[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
