[fltsim.0]
title=DR400_F-GNNK
sim=DR400
model=
panel=
sound=
texture=
kb_checklists=DR400_check
kb_reference=DR400_ref
atc_id=F-GNNK
ui_manufacturer=Robin
ui_type=DR400
ui_variation=DR400 F-GNNK
visual_damage=0
description=La plupart des pilotes franзais on volй au moins quelques heures sur Robin DR 400,  c'est l'appareil le plus rйpandu dans les aйro-clubs et il est utilisй par la plupart des йcoles de pilotage. modйlisation FSDS ©Yannick Lavigne-Fred Banting-Rob Young - novembre 2002. Adaptation model visuel pour FS2004 par Eric Dantиs 02/2004. Adaptation modиle de vol pour FS2004 par Jean-Pierre Bourgeois 03/2004. Livrйe F-GNNK par Christian Daboudet.

[General]
editable=0
atc_type=Robin
atc_model=DR400
performance=Maximum Speed\t160 kts\nCruise Speed\t140 kts\nEngine\tLycoming O-360-A3A 180 hp\nPropeller\tTwo-bladed Sensenich Fixed\nMaximum Range\t757 nm\nService Ceiling\t15,500 ft\nFuel Capacity\t50 U.S gal\nMax Gross Weight\t2425 lbs\nLength\t\t23 ft, 3 in\nWingspan\t\t28 ft, 7 in\nHeight\t\t7 ft, 4 in\nSeating\t\t4\nUseful Load\t1019 lb\n

[WEIGHT_AND_BALANCE]
max_gross_weight=2425.0
empty_weight=1406.0

reference_datum_position=0.0, 0.0, 0.0
empty_weight_CG_position=0.0, 0.0, 0.0 //-0.55

max_number_of_stations=10
//MAX station loads (Including Fuel) 1019 lbs.
//Weight (lbs), long, lat, vert positions from datum (feet)
station_load.0=170.0, 1.0, 0.0, 0.0		//Pilot
station_load.1=170.0, 1.0, 0.0, 0.0		//Co Pilot
station_load.2=100.0, -2.0, 0.0, 0.0	//Rear Passenger
station_load.3=100.0, -2.0, 0.0, 0.0	//Rear Passenger
station_load.4=060.0, -4.4, 0.0, 0.0	//Baggage

//Moments of Inertia
empty_weight_pitch_MOI=2400.0 // 1400
empty_weight_roll_MOI=2200.0 // 1200
empty_weight_yaw_MOI=1226.0 // 2400
empty_weight_coupled_MOI=0.0
CG_forward_limit=0.0
CG_aft_limit=1.0


[Views]
eyepoint=-0.25, -0.85, 2.0	//(feet) longitudinal, lateral, vertical

[fuel]
Center1=-0.20,   0.0,  -1.7,  26.5,  0.0
LeftMain=-0.20,  -2.5,  -1.5,  10.5,  0.0
RightMain=-0.20,   2.5,   -1.5,  10.5,  0.0
fuel_type=1.0
number_of_tank_selectors=1
electric_pump=1

[electrical]
//BusType, MaxAmpLoad, MinVoltage
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
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
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

[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

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=0
autoland_available=0
pitch_takeoff_ga=5.0
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
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

[pitot_static]
vertical_speed_time_constant=0.7             

[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=0.8
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
p_factor_on_yaw=1.2
torque_on_roll=1.2
gyro_precession_on_roll=1.0
gyro_precession_on_yaw=1.0


[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=3,  0.324, -14.645, -0.241, dr_navred
light.1=3,  0.324,  14.645, -0.241, dr_navgre
light.2=1,-14.081,    0.00,  4.200, dr_navwhi
light.3=5,  1.847,  -7.972, -1.334, dr_landing.fx 
light.4=5,  1.847,  -7.562, -1.334, dr_landing.fx
light.5=2, -5.780,   0.000,  1.900, dr_strobe
light.6=4,  0.000,    0.000,  2.200, fx_vclight

[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=1,0

[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=100,  180
aileron=200, 1000
rudder=200, 1000

[effects]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[GeneralEngineData]
engine_type=0
Engine.0=6.5, 0.0, 0.0
fuel_flow_scalar=1.04
min_throttle_limit=0.000000

[piston_engine]
power_scalar=1.1
cylinder_displacement=90.0
compression_ratio=8.5
number_of_cylinders=4
max_rated_rpm=2700.0
max_rated_hp=180.0
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.1
turbocharged=0
max_design_mp=0.0
min_design_mp=0.0
critical_altitude=0.0
emergency_boost_type=0
emergency_boost_mp_offset=0.0
emergency_boost_gain_offset=0.0
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=1.0
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=1.6

[propeller]
thrust_scalar=0.81
propeller_type=1
propeller_diameter=6.5 // 6.33
propeller_blades=2
propeller_moi=2.2
beta_max=0.0
beta_min=0.0
min_gov_rpm=0.0
prop_tc=0.0
gear_reduction_ratio=1.0
fixed_pitch_beta=19.0
low_speed_theory_limit=80.0
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.0
beta_feather=0.0
power_absorbed_cf=0.0
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.0
minimum_reverse_beta=0.0

