//PREMIER AIRCRAFT DESIGN © 2009
//CANADAIR (Bombardier) CRJ100/200 FOR FS2004
//FSDS DESIGN BY JP BRISARD
//FD BY BOB MAY
[fltsim.0]
title=crj100_Air Canada Jazz
sim=crj200
model=
panel=crj200fs9
sound=0
texture=jazz_orange
kb_checklists=crj_check
kb_reference=crj_ref
atc_airline=Air Canada
atc_flight_number=2088
atc_heavy=0
atc_id=C-GKEW
ui_manufacturer=Bombardier
ui_type=Canadair CRJ 100LR
ui_variation=Air Canada Jazz
description=Bombardier \nCRJ100 for FS2004\nPremier Aircraft Design\nwww.premaircraft.com\/\nAll Files Copyright 2009
[fltsim.1]
title=crj100_Air Nostrum
sim=crj200
model=
panel=crj200fs9
sound=0
texture=air_nostrum
kb_checklists=crj_check
kb_reference=crj_ref
atc_airline=Iberia
atc_flight_number=248
atc_heavy=0
atc_id=EC-GZA
ui_manufacturer=Bombardier
ui_type=Canadair CRJ 200LR
ui_variation=Air Nostrum
description=Bombardier \nCRJ200 for FS2004\nPremier Aircraft Design\nwww.premaircraft.com\/\nAll Files Copyright 2009
[General]
atc_type=Bombardier
atc_model=CRJ200
editable=1
performance=Normal Cruise Speed\tMach .74\nMaximum Range\t1345 nm\nService Ceiling\t38,000 ft\nMax Gross Weight\t51,250 lb\nSeating\t\tUp to 50\nUseful Load\t13,100 lbS\n
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight=51100.0
empty_weight=20500.00000
reference_datum_position = 49.7, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -49.000, -0.000, -0.000
max_number_of_stations =3
station_name.0 = "Pilot"
station_name.1 = "Co-Pilot"
station_name.2 = "Passengers"
;Moments of Inertia
empty_weight_roll_MOI=53257.14000
empty_weight_pitch_MOI=148771.51000
empty_weight_yaw_MOI=142595.98000
empty_weight_coupled_MOI=0.00000
max_gross_weight=51100.0
empty_weight=20500.00000
station_load.0= 170, -49.700, -1.400, 0.000, //
station_load.1= 170, -49.700, 1.400, 0.000, //
station_load.2= 5700, -49.700, 0.000, 0.000, //
[airplane_geometry]
wing_area =624.40000
wing_span =69.70000
wing_root_chord =9.41000
wing_dihedral =3.00000
wing_incidence =2.00000
wing_twist =0.00000
oswald_efficiency_factor=0.78500
wing_winglets_flag =1
wing_sweep =27.00000
wing_pos_apex_lon =-38.72832
wing_pos_apex_vert =0.00000
htail_area =121.00000
htail_span =24.33000
htail_pos_lon =-74.45000
htail_pos_vert =12.70000
htail_incidence =0.00000
htail_sweep =35.00000
vtail_area =108.00000
vtail_span =11.60000
vtail_sweep =44.00000
vtail_pos_lon =-70.00000
vtail_pos_vert =3.70000
elevator_area =42.10000
aileron_area =22.00000
rudder_area =21.40000
elevator_up_limit =28.00000
elevator_down_limit =20.00000
aileron_up_limit =18.00000
aileron_down_limit =18.00000
rudder_limit =30.00000
elevator_trim_limit =15.00000
spoiler_limit =60.00000
spoiler_extension_time =2.00000
spoilerons_available =1
aileron_to_spoileron_gain =4.60000
min_ailerons_for_spoilerons =5.00000
min_flaps_for_spoilerons=0.00000
auto_spoiler_available =1
positive_g_limit_flaps_up =3.00000
positive_g_limit_flaps_down=2.10000
negative_g_limit_flaps_up =-2.40000
negative_g_limit_flaps_down=-1.80000
load_safety_factor =1.50000
spoiler_handle_available=1
[Flaps.0]
type= 1
system_type=0
span-outboard= 0.500
extending-time= 5.0
damaging-speed=297.0
blowout-speed=330.0
flaps-position.0=0.00
flaps-position.1=11.25
flaps-position.2=22.50
flaps-position.3=33.75
flaps-position.4=45.00
lift_scalar=1.30
drag_scalar=1.20
pitch_scalar=0.00
[Flaps.1]
type= 1
system_type=0
span-outboard= 0.500
extending-time= 5.0
damaging-speed=297.0
blowout-speed=330.0
flaps-position.0=0.00
flaps-position.1=11.25
flaps-position.2=22.50
flaps-position.3=33.75
flaps-position.4=45.00
lift_scalar=1.30
drag_scalar=1.20
pitch_scalar=0.00
[Reference Speeds]
flaps_up_stall_speed = 112.0 //Knots True (KTAS)
full_flaps_stall_speed = 102.0 //Knots True (KTAS)
cruise_speed =280.00000
max_mach =0.83000
max_indicated_speed =335.00000
[flight_tuning]
cruise_lift_scalar =1.80000
parasite_drag_scalar =1.00000
induced_drag_scalar =1.00000
elevator_effectiveness =1.00000
aileron_effectiveness =1.00000
rudder_effectiveness =1.00000
pitch_stability =1.00000
roll_stability =1.00000
yaw_stability =1.00000
elevator_trim_effectiveness =1.00000
aileron_trim_effectiveness =1.00000
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 =-74.000, -7.500, -0.000
Engine.1 =-74.000, 7.500, -0.000
