[fltsim.0]
title=JODEL_D120
sim=Jodel_D120
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=F-BIRR
ui_manufacturer=Jodel
ui_type=D_120
ui_variation=WASSMER Aviation
description=A very popular aircraft in France, build by WASSMER Aviation at Issoudun (France), this is a more comfortable version of the D 112, use for travels with a more powerful engine.\nCreate in 1950 by Joly and Delemontez to developpe the french aeroclubs after WWII.
atc_heavy=0
atc_airline=Privé
atc_flight_number=
[General]
atc_type=JODEL
atc_model=D 120
performance=Envergure : 8,2 m\nLongueur : 6,2 m\nSurface ailaire : 12,75 m2\nMasse à vide : 375 kg\nMasse maxi : 650 kg\nMoteur : Continental C 90\nVitesse de décrochage : 75 km\/h\nVitesse d'approche : 90 km\/h\nVitesse de montée : 100 km\/h\nVitesse ascensionnelle : 2,5 m\/s\nVitesse maxi : 195 km\/h\nVitesse Croisière : 165 km\/h\nRéservoir AV : 60 l \nRéservoir AR : 55 l\nRayon d'action : 980 kms\nNb de personnes : 2
[WEIGHT_AND_BALANCE]
max_gross_weight= 1050.000
empty_weight= 950.000
reference_datum_position= 3.600, 0.000, 0.000
empty_weight_CG_position= -3.000, 0.000, 0.000
max_number_of_stations=50
station_load.0= 150.000, -1.000, -1.000, 0.000
station_load.1= 170.000, -3.000, 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= 2500.000
empty_weight_roll_MOI= 2300.000
empty_weight_yaw_MOI= 2460.000
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=1.086
induced_drag_scalar=1.000
elevator_effectiveness=0.981
aileron_effectiveness=0.981
rudder_effectiveness=0.981
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.121
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type= 0
Engine.0= 3.400, 0.000, 0.000
fuel_flow_scalar= 1.000
[piston_engine]
power_scalar=1.000
cylinder_displacement= 85.000
compression_ratio= 8.000
number_of_cylinders= 4
max_rated_rpm= 2700.000
max_rated_hp= 90.000
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=0.986
propeller_type= 1
propeller_diameter= 6.500
propeller_blades= 2
propeller_moi= 4.000
beta_max= 0.000
beta_min= 0.000
min_gov_rpm= 1400.000
prop_tc= 0.000
gear_reduction_ratio= 1.000
fixed_pitch_beta= 19.500
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, -12.000, 0.000, -2.100, 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, -3.750, 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, -3.750, 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= 6.130
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= 14.000, 0.000, 0.000, 14.000, 12.000
Center2= -14.000, 0.000, 0.000, 12.000, 10.000
[airplane_geometry]
wing_area= 153.000
wing_span= 26.900
wing_root_chord= 4.900
wing_dihedral= 1.500
wing_incidence= 3.500
wing_twist= -2.000
oswald_efficiency_factor= 0.800
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= 9.700
htail_pos_lon= -18.300
htail_pos_vert= 0.500
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 18.000
vtail_span= 4.800
vtail_sweep= 20.000
vtail_pos_lon= -16.200
vtail_pos_vert= 1.500
elevator_area= 12.700
aileron_area= 18.300
rudder_area= 6.800
elevator_up_limit= 25.000
elevator_down_limit= 20.000
aileron_up_limit= 12.000
aileron_down_limit= 12.000
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= 43.200
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
[Flaps.0]
type= 0
span-outboard= 0.500
extending-time= 7.000
system_type= 4
damaging-speed= 120.000
blowout-speed= 150.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 0.000, 0.000