[fltsim.0] title=DH106 Comet sim=RAECOM4C panel= model= sound= texture= checklists= description=DH106 Comet 4C XS235 'Canopus' was delivered new to the Royal Aircraft Establishment in 1963 & served until 1997.\nIt was the last airworthy Comet & is still kept in working order at Bruntingthorpe. It is planned that it will fly again soon after a full restoration by the National Air Pageant.\nSee website www.cometcampaign.cjb.net for more info. ui_manufacturer=deHavilland ui_type=DH 106 Comet ui_variation=Olympic Airways atc_heavy=0 atc_id= atc_airline=Olympic atc_flight_number= visual_damage=1 [fltsim.1] title=DH106 Comet 4C Dan-Air sim=RAECOM4C model= panel= sound= texture=DAN checklists= ui_manufacturer=DeHavilland ui_type=DH 106 Comet ui_variation=DAN-AIR London atc_id=G-BDIT atc_airline=Dan-Air London atc_flight_number=1123 description=The first trans atlantic jet airliner. atc_heavy=1 visual_damage=1 [General] performance=Length: 118 ft\nSpan: 114 ft 10in\nEngines: Rolls-Royce Avon RA.20 Mk 525\n\nModel & Animation by David Maltby\nCheck for updates at the website\nwww.Maltbyd.fsnet.co.uk\nPainted by David Maltby\n\n atc_type=DeHallivand atc_model=DH 106 [forcefeedback] 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=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 empty_weight= 130000.000 empty_weight_roll_MOI= 5000000.000 empty_weight_pitch_MOI= 8000000.000 empty_weight_yaw_MOI= 6000000.000 empty_weight_coupled_MOI= 10000.000 max_gross_weight= 195000.000 max_number_of_stations= 50 station_load.0= 0.000, 0.000, 0.000, 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= 0.000, 0.000, 0.000, 3200.000, 0.000 LeftMain= 0.000, 15.000, 0.000, 3200.000, 0.000 RightMain= 0.000, -15.000, 0.000, 3200.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area= 2000.000 wing_span= 107.000 wing_root_chord= 22.000 wing_dihedral= 2.197 wing_incidence= 0.000 wing_twist= 2.999 oswald_efficiency_factor= 13.348 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 580.000 htail_span= 31.667 htail_pos_lon= -56.500 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 400.000 vtail_span= 22.804 vtail_sweep= 0.000 vtail_pos_lon= -54.167 vtail_pos_vert= 21.667 elevator_area= 60.000 aileron_area= 56.000 rudder_area= 60.000 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 20.054 aileron_down_limit= 20.054 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, 48.333, 0.000, -8.333, 1574.803, 0.000, 2.005, 64.800, 0.236, 2.500, 0.778, 9.000, 9.000, 0.000, 0.000, 0.000 point.1= 1.000, -5.333, -15.250, -8.583, 1574.803, 1.000, 2.005, 0.000, 0.493, 2.500, 0.497, 11.000, 11.000, 2.000, 0.000, 0.000 point.2= 1.000, -5.333, 15.250, -8.583, 1574.803, 2.000, 2.005, 0.000, 0.493, 2.500, 0.497, 12.000, 12.000, 3.000, 0.000, 0.000 point.3= 2.000, -14.750, -56.500, 1.333, 1501.849, 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, -14.750, 56.500, 1.333, 1501.849, 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, -59.250, 0.083, 3.917, 1501.849, 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, 57.250, 0.000, -0.250, 1501.849, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -0.264 static_cg_height= 8.168 gear_system_type=0 [brakes] toe_brakes_scale=0.549333 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 [GeneralEngineData] engine_type= 1 Engine.0= -8.333, -11.000, 0.000 Engine.1= -8.333, -15.583, 0.000 Engine.2= -8.333, 11.000, 0.000 Engine.3= -8.333, 15.583, 0.000 fuel_flow_scalar= 1.000 min_throttle_limit=-0.079956 [SMOKESYSTEM] smoke.0=0.000, -8.333, -11.000, fx_smoke_rx smoke.1=0.000, -8.333, -15.583, fx_smoke_rx, smoke.2=0.000, -8.333, 11.000, fx_smoke_rx, smoke.3=0.000, -8.333, 15.583, fx_smoke_rx, [TurbineEngineData] fuel_flow_gain= 0.003 inlet_area= 3.000 rated_N2_rpm= 30000.000 static_thrust= 10500.000 afterburner_available= 0 reverser_available= 0 [Reference Speeds] flaps_up_stall_speed= 100.000 full_flaps_stall_speed= 80.000 cruise_speed= 250.000 max_indicated_speed=600.000000 max_mach=0.860010 [keyboard_response] elevator=100.000000,200.000000 aileron=100.000000,200.000000 rudder=100.000000,200.000000 [Views] eyepoint=51.404097,-1.166236,3.280840 [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=1200.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 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=1.000000 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.000000 [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] type= 1 span-outboard= 0.500 extending-time= 18.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 13.331, 0.000 flaps-position.2= 26.662, 0.000 flaps-position.3= 39.992, 0.000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -14.14, -56.24, 1.38, fx_navredm , light.1 = 3, -14.14, 56.24, 1.38, fx_navgrem , light.2 = 3, -60.00, 0.00, 4.00, fx_navwhih , light.3 = 2, -14.22, -56.08, 1.38, fx_strobeh , light.4 = 2, -14.22, 56.08, 1.38, fx_strobeh , light.5 = 2, 9.00, 0.00, -3.60, fx_beaconb , light.6 = 1, 9.00, 0.00, 7.30, fx_beaconh , light.7 = 4, 44.41, 0.00, 3.50, fx_vclighth ,