[fltsim.0] title= SE 210 Caravelle Mark III sim=caravelle model= panel= sound= texture=transavia panel_alias = sound_alias = kb_checklists= kb_reference= atc_id=NTEJ atc_id_color=0xffffffff atc_airline= atc_flight_number=0001 ui_manufacturer=Sud Aviation ui_type=Caravelle SE 210 Mark III ui_variation=Transavia description= Transavia purchased the PH-TRR from Swissair. In service from March 1970 till February 1975. Scraped in February 1976 at Schiphol Airport, Amsterdam. Original model by Mike Stone, repaint by Hans van Spelde(2012) atc_heavy=0 [General] atc_type=Caravelle atc_model= editable=1 performance=Wing span: 34.20 m, Length: 32.01 m, Height: 8.72 m, Powerplant: 2 Rolls Royce Avon RA.29 MK 527 of 5,170 kg thrust, Max: speed: 860 km/u, Cruising spee: 805 km/u, Range: 2,700 km, Pax: 94 [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight = 101411.000 empty_weight = 53318.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 max_number_of_stations =50 ;Moments of Inertia empty_weight_pitch_MOI = 2400000.000 empty_weight_roll_MOI = 700000.000 empty_weight_yaw_MOI = 2000000.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 station_load.0=0.000000,0.000000,0.000000,0.000000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =0.509 aileron_effectiveness =1.000 rudder_effectiveness =1.000 pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =0.509 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [GeneralEngineData] engine_type = 1 Engine.0 = -29.000, -8.000, 0.000 Engine.1 = -29.000, 8.000, 0.000 fuel_flow_scalar = 1.000 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 15.000 rated_N2_rpm = 29920.000 static_thrust = 12400.000 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar =1.000 [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, 10, 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 20, 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] point.0= 1.000, 40.000, 0.000, -8.300, 1181.100, 0.000, 1.442, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000 point.1= 1.000, -7.750, -8.580, -8.800, 1574.800, 1.000, 1.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000 point.2= 1.000, -7.750, 8.580, -8.800, 1574.800, 2.000, 1.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000 point.3= 2.000, -14.170, -47.330, 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, -14.170, 47.330, 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, -54.000, 0.000, 2.830, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points = 21 static_pitch= 0.620 static_cg_height= 7.900 gear_system_type=0 [Views] eyepoint=43.7, -1.31, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum [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, -14.45, -55.51, -0.03, fx_navredm , light.1 = 3, -14.45, 55.51, -0.03, fx_navgrem , light.2 = 2, -14.35, -55.51, -0.03, fx_strobeh , light.3 = 2, -14.35, 55.51, -0.03, fx_strobeh , light.4 = 1, -52.52, 0.00, 22.75, fx_beaconh , light.5 = 4, 43.77, 0.00, 4.50, fx_vclight , [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 [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=10.000000 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 [fuel] Center1 = 0.000, 0.000, 0.000, 1800.000, 0.000 LeftMain = -3.000, -19.000, 0.000, 1200.000, 0.000 RightMain = -3.000, 19.000, 0.000, 1200.000, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 1400.000 wing_span = 110.000 wing_root_chord = 20.000 wing_dihedral = 4.000 wing_incidence = 0.000 wing_twist = -0.500 oswald_efficiency_factor= 0.750 wing_winglets_flag = 0 wing_sweep = 25.000 wing_pos_apex_lon = 8.000 wing_pos_apex_vert = 0.000 htail_area = 342.000 htail_span = 36.000 htail_pos_lon = -42.000 htail_pos_vert = 10.000 htail_incidence = 0.000 htail_sweep = 30.000 vtail_area = 220.000 vtail_span = 17.000 vtail_sweep = 40.000 vtail_pos_lon = -46.000 vtail_pos_vert = 6.000 elevator_area = 72.000 aileron_area = 34.000 rudder_area = 42.000 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 = 3.000 min_ailerons_for_spoilerons = 10.000 min_flaps_for_spoilerons = 0.000 [Reference Speeds] flaps_up_stall_speed = 142.000 full_flaps_stall_speed = 113.000 cruise_speed = 477.000 max_indicated_speed=340.000000 max_mach=0.820020 [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 [Flaps.0] type= 1 span-outboard= 0.700 extending-time= 8.000 system_type= 1 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= 1.000, 0.000 flaps-position.2= 2.000, 0.000 flaps-position.3= 5.000, 0.000 flaps-position.4= 10.000, 0.000 flaps-position.5= 15.000, 0.000 flaps-position.6= 25.000, 0.000 flaps-position.7= 30.000, 0.000 flaps-position.8= 40.000, 0.000 [brakes] toe_brakes_scale=0.885037 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0