[fltsim.0]
title=Project SkyWorks CRJ-700 Paint Kit
sim=BombardierCRJ-700
model=
panel=
sound=
texture=paintkit
kb_checklists=BombardierCRJ-700_check
kb_reference=BombardierCRJ-700_ref
atc_id=
atc_airline=
atc_flight_number=
ui_manufacturer=Bombardier
ui_type="CRJ-700"
ui_variation="Paint Kit"
description="Welcome to Project SkyWorks's Canadair CRJ-700. We hope you enjoy flying it as much as we did designing the whole project. Below is our CRJ-700 Team :
Model Designer & Executive Painter :
Massimo Altieri
Panel Designers :
Paul Scarratt & Ken Mitchell
Sound Technician :
Leon Medado
Aircraft Painters :
Dirk Kiefer, Fahim Safi & Tim Adams
Presentation Designer :
Cameron Dougall
Team Administrator :
James Jaw"
atc_parking_types=GATE,RAMP
[General]
atc_type=BOMBARDIER
atc_model=CARJ
editable=0
performance="High Cruise Speed\n0.83 Mach\n\nCruise Speed\n0.78 Mach\n\nEngines\nGeneral Electric CF34-8C5\n\nMax Range\n2.062 NM\n\nService Ceiling\n41.000 Ft\n\nMax Fuel Load\n19.450 Lbs\n\nEmpty Weight\n47.100 Lbs\n\nMax Weight\n82.750 Lbs\n\nLength \n119,4 ft\n\nWing Span\n76,3 Ft\n\nEight\n24,7 Ft\n\nSeats\n70 to 75"
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
reference_datum_position = 0.000, 0.000, 0.000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.000, 0.000, 0.000 // (feet) longitudinal, lateral, vertical distance from specified datum
empty_weight = 43100 // (pounds)
empty_weight_pitch_MOI = 317243
empty_weight_roll_MOI = 160218
empty_weight_yaw_MOI = 433724
empty_weight_coupled_MOI = 0
max_gross_weight = 70750 // (pounds)
max_number_of_stations = 50
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.0 = 170.0, 41.0, -1.5, 0.0 // pilota
station_load.1 = 170.0, 41.0, 1.5, 0.0 // Copilota
station_load.3 = 1360.0, 25.5, 0.0, 0.0 // Prima classe
station_load.4 = 8160.0, 11.0, 0.0, 0.0 // Classe economica 3-10
station_load.5 = 8160.0, -10.0, 0.0, 0.0 // Classe economica 11-18
station_load.6 = 7140.0, -30.5, 0.0, 0.0 // Classe economica 19-25
[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
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -42.3, -7.5, 4.7 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -42.3, 7.5, 4.7 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1 //Scalar for fuel flow efficiency
min_throttle_limit = -0.35 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear
[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
bypass_ratio=4.890
inlet_area = 14.51 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920.000 //RPM, second stage compressor rated value
static_thrust = 14500.000 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2, 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 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
//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)
[contact_points]
// 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.0=1, 36.00, 0.00, -5.30, 1181.1, 0, 0.8, 55.92, 0.35, 2.5, 0.6, 4.0, 4.0, 1, 250.0, 290.0
point.1=1, -4.00, -5.62, -5.95, 1574.8, 1, 0.8, 0.00, 0.35, 2.5, 0.6, 6.9, 6.5, 2, 250.0, 290.0
point.2=1, -4.00, 5.62, -5.95, 1574.8, 2, 0.8, 0.00, 0.35, 2.5, 0.6, 7.1, 6.5, 3, 250.0, 290.0
point.3=2, -18.5, -35.30, -1.28, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -18.5, 35.30, -1.28, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -50.70, 0.00, 3.24, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -50.90, 0.00, 15.31, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, 42.60, 0.00, -0.20, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
max_number_of_points = 21
static_pitch= -0.5 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=5.62 //feet, altitude of CG when at rest on the ground
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 = 5.0 //Flap angle that activates warning at idle
flap_limit_power = 25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.885 //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=32.5, -1.45, 3.73 //(feet) longitudinal, lateral, vertical distance from reference datum
[Flaps.0]
type=1
span-outboard=0.60000
extending-time=2.0000
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=10.00000,0.000000
flaps-position.2=20.00000,0.000000
flaps-position.3=30.00000,0.000000
flaps-position.4=35.00000,0.000000
drag_scalar=1.0
[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, 5=landing
light.0 = 3, -19.14, -35.30, -1.28, fx_navredm ,
light.1 = 3, -19.14, 35.30, -1.28, fx_navgrem ,
light.2 = 3, -50.72, 0.00, 3.24, fx_navwhih ,
light.3 = 2, -22.82, -36.00, 3.65, fx_strobeh ,
light.4 = 2, -22.82, 36.00, 3.65, fx_strobeh ,
light.5 = 2, -2.65, 0.00, -3.70, fx_beaconb ,
light.6 = 1, 2.20, 0.00, 6.20, fx_beaconh ,
light.7 = 4, 32.00, 0.00, 3.20, fx_vclighth ,
light.8 = 3, 0.00, -7.00, -1.50, fx_navwhih ,
light.9 = 3, 0.00, 7.00, -1.50, fx_navwhih ,
[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 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[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=10.0
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=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[fuel]
Center1 = 0, 0, 0, 1473, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -3, -19, 0, 737, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3, 19, 0, 737, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 859.0 //Square feet
wing_span = 76.25 //Feet
wing_root_chord = 16.29 //Feet
wing_dihedral = 3.8 //Degrees
wing_incidence = -1.0 //Degrees
wing_twist = -0.5 //Degrees
oswald_efficiency_factor= 1.85 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 19.0 //Degrees, wing leading edge
wing_pos_apex_lon = 1.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 227.0 //Square feet
htail_span = 28.0 //Feet
htail_pos_lon = -52.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 13.8 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 19.0 //Degrees, horizontal tail leading edge
vtail_area = 165.0 //Square feet
vtail_span = 12.8 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -36.8 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 6.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 70.5 //Square feet
aileron_area = 26.9 //Square feet
rudder_area = 56.2 //Square feet
elevator_up_limit = 24.5 //Degrees
elevator_down_limit = 19.5 //Degrees
aileron_up_limit = 24.0 //Degrees
aileron_down_limit = 22.0 //Degrees
rudder_limit = 26.0 //Degrees
elevator_trim_limit = 20.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 142.0 //Knots True (KTAS)
full_flaps_stall_speed = 113.0 //Knots True (KTAS)
cruise_speed = 502.0 //Knots True (KTAS)
max_mach = 0.90
max_indicated_speed = 400 //Red line (KIAS)
[forcefeedback]
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=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 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
