// CRJ700-ER series 701 for FS2004 by Jean-Pierre Brisard and Barry Blaisdell
// FSDS2.24 design. Version 4.5.3.1 US Airways Express
// Panel and VC by JP Brisard, B. Blaisedell
// Paint by Bob May
// Copyright 2005
//-----------------------------------------------------------
[fltsim.0]
title=crj700uae4531
sim=crj700er
model=
panel=706
sound=
texture=706
kb_checklists=crj700_check
kb_reference=crj700_ref
atc_id=N706PS
atc_airline=US Air
atc_flight_number=706
description=FS2004 Bombardier CRJ700-ER series 701\nUS Airways Express\nN706PS - A/C# 10150\nA 70 seat, Twin Turbofan Regional Jetliner.\nvisit the Premier Aircraft Design Website: \nwww.flightsimnetwork.com\premaircraft\nAll Files Copyright 2005 by Premier Aircraft Design.
ui_manufacturer=Bombardier
ui_type=PAD_CRJ700-ER
ui_variation=US Airways Express w/o GPWS
atc_parking_types=gate,ramp
atc_parking_codes=USA, USAX
[fltsim.1]
title=crj700uae4532
sim=crj700er
model=
panel=706GPWS
sound=
texture=706
kb_checklists=crj700_check
kb_reference=crj700_ref
atc_id=N706PS
atc_airline=US Air
atc_flight_number=706
description=FS2004 Bombardier CRJ700-ER series 701\nUS Airways Express\nN706PS - A/C# 10150\nA 70 seat, Twin Turbofan Regional Jetliner.\nvisit the Premier Aircraft Design Website: \nwww.flightsimnetwork.com\premaircraft\nAll Files Copyright 2005 by Premier Aircraft Design.
ui_manufacturer=Bombardier
ui_type=PAD_CRJ700-ER
ui_variation=US Airways Express with GPWS
atc_parking_types=gate,ramp
atc_parking_codes=USA, USAX
[General]
performance=Length: 106 ft 8 in\nWing Span: 76 ft 3 in\nHeight: 24 ft 10 in\nRange-2,005 nm \/ Max ROC 1,950 fpm@SL\nWeight:75,000 lbs MTOW \/ Stall: 130\/104\nPower:2 x 12,670 lb thrust GE CF34-8C1 turbofans\nMax cruise .83 Mach @ 37,000 Feet\nDetails: 70 Passenger Regional Airliner\nDesigner: Jean-Pierre Brisard\nFD Designer: Barry Blaisdell\nPanel/VC by Jean-Pierre Brisard & Barry Blaisdell\nMaster Textures: Jean-Pierre Brisard\nFactory Paint: Bob May
atc_type=BOMBARDIER
atc_model=CARJ
editable=1
[fltsim.2]
title=crj700uae4533
sim=crj700er
model=
panel=706
sound=
texture=708
kb_checklists=crj700_check
kb_reference=crj700_ref
atc_id=N708PS
atc_airline=US Air
atc_flight_number=708
description=FS2004 Bombardier CRJ700-ER series 701\nUS Airways Express Alliance\nN708PS - A/C# 10160\nA 70 seat, Twin Turbofan Regional Jetliner.\nvisit the Premier Aircraft Design Website: \nwww.flightsimnetwork.com\premaircraft\nAll Files Copyright 2005 by Premier Aircraft Design.
ui_manufacturer=Bombardier
ui_type=PAD_CRJ700-ER
ui_variation=US Airways Express Alliance w/o GPWS
atc_parking_types=gate,ramp
atc_parking_codes=USA, USAX
[fltsim.3]
title=crj700uae4534
sim=crj700er
model=
panel=706GPWS
sound=
texture=708
kb_checklists=crj700_check
kb_reference=crj700_ref
atc_id=N708PS
atc_airline=US Air
atc_flight_number=708
description=FS2004 Bombardier CRJ700-ER series 701\nUS Airways Express Alliance\nN708PS - A/C# 10160\nA 70 seat, Twin Turbofan Regional Jetliner.\nvisit the Premier Aircraft Design Website: \nwww.flightsimnetwork.com\premaircraft\nAll Files Copyright 2005 by Premier Aircraft Design.
