[fltsim.0] title=JODEL_D140E sim=Jodel_D140E model= panel= sound= texture= kb_checklists= kb_reference= atc_id=F-BNIZ ui_manufacturer=Jodel ui_type=D_140 E "Mousquetaire IV" ui_variation=aéroclub de Cormeilles description=A very popular aircraft in France, build for family-travel.\nBase on the Jodel aircraft by Joly and Delemontez, she was a five seats airplane, more powerfull. Her first fly was made on the 4th of July 1958.\nTo day, she always flew over French Alpes and other European countries, as Germany and England. atc_heavy=0 atc_airline=Privé atc_flight_number= [General] atc_type=JODEL atc_model=D 140E performance=Envergure : 10,27 m\nLongueur : 7,92 m\nSurface ailaire : 18,5 m2\nMasse à vide : 660 kg\nMasse maxi : 1200 kg\nMoteur : Lycoming O 360\nVitesse de décrochage : 88 km\/h\nVitesse d'approche : 115 km\/h\nVitesse de montée : 115 km\/h\nVitesse ascensionnelle : 3,6 m\/s\nVitesse maxi : 240 km\/h\nVitesse Croisière : 230 km\/h\nRéservoir AV : 90 l \nRéservoir AR : 125 l\nRayon d'action : 1700 kms\nNb de personnes : 4\/5 [WEIGHT_AND_BALANCE] max_gross_weight= 2450.000 empty_weight= 1550.000 reference_datum_position= 3.600, 0.000, 0.000 empty_weight_CG_position= -3.400, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, -3.500, -1.500, 0.000 station_load.1= 170.000, -3.500, 1.500, 0.000 station_load.2=0, -6.2, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI= 2200.000 empty_weight_roll_MOI= 1700.000 empty_weight_yaw_MOI= 2900.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 0 Engine.0= 8.200, 0.000, -0.500 fuel_flow_scalar= 1.000 [piston_engine] power_scalar=1.000 cylinder_displacement= 90.000 compression_ratio= 8.500 number_of_cylinders= 4 max_rated_rpm= 2800.000 max_rated_hp= 188.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 0 max_design_mp= 0.000 min_design_mp= 0.000 critical_altitude= 0.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [propeller] thrust_scalar=1.000 propeller_type= 1 propeller_diameter= 6.300 propeller_blades= 2 propeller_moi= 4.000 beta_max= 0.000 beta_min= 0.000 min_gov_rpm= 500.000 prop_tc= 0.000 gear_reduction_ratio= 1.000 fixed_pitch_beta= 18.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [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 //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 [contact_points] point.0= 1.000, -13.000, 0.000, -3.020, 1180.000, 0.000, 0.500, 22.000, 0.388, 2.500, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, 0.700, -4.500, -4.700, 1574.000, 1.000, 1.200, 0.000, 0.250, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, 0.700, 4.500, -4.700, 1574.000, 2.000, 1.200, 0.000, 0.250, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, -3.900, -18.000, 3.000, 1800.000, 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, -3.900, 18.000, 3.000, 1800.000, 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, -20.230, 0.000, 0.300, 1800.000, 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, 1.480, 0.000, -2.170, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.7= 2.000, -22.800, 0.000, 5.830, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 point.8= 2.000, -4.900, 0.000, -2.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 max_number_of_points=21 static_pitch= 6.120 static_cg_height= 2.650 [Views] eyepoint=-3.95, -0.85, 2.1 //(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 [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 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain= -3.900, -2.100, 2.500, 26.500, 0.000 RightMain= -3.900, 2.100, 2.500, 26.500, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 Center1= 3.700, 0.000, 0.000, 20.000, 0.000 Center2= -1.500, 0.000, -2.000, 26.500, 0.000 [airplane_geometry] wing_area= 163.000 wing_span= 33.690 wing_root_chord= 4.500 wing_dihedral= 1.500 wing_incidence= 3.500 wing_twist= -3.000 oswald_efficiency_factor= 0.720 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -2.400 wing_pos_apex_vert= 0.000 htail_area= 28.500 htail_span= 11.700 htail_pos_lon= -18.300 htail_pos_vert= 0.500 htail_incidence= 0.000 htail_sweep= 15.000 vtail_area= 18.000 vtail_span= 5.200 vtail_sweep= 20.000 vtail_pos_lon= -16.200 vtail_pos_vert= 1.500 elevator_area= 18.000 aileron_area= 22.300 rudder_area= 9.400 elevator_up_limit= 25.000 elevator_down_limit= 24.000 aileron_up_limit= 14.000 aileron_down_limit= 14.000 rudder_limit= 25.000 elevator_trim_limit= 20.000 spoiler_limit= 0.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [Reference Speeds] flaps_up_stall_speed= 54.000 full_flaps_stall_speed= 51.000 cruise_speed= 129.000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.000 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, 1.68, -17.05, -0.47, fx_navred light.1=3, 1.68, 17.05, -0.47, fx_navgre light.2=3,-16.25, 0.00, -0.52, fx_navwhih light.3=4, -15.15, 0.00, 5.05, fx_beacon light.4=2, -8.25, 0.00, 1.45, fx_strobe light.5=5, 2.98, -6.05, -1.40, fx_landing light.6=5, 2.98, -5.75, -1.40, fx_landing [exits] number_of_exits=2 exit_rate.0=0.5 ;Percent per second exit_rate.1=0.6 [Flaps.0] type= 1 span-outboard= 0.760 extending-time= 5.000 system_type= 3 damaging-speed= 120.000 blowout-speed= 150.000 lift_scalar= 8.000 drag_scalar= 0.500 pitch_scalar= 0.400 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 30.000, 0.000