12=1, -8.00, 0.00, 4.5, 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]
LeftMain= 3.400, -9.360, -1.000, 1067.637, 0.000
RightMain= 3.400, 9.360, -1.000, 1067.637, 0.000
fuel_type= 2.000
number_of_tank_selectors= 1
electric_pump=1
[airplane_geometry]
wing_area= 520.400
wing_span= 69.600
wing_root_chord= 12.200
wing_dihedral= 2.300
wing_incidence= 0.000
wing_twist= -0.500
oswald_efficiency_factor= 0.680
wing_winglets_flag= 1
wing_sweep= 24.700
wing_pos_apex_lon= 9.700
wing_pos_apex_vert= -1.200
htail_area= 101.600
htail_span= 20.800
htail_pos_lon= -36.000
htail_pos_vert= 14.000
htail_incidence= 0.000
htail_sweep= 30.000
vtail_area= 98.800
vtail_span= 8.600
vtail_sweep= 41.000
vtail_pos_lon= -26.000
vtail_pos_vert= 6.000
elevator_area= 53.500
aileron_area= 20.000
rudder_area= 46.400
elevator_up_limit= 22.500
elevator_down_limit= 19.500
aileron_up_limit= 20.000
aileron_down_limit= 20.000
rudder_limit= 26.000
elevator_trim_limit= 20.000
spoiler_limit= 60.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed = 112.000
full_flaps_stall_speed = 102.000
cruise_speed = 464.000
max_mach = 0.81
max_indicated_speed = 330
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
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
[Flaps.0]
type= 1
span-outboard= 0.300
extending-time= 6.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 45.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.500
extending-time= 15.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 45.000, 0.000