// CRJ700-ER series 705 for FS2004 by Jean-Pierre Brisard and Barry Blaisdell // FSDS2.24 design. Version 4.5.1 ALLIANCE // Panel and VC by JP Brisard, B. Blaisedell // Paint by Bob May // Copyright 2004 //----------------------------------------------------------- [fltsim.0] title=crj700all45 sim=crj700er model= panel=ALL_CPQ sound= texture=ALL_CPQ kb_checklists=crj700_check kb_reference=crj700_ref atc_id=D-ACPQ atc_airline=LUFTHANSA atc_flight_number=1126 description=FS2004 Bombardier CRJ700-ER\nLufthansa Alliance\nD-ACPQ - A/C# 10091\nA 75 seat, Twin Turbofan Regional Jetliner.\nvisit the Premier Aircraft Design Website: \nwww.premaircraft.com\nAll Files Copyright 2004 by Premier Aircraft Design. ui_manufacturer=Bombardier ui_type=PAD_CRJ700-ER ui_variation=Lufthansa Alliance D-ACPQ atc_parking_types=gate,ramp atc_parking_codes=LUF [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\nAlliance 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, fx_strobeh , light.1=2, -11.4, 37.9, -2.4, fx_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 , [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