[fltsim.0]
title=DROMADER TMS Interflug
sim=PZL-18
model=
panel=
sound=
texture=TMS
checklists=
kb_reference=drom_ref
ui_manufacturer=PZL
ui_type=M18A Dromader
ui_variation=DDR-TMS Interflug
atc_id=DDR-TMS
atc_airline=AgroAir
atc_flight_number=6667
description=PZL M18A Dromader is the agricultural aircraft. Author: Jan Moravec, Repaint: Ingo Schwan 



[General]
performance=Wingspan: 17.7m \nLength: 9.5m \nWing Area: 40m2 \nEngine Asz-62 power: 750kW (1000hp) \nFuel: 2x356l \nMax. Take-off Weight: 4700kg \nMax. Speed: 230 km/h \nOperating Speed:170-200km/h \nStalling Speed (Flaps 15°): 109km/h \nMax. Rate of Climb: 6.85m/s \nModel Copyright (c) 2004 Jan Moravec
atc_type=
atc_model=

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000


[WEIGHT_AND_BALANCE]

empty_weight=5800.018

reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.00, 0.00, 0.00        //long,later.,vertical

max_number_of_stations=50

;#Cargo
station_load.0= 2529.110, 0.0, 0.0, -0.630     //chem
station_load.1=198.3468,-5.0,0.0,-0.63         //pilot
station_load.2=180.3468,-7.0,0.0,-0.63         //mechanik
station_load.3=100.3468,-7.5,0.0,-0.63         //zavazadlo

empty_weight_roll_MOI= 41359.000
empty_weight_pitch_MOI= 66956.000           //36956.0
empty_weight_yaw_MOI= 66398.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 11095.284
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=0.000000,0.000000,0.000000,0.000000


[flight_tuning]
cruise_lift_scalar     = 1.3
parasite_drag_scalar   = 0.7
induced_drag_scalar    = 0.7
elevator_effectiveness = 1.0
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.4
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0


[ground_reaction]
main_gear_static_compression=0.46
center_gear_static_compression=0.3
main_gear_damping_ratio=0.75
center_gear_damping_ratio=0.75

[electrical]


;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=2, 0.1 , 17.0
autopilot=2, 0.1 , 17.0
avionics=2, 0.1 , 17.0
pitot_heat=2, 0.1 , 17.0
additional_system=2, 0.1, 17.0
marker_beacon=2, 0.1 , 17.0
gear_warning=2, 0.1 , 17.0
fuel_pump=2, 0.1 , 17.0
starter1=2, 0.1, 17.0
light_nav=2, 0.1 , 17.0
light_beacon=2, 0.1 , 17.0Leng
light_landing=2, 0.1 , 17.0
light_taxi=2, 0.1 , 17.0
light_strobe=2, 0.1 , 17.0
light_panel=2, 0.1 , 17.0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1
Com.2=1
Nav.1=1
Nav.2=1
Adf.1=1
Transponder.1=1
Marker.1=1


[fuel]
LeftMain= -1.237, -7.000, 2.264, 94.500, 0.000
RightMain= -1.237, 7.000, 2.264, 94.500, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area= 600.000
wing_span= 58.056
wing_root_chord= 7.444
wing_dihedral= 3.999
wing_incidence= 2.999
wing_twist= 0.000
oswald_efficiency_factor= 0.751
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 1.861
wing_pos_apex_vert= 0.000
htail_area= 80.600
htail_span= 19.833
htail_pos_lon= -20.691
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 38.300
vtail_span= 8.849
vtail_sweep= 0.000
vtail_pos_lon= -20.441
vtail_pos_vert= 1.500
elevator_area= 73.960
aileron_area= 77.200
rudder_area= 37.800
elevator_up_limit= 42.000
elevator_down_limit= 22.500
aileron_up_limit= 32.000
aileron_down_limit= 24.000
rudder_limit= 30.000
rudder_1_limit=75
elevator_trim_limit= 19.481
spoiler_limit= 57.296
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[contact_points]
// //0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
        //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)                    
           0       1       2       3      4         5       6      7       8      9      10     11     12     13     14    15
point.0= 1.000, -14.583, 0.000, -1.930,  3200.000, 0.000, 0.770, 60.320, 0.250, 4.000, 1.000, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000,  6.000, -5.667, -5.430,  2200.000, 1.000, 1.310, 0.000,  0.295, 4.000, 0.800, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000,  6.000,  5.667, -5.430,  2200.000, 2.000, 1.310, 0.000,  0.295, 4.000, 0.800, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, -0.500, -25.417, 5.667,  1574.803, 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, -0.500,  25.417, 5.667,  1574.803, 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, -22.500, 0.000, -1.917,  1574.803, 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,  10.083, 0.000, -1.583,  1574.803, 0.000, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch= 8.991
static_cg_height= 3.910


[GeneralEngineData]
engine_type= 0
Engine.0= 9.167, 0.000, -2.000
fuel_flow_scalar= 1.000
min_throttle_limit=0.050000

[piston_engine]
cylinder_displacement= 204.400
compression_ratio= 6.400
number_of_cylinders= 9
max_rated_rpm= 2200.000
max_rated_hp= 1000.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque=0.035
turbocharged= 1
max_design_mp= 41.500
min_design_mp= 1.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 1
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
propeller_type= 0
propeller_diameter= 11.800
propeller_blades= 4
propeller_moi= 20.000
beta_max= 40.000
beta_min= 15.000
min_gov_rpm= 1400.000
prop_tc= 0.010
gear_reduction_ratio= 1.454
fixed_pitch_beta= 20.000
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= 15.000
minimum_reverse_beta= 15.000
prop_animation_ratio= -1.7

[Reference Speeds]
flaps_up_stall_speed= 77.000
full_flaps_stall_speed= 71.000
cruise_speed=124
max_indicated_speed=125.632813

[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[Views]
eyepoint=-6.3,0.07,5.85    //délka, -vlevo +vpravo, výška

[autopilot]
autopilot_available=0
flight_director_available=0


[direction_indicators]
direction_indicator.0=1,0



[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tiremark_6, 1

[Lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,   0.90, -28.16, 2.75, fx_navred           // (feet) longitudinal, lateral, vertical 
light.1=3,   1.10,  28.36, 2.75, fx_navgre
light.2=1,  -7.80,   0.00, 7.40, fx_beacon
light.3=1,  -7.80,   0.00, 7.40, fx_beacon
light.4=4,  -4.05,   0.00, 7.00, fx_vclight
light.5=4,   2.05,   0.00, 3.00, fx_vclight

[SMOKESYSTEM]
smoke.0=-20.00,-11.00,-7.00, fx_smoke_w      //vertical,longitudinal,lateral
smoke.1=-20.00,-11.50,-5.00, fx_smoke_wvb
smoke.2=-20.00,-11.00,-2.50, fx_smoke_wvc
smoke.3=-20.00,-11.00, 2.50, fx_smoke_wvc
smoke.4=-20.00,-11.50, 5.00, fx_smoke_wvb
smoke.5=-20.00,-11.00, 7.00, fx_smoke_w

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 4.500
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000



[exits]
number_of_exits=2
exit_rate.0=0.2
exit_rate.1=0.2

[TailHook]
tailhook_length=3.0                           ;(feet)
tailhook_position=0.0, 0.0, 3.5            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0

[brakes]
toe_brakes_scale=0.905185
parking_brake=1

[hydraulic_system]
normal_pressure=6.930556
engine_map=1,0,0,0

[stall_warning]
type=0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0