[fltsim.0]
title=NC1071
sim=NC1071
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=SNCAC
ui_type=NC 1071
ui_variation=Prototype
description="SNCAC NC 1071, 1948"

[WEIGHT_AND_BALANCE]
empty_weight = 9192
reference_datum_position     =  0.0, 0, 0	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -0.065, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 200,  3.0, 0.0, 3.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI  = 12850
empty_weight_roll_MOI  = 7448
empty_weight_yaw_MOI  = 21800
empty_weight_coupled_MOI=0.000000
max_gross_weight=14088.000000

[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

[jet_engine]
thrust_scalar = 1.0

[exits]
number_of_exits = 1
exit_rate.0 = 0.4  				;Percent per second

[CameraDefinition.0]
Title=Train d'atterrissage
Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description=Vue du train d'atterrissage sous l'aile gauche
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.52
ShowWeather=Yes
InitialXyz=-2.2, -1.2, -7
InitialPbh=0, 0, 13
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title=Empennage
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Vue de l'arrière de l'avion
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.75
ShowWeather=Yes
InitialXyz=0, 2, -25.0
InitialPbh=5, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title=Aile droite
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Vue de droite
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=17, 1.6, -3.0
InitialPbh=6, 0, 280
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum

[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 160.0
;setting=BusType, MaxAmpLoad, MinVoltage
;where BusTypes: 0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 0.0
gear_motor=0, 5 , 0.0
autopilot=0, 5 , 0.0
avionics_bus=0, 10, 0.0
avionics=1, 5 , 0.0
pitot_heat=0, 2 , 0.0
additional_system=0, 20, 0.0
marker_beacon=1, 2 , 0.0
gear_warning=0, 2 , 0.0
fuel_pump=0, 5 , 0.0
starter1=0, 20, 0.0
light_nav=0, 5 , 0.0
light_beacon=0, 5 , 0.0
light_landing=0, 5 , 0.0
light_taxi=0, 5 , 0.0
light_strobe=0, 5 , 0.0
light_panel=0, 5 , 0.0

[contact_points]
	//0  Class
	//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, 10.8,   0.0, -6.1, 2200.0, 0, 1.0, 40.0, 0.29, 2.5, 0.95, 5.0, 5.0, 0, 330.0, 330.0     //nose wheel
point.1=1, -1.50, -4.5, -5.7, 2200.0, 1, 1.3,  0.0, 0.45, 2.5, 0.75, 5.0, 5.0, 2, 330.0, 330.0     //left wheel
point.2=1, -1.50,  4.5, -5.7, 2200.0, 2, 1.3,  0.0, 0.45, 2.5, 0.75, 5.0, 5.0, 3, 330.0, 330.0     //right wheel
point.3=2, -0.08,-19.9, -3.3, 1574.8, 0, 0.0,  0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 5      //left wing
point.4=2, -0.08, 19.9, -3.3, 1574.8, 0, 0.0,  0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 6      //right wing
point.5=2,-18.47,  0.0, -1.2, 1574.8, 0, 0.0,  0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 9 	        //tail
point.6=2, 10.08,  0.0, -1.7, 1574.8, 0, 0.0,  0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 4 	        //belly
static_pitch=1.3
static_cg_height=6.1
gear_system_type=1

[flaps.0]
type=1				// 1 - tail, 2 - lead
span-outboard=0.12		// 0.0 .. 1.0
extending-time=5			// seconds
flaps-position.0=0					// degrees, KIAS
flaps-position.1=14,330					// degrees, KIAS
flaps-position.2=28,260					// degrees, KIAS
flaps-position.3=42,210					// degrees, KIAS
flaps-position.4=55,170					// degrees, KIAS
damaging-speed=340					// KIAS
blowout-speed=380					// KIAS

[Views]
eyepoint=7.0,0.0,4.8

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 
//1  Longitudinal - minus rear        (feet)
//2  Lateral      - minus left        (feet)
//3  elevation    - minus lower        (feet)
light.0=3,  1.90, -32.95, 3.20, fx_navred
light.1=3,  1.90,  32.95, 3.20, fx_navgre
light.2=3,  -13.5,  -13.49,  8.7, fx_navwhi
light.3=3,  -13.5,  13.49,  8.7, fx_navwhi
light.4=4,  7.88,  0.00, 4.71, fx_vclight

[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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

[General]
performance=SNCAC NC1071\nFrench\n3 seat\nLength: 10.75 m (35 ft 3 in)\nSpan: 20.00 m (65 ft 7 in)\nEmpty weight: 7,980 kg (17,593 lb)\nMax weight: 13,750 kg (30,314 lb)\nMax speed: 800 km/h (497 mph)\nCruise speed: 724 km/h (450 mph)\nEngines : 2 x 2350kg Hispano-Suiza Rolls-Royce Nene 101 \n1st flight : October 12th, 1948. 

[fuel]
Center1=4.000000,0.000000,-1.000000,240.000000,0.000000
Center2=-1.000000,0.000000,-1.000000,53.000000,0.000000
Center3=-3.500000,0.000000,-1.000000,362.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=270.000000
wing_span=41.083333
wing_root_chord=6.583333
wing_dihedral=2.499390
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=0.891068
wing_winglets_flag=1
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=29.000000
htail_span=16.416667
htail_pos_lon=-19.083333
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=14.000000
vtail_span=4.266146
vtail_sweep=0.000000
vtail_pos_lon=-19.083333
vtail_pos_vert=6.166667
elevator_area=19.700000
aileron_area=23.800000
//rudder_area=10.700000
rudder_area=34.000000
elevator_up_limit=35.000000
elevator_down_limit=35.000000
aileron_up_limit=20.000000
aileron_down_limit=20.000000
rudder_limit=22.000000
elevator_trim_limit=35.000000
spoiler_limit=0.000000
spoilerons_available=1
aileron_to_spoileron_gain=4.600000
min_ailerons_for_spoilerons=4.984733
min_flaps_for_spoilerons=0.000000

[GeneralEngineData]
engine_type=1
Engine.0=0.083333,-8.166667,-0.333333
Engine.1=0.083333,8.166667,-0.333333
fuel_flow_scalar=1.000000
min_throttle_limit=-0.250000

[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=0.586462
rated_N2_rpm=9000.000000
//static_thrust=1984.000000
static_thrust=2500.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=120.000000
full_flaps_stall_speed=96.000000
cruise_speed=338.680853
max_indicated_speed=579.039063
max_mach=0.864746

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[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=6.000000
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=0.000000

[direction_indicators]
direction_indicator.0=3,0

[SMOKESYSTEM]
smoke.0=-8.9,-26.0,-8.5, fx_me262smoke                                                        
smoke.1=-8.9,-26.0,8.5,  fx_me262smoke

[brakes]
toe_brakes_scale=0.640889
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494

[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