[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 ,