ui_manufacturer=Bombardier
ui_type=PAD_CRJ700-ER
ui_variation=US Airways Express Alliance with GPWS
atc_parking_types=gate,ramp
atc_parking_codes=USA, USAX
[General]
performance=Length: 106 ft 8 in\nWing Span: 76 ft 3 in\nHeight: 24 ft 10 in\nRange-2,005 nm \/ Max ROC 1,950 fpm@SL\nWeight:75,000 lbs MTOW \/ Stall: 130\/104\nPower:2 x 12,670 lb thrust GE CF34-8C1 turbofans\nMax cruise .83 Mach @ 37,000 Feet\nDetails: 70 Passenger Regional Airliner\nDesigner: Jean-Pierre Brisard\nFD Designer: Barry Blaisdell\nPanel/VC by Jean-Pierre Brisard & Barry Blaisdell\nMaster Textures: Jean-Pierre Brisard\nFactory Paint: Bob May
atc_type=BOMBARDIER
atc_model=CARJ
editable=1
[Views]
eyepoint=38.450, -2.170, 1.260
[weight_and_balance]
max_gross_weight=75250.000
empty_weight=43500.000
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
empty_weight_pitch_MOI=1038638.000
empty_weight_roll_MOI=153909.000
empty_weight_yaw_MOI=882504.000
empty_weight_coupled_MOI=4305.000
max_number_of_stations=10
station_load.0= 9000.000, 0.000, 0.000, 0.000
CG_forward_limit=0.000
CG_aft_limit=1.000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=2, -11.4, -37.9, -2.4, crj9fx_strobeh ,
light.1=2, -11.4, 37.9, -2.4, crj9fx_strobeh ,
light.2=1, 17.71 , 0.00, 3.6, fx_beaconh ,
light.3=1, 17.71 , 0.00, -5.085, fx_beaconh ,
light.4=4, 42.2, 0.00, 0.07, fx_vclighth ,
light.5=2, -53.20, 0.00, 12.000, fx_strobeh ,
light.6=3, -11.5, -38.2, -2.4, crj9fx_navred ,
light.7=3, -11.5, 38.2, -2.4, crj9fx_navgre ,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type=1
fuel_flow_scalar=0.950
engine.0=-14.583, -5.083, 2.167
engine.1=-14.583, 5.083, 2.167
min_throttle_limit=-0.300
[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
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2
number_of_tank_selectors=1
Center1 = 0, 0, 0, 1580, 0
LeftMain=0.000, -10.000, 0.000, 720.000, 0.000
RightMain=0.000, 10.000, 0.000, 720.000, 0.000
electric_pump=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)
point.0=1.000, 43.800, 0.000, -8.100, 1474.803, 0.000, 1.022, 55.000, 0.508, 3.500, 0.455, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1.000, -3.000, -7.083, -9.300, 1574.803, 1.000, 2.358, 0.000, 0.976, 2.500, 0.861, 6.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, -3.000, 7.083, -9.300, 1574.803, 2.000, 2.358, 0.000, 0.976, 2.500, 0.861, 6.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -12.333, -35.333, 2.167, 774.803, 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, -12.333, 35.333, 2.167, 774.803, 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, -38.333, 0.000, -1.083, 774.803, 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, 35.333, 0.000, -1.083, 774.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.500
static_cg_height=7.800
gear_system_type=1 //Hydraulic
[keyboard_response]
elevator=150.000000, 250.000000
aileron=150.000000, 250.000000
rudder=150.000000, 250.000000
[forcefeedback]
gear_bump_nose_magnitude=3000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=2700
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=2700
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=1300
ground_bumps_angle1=08900
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200
ground_bumps_angle2=09100
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
[airplane_geometry]
wing_area=740.000
wing_span=76.250
wing_root_chord=9.690
wing_dihedral=3.329
wing_incidence=2.673
wing_twist=-0.494
oswald_efficiency_factor=0.764
wing_winglets_flag=1
wing_sweep=20.000
wing_pos_apex_lon=1.000
wing_pos_apex_vert=0.000
htail_area=245.000
htail_span=22.333
htail_pos_lon=-43.333
htail_pos_vert=5.000
htail_incidence=0.000
htail_sweep=20.000
vtail_area=191.000
vtail_span=15.758
vtail_sweep=10.000
vtail_pos_lon=-47.917
vtail_pos_vert=5.833
elevator_area=57.500
aileron_area=25.000
rudder_area=32.300
elevator_up_limit=27.502
elevator_down_limit=20.626
aileron_up_limit=19.481
aileron_down_limit=14.897
rudder_limit=23.491
elevator_trim_limit=19.481
spoiler_limit=59.989
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000
spoilerons_available=0
[electrical]
max_battery_voltage=36.0
generator_alternator_voltage=36.0
max_generator_alternator_amps=160.0
electric_always_available=0
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
//BusType, MaxAmpLoad, MinVoltage
autopilot = 0, 5 , 1.0
avionics_bus = 0, 10, 10.0
avionics = 1, 5 , 10.0
gear_warning = 0, 2 , 1.0
fuel_pump = 0, 5 , 1.0
light_nav = 0, 5 , 1.0
light_beacon = 0, 5 , 1.0
light_landing = 0, 5 , 7.0
light_taxi = 0, 5 , 7.0
light_strobe = 0, 5 , 7.0
light_panel = 0, 5 , 1.0
pitot_heat = 0, 15, 1.0
additional_system = 0, 20, 1.0
marker_beacon = 1, 2, 1.0
starter1 = 0, 20, 1.0
starter2 = 0, 20, 1.0
auto_brakes = 0, 15, 1.0
hydraulic_pump = 0, 2, 1.0
fuel_transfer_pump = 0, 5, 1.0
[brakes]
toe_brakes_scale=0.450697
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=14.750
rated_N2_rpm=29920.000
static_thrust=15000.00
afterburner_available=0
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed=121.000
full_flaps_stall_speed=105.000
cruise_speed=450.000
max_indicated_speed=380.000000
max_mach=0.8700
[pitot_static]
vertical_speed_time_constant=10
[autopilot]
autopilot_available=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=10.000000
use_no_default_pitch=1
use_no_default_bank=1
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
default_pitch_mode=0
default_bank_mode=0
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
max_pitch=10.000000
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=3,0
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 -
lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 15 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 8 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 30 // degrees
flaps-position.4 = 45 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.000
drag_scalar = 1.000
pitch_scalar= 1.0000
system_type = 1 //Hydraulic
[flaps.1] //Inboard Leading Edge Slat
type = 2 // 1 - tail, 2 -
lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 3 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.000
drag_scalar = 1.000
pitch_scalar= 1.000
system_type = 1 //Hydraulic
[flaps.2] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 -
lead
span-outboard = 0.5 // 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 = 1.000
drag_scalar = 1.000
pitch_scalar= 1.000
system_type = 1 //Hydraulic
[jet_engine]
thrust_scalar=1.000
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
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