fuel_flow_scalar=0.7500
min_throttle_limit =-0.25000
max_contrail_temperature = -25.00
[TurbineEngineData]
bypass_ratio=5.370
fuel_flow_gain=0.00300
inlet_area=3.96320
rated_N2_rpm=22920.00000
static_thrust=7926.50000
afterburner_available=0
reverser_available=1
afterburner_throttle_threshold=0.00000
ThrustSpecificFuelConsumption=0.00000
AfterBurnThrustSpecificFuelConsumption=0.00000
[jet_engine]
thrust_scalar =1.00000
[fuel]
Center1 = -49.700, 0.000, -4.000, 700.000, 0.000
LeftMain = -49.700, -7.700, -3.500, 600.000, 0.000
RightMain = -49.700, 7.700, -3.500, 600.000, 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
[contact_points]
static_pitch = -0.600
static_cg_height = 4.860
gear_system_type=1
emergency_extension_type=2 //None=0,Pump=1,Gravity=2
max_number_of_points=10
tailwheel_lock=0
//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
point.0= 1, -4.488, 0.000, -5.565, 2600, 0, 1.363, 65.800, 0.410, 2.500, 0.550, 10.000, 10.000, 0, 260.0, 260.0
point.1= 1, -52.488, -6.760, -5.790, 2600, 1, 1.800, 0.000, 1.000, 2.500, 0.650, 9.000, 9.000, 2, 260.0, 260.0
point.2= 1, -52.488, 6.760, -5.790, 2600, 2, 1.800, 0.000, 1.000, 2.500, 0.650, 9.000, 9.000, 3, 260.0, 260.0
point.3= 2, -65.000, -39.000, 0.000, 1000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -65.000, 39.000, 0.000, 1000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -43.000, 0.000, -3.800, 1000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, -98.000, 0.000, 16.000, 1000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.7= 2, -8.000, 0.000, -2.000, 1000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.8= 2, -80.000, 0.000, -1.500, 1000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.9= 5, 23.030, 0.000, -1.500, 1787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
[gear_warning_system]
gear_warning_available =1
pct_throttle_limit =0.10000
flap_limit_idle =15.00000
flap_limit_power =30.00000
[brakes]
parking_brake =1
toe_brakes_scale =1.20000
auto_brakes =0
hydraulic_system_scalar =1.00000
differential_braking_scale=0.00000
[electrical]
max_battery_voltage=24
generator_alternator_voltage=26
max_generator_alternator_amps=100
electric_always_available=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
[hydraulic_system]
normal_pressure=3000.00000
electric_pumps=0 //electric pumps enabled
engine_map=1,1,0,0 //pumps on Eng1,2
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
pitot_heat=1.000000
[stall_warning]
type=2
stick_shaker=1
[deice_system]
structural_deice_type=0
[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
//[airspeed_indicators]
//airspeed_indicator.0=1
//airspeed_indicator.1=1
[altimeters]
altimeter.0=1
altimeter.1=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[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
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm =95
autothrottle_takeoff_ga=0
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=30
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=11
nav_integrator_control=0.2
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain =1
default_pitch_mode=0
default_bank_mode=0
use_no_default_bank=1
use_no_default_pitch=1
[Views]
eyepoint = -17.1, -1.65, 4.00
[exits]
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 0.4
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -60.700000, -33.000000, -0.500000, fx_navredm
light.1 =3, -60.700000, 33.000000, -0.500000, fx_navgrem
light.2 =3, -86.520000, 0.000000, 4.300000, fx_navwhi
light.3 =4, -18.000000, 0.000000, 3.300000, fx_vclighth
//light.4 =2, 104.630000, 0.000000, 15.000000, fx_strobe
light.5 =1, -86.000000, 0.000000, 15.500000, fx_beaconh
//light.6 =4, -18.000000, 0.000000, 4.500000, fx_beaconh
light.7 =2, -62.000000, -34.500000, -0.500000, fx_strobe
light.8 =2, -62.200000, 34.500000, -0.500000, fx_strobe
light.9=4, -33.000000, 0.000000, 5.000000, fx_vclighth
light.10=4, -48.000000, 0.000000, 5.000000, fx_vclighth
[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_tchdwnCX, 1
touchdown=fx_tchdwn_s, 1
[forcefeedback]
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
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
[GPWS]
max_warning_height=1500
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100