[flaps.0]
type=1					// 1 - trail, 2 - lead
span-outboard=0.56			// 0.0 .. 1.0
extending-time=3.0			// seconds
system_type=3				// 0=Elec, 1=Hyd, 2=Pneu, 3=Man, 4=None
flaps-position.0=0.0, 0.0		//Degrees
flaps-position.1=15.0, 0.0 //was 15.0 but needs more drag Degrees
flaps-position.2=60.0, 0.0		//Degrees
damaging-speed=120			//KIAS
blowout-speed=150				//KIAS

[reference speeds]
flaps_up_stall_speed=57.0		//Knots True (KTAS)
full_flaps_stall_speed=51.0		//Knots True (KTAS)
cruise_speed=140.0			//Knots True (KTAS)
max_indicated_speed=166.000000

[airplane_geometry]
wing_area=153.0
wing_span=28.58
wing_root_chord=6.16
wing_dihedral=2.0  //7.0
wing_incidence=4.6
wing_twist=-0.8  // -1.5
oswald_efficiency_factor=0.95// 0.6
wing_winglets_flag=0
wing_sweep=0.0
wing_pos_apex_lon=1.58
wing_pos_apex_vert=-1.3
htail_area=31.0
htail_span=10.50
htail_pos_lon=-12.3
htail_pos_vert=0.5
htail_incidence=2.0 // 2.2
htail_sweep=0.0
vtail_area=18.0
vtail_span=4.8
vtail_sweep=30.0
vtail_pos_lon=-13.3
vtail_pos_vert=1.66
elevator_area=16.6
aileron_area=12.26
rudder_area=6.78
elevator_up_limit=25.0
elevator_down_limit=24.0 // 16.0
aileron_up_limit=15.0
aileron_down_limit=12.0 //15.0
rudder_limit=25.0
elevator_trim_limit=20.0
spoiler_limit=0.0
spoilerons_available=0
aileron_to_spoileron_gain=0.0
min_ailerons_for_spoilerons=0.0
min_flaps_for_spoilerons=0.0

[contact_points]
//0  Class
//1  Longitudinal Position		(feet, +=fwd)
//2  Lateral Position			(feet, +=right)
//3  Vertical Position			(feet, +=above)
//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)
//       0     1      2     3     4      5    6    7     8     9   10   11   12   13   14   15
point.0=1.0,  4.4,  0.0, -3.90, 1500.0, 0.0, 0.5, 29.0, 0.18, 1.5, 1.0, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=1.0, -1.5, -4.5, -4.00, 3000.0, 1.0, 0.5, 0.0,  0.25, 1.5, 0.8, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1.0, -1.5,  4.5, -4.00, 3000.0, 2.0, 0.5, 0.0,  0.25, 1.5, 0.8, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=2.0,  0.0,-14.1, -0.75, 1200.0, 0.0, 0.0, 0.0,  0.0,  0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2.0,  0.0, 14.1, -0.75, 1200.0, 0.0, 0.0, 0.0,  0.0,  0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2.0,-14.5,  0.0, -1.0,  1200.0, 0.0, 0.0, 0.0,  0.0,  0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2.0,  5.8,  0.0, -1.2,  1200.0, 0.0, 0.0, 0.0,  0.0,  0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0
point.7=2.0,-16.3,  0.0,  4.0,  1200.0, 0.0, 0.0, 0.0,  0.0,  0.0, 0.0, 0.0, 0.0, 7.0, 0.0, 0.0
max_number_of_points=10
static_pitch=-0.7			//degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=3.65		//feet, altitude of CG when at rest on the ground


//       0     1      2     3     4      5    6    7     8     9   10   11   12   13   14   15
//point.0=1.0,  4.0,  0.0, -3.95, 1500.0, 0.0, 0.5, 29.0, 0.15, 2.5, 0.8, 0.0, 0.0, 0.0, 0.0, 0.0
//point.1=1.0, -1.5, -4.5, -4.06, 3000.0, 1.0, 0.5, 0.0,  0.25, 2.5, 0.8, 0.0, 0.0, 2.0, 0.0, 0.0
//point.2=1.0, -1.5,  4.5, -4.06, 3000.0, 2.0, 0.5, 0.0,  0.25, 2.5, 0.8, 0.0, 0.0, 3.0, 0.0, 0.0
//point.3=2.0,  0.0,-14.1, -0.75, 1200.0, 0.0, 0.0, 0.0,  0.0,  0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
//point.4=2.0,  0.0, 14.1, -0.75, 1200.0, 0.0, 0.0, 0.0,  0.0,  0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
//point.5=2.0,-14.5,  0.0, -1.0,  1200.0, 0.0, 0.0, 0.0,  0.0,  0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
//point.6=2.0,  5.8,  0.0, -1.2,  1200.0, 0.0, 0.0, 0.0,  0.0,  0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0
//point.7=2.0,-16.3,  0.0,  4.0,  1200.0, 0.0, 0.0, 0.0,  0.0,  0.0, 0.0, 0.0, 0.0, 7.0, 0.0, 0.0
//max_number_of_points=10
//static_pitch=-0.7			//degrees, pitch when at rest on the ground (+=Up, -=Dn)
//static_cg_height=3.55		//feet, altitude of CG when at rest on the ground


[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

[brakes]
toe_brakes_scale=0.543229
parking_brake=1

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0