


[fltsim.0]
title=Dornier Do-16 "8-t-Wal" M-MWAL Plus Ultra
sim=Do_Wal
model=8-t-Wal
panel=
sound=
texture=M-MWAL_8
kb_checklists=Do_Wal_check
kb_reference=Do_Wal_ref
atc_id=D2053
atc_id_color=0xff000000
ui_manufacturer=Dornier
ui_type=Do-16 "8-t-Wal"
ui_variation=M-MWAL Plus Ultra
visual_damage=1
editable=1
description=The Germans constructed this plane through the Italian company Societá di Costruzioni di Pisa, due to the restrictions imposed that overcame at the end of the World War I. It was an airplane that was used in great raids of 1925, obtaining 20 record world-wide. In 1925, Roald Amundsen arrived with him to the North Pole, soon he wanted to cross the Atlantic but, when stopping, the airplane was acquired by Wolfran Von Gronau for the German Commercial Flight School and the 18th of August of 1930 flew of List to New Cork, over flying the Faeroe Islands, Iceland, Greenland and Labrador. Lufthansa, in 1932, established the airmail service with South America and it used for the passage of the Atlantic, was carrying out the inaugural flight the 3rd of February of 1934, from Stuttgart by Seville, Bathurst, the Westfalen ship with catapult and Natal to Buenos Aires, in four days. In January of 1926, it made the first passage of the South Atlantic, as only airplane, covering the distance with 10,270 km From Palos to...
atc_heavy=0
atc_airline=
atc_flight_number=

[General]
performance=...Buenos Aires in 59 hours, taking mail between Buenos Aires and Montevideo.\nThis historical flight was manned by Ramon Franco (pilot), Julio Ruiz de Alda (copilot), Juan Manuel Durán (observer) and Pablo Rada (repair man). It made the stops in Las Palmas, Porto Praia (Cape Verde), Fernando Noronha Island, Pernambuco (Recife), Rio de Janeiro and Buenos Aires. This hydroplane was donated to Argentina by King Alfonso XIII where it is conserved at the moment in the aviation museum of Luján.\nWingspan: 27.2m\nLength: 18.2m\nHeight: 5.5m (including rotating Propellers)\nEngine:\n               -Two Napier Lion 450CV\n               -Two BMW VI 690CV\nCrew: 4-6\nMaximum Speed: 97NM\/h-180km\/h\nCruise Speed: 83NM\/h-155km\/h\nCeiling: 10500ft-3.500m\nMaximum Range: 6480NM-1200km\n
atc_type=DORNIER
atc_model=Wal
editable=0
Category=airplane

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[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
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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,   1.65, -37.0,  3.62, fx_navred ,
light.1=3,   1.65,  37.0,  3.62, fx_navgre ,
light.2=3,   -38.13,  0.00, -0.62, fx_navwhi ,
light.3=5,   20.60,  0.00, -1.42, fx_landing ,
//front motor exhaust 9 = nur wenn alle Lichter aus sind ist auch das hier aus.
//Besser auf Strobe und Beacon legen, der kann dann über spezielles Gauge (rpm Messer) bei rpm > 0 an und rpm = 0 ausgeschaltet werden.
//Vorteil: Jede Engine ist seperat und ist auch nur dann an, wenn gebraucht.
light.4=2, 1.5, 0.0, 8.0, fx_xfirewal
light.5=2, 3.2, 0.0, 8.0, fx_xfirewal
light.6=2, 4.9, 0.0, 8.0, fx_xfirewal
light.7=1, -7.4, 0.0, 7.7, fx_xfirewal
light.8=1, -5.7, 0.0, 7.7, fx_xfirewal
light.9=1, -4.0, 0.0, 7.7, fx_xfirewal
light.10=4, 0.0, 0.0, 5.0, fx_fxvclighth_wal.fx
light.11=4, 14.0, 0.0, -0.6, fx_fxvclighth_wal.fx

[SMOKESYSTEM]
//Neu! Kann Triebwerksfehlverhalten simulieren. Gesteuert auch über gauges oder adventure 
smoke.0=0.00, -4.00, 0.00, fx_enginefailure.fx
smoke.1=0.00,  4.00, 2.00, fx_Wal1_smoke
smoke.2=0.00,  4.00,-2.00, fx_Wal1_smoke
smoke.3=0.00, -5.00, 2.00, fx_Wal2_smoke
smoke.4=0.00, -5.00,-2.00, fx_Wal2_smoke

[contact_points]
//0  Class (1=wheel, 2=scrape, 3=skid, 4=float, 5=waterrudder)
//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)

//Boot
point.0= 4.000, 16.840, -1.700, -4.500, 1800.000, 0.000, 0.000, 0.000, 0.400, 2.500, 0.520, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 4.000, 16.840, 1.700, -4.500, 1800.000, 0.000, 0.000, 0.000, 0.400, 2.500, 0.520, 0.000, 0.000, 3.000, 0.000, 0.000
point.2= 4.000, -8.850, -4.700, -4.500, 1800.000, 0.000, 0.000, 0.000, 0.400, 2.500, 0.520, 0.000, 0.000, 2.000, 0.000, 0.000
point.3= 4.000, -8.850, 4.700, -4.500, 1800.000, 0.000, 0.000, 0.000, 0.400, 2.500, 0.520, 0.000, 0.000, 3.000, 0.000, 0.000
point.4= 4.000, -19.540, 0.000, -4.450, 1800.000, 0.000, 0.000, 0.000, 0.400, 2.500, 0.520, 0.000, 0.000, 0.000, 0.000, 0.000
//scrape
point.5= 2.000, 0.980, -38.350, 3.070, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.6= 2.000, 0.980, 38.350, 3.070, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.7= 2.000, 16.860, 0.000, 1.000, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.8= 2.000, -8.180, 0.000, 13.670, 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.9= 2.000, -38.290, 0.000, -1.420, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//Wheel virtual
point.10= 3.000, 13.340, 0.000, -6.440, 1300.000, 0.000, 0.700, 10.000, 0.550, 1.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000
point.11= 1.000, -11.650, -2.500, -6.440, 1300.000, 1.000, 0.800, 0.000, 0.550, 1.500, 0.650, 0.000, 0.000, 4.000, 0.000, 0.000
point.12= 1.000, -11.650, 2.500, -6.440, 1300.000, 2.000, 0.800, 0.000, 0.550, 1.500, 0.650, 0.000, 0.000, 4.000, 0.000, 0.000
//Stummel,verhindert starkes kippen auf Eis
point.13= 3.000, -6.310, -9.900, -4.950, 1300.000, 0.000, 0.000, 0.000, 0.250, 2.500, 0.650, 0.000, 0.000, 7.000, 0.000, 0.000
point.14= 3.000, -6.310, 9.900, -4.950, 1300.000, 0.000, 0.000, 0.000, 0.250, 2.500, 0.650, 0.000, 0.000, 8.000, 0.000, 0.000
//Wasserruder
point.10= 4.000, 16.840, 0.000, -4.500, 1800.000, 0.000, 0.000, 45.000, 0.400, 2.500, 0.520, 0.000, 0.000, 0.000, 0.000, 0.000
//Stummel aussen und noch mal Ruder
point.11= 4.000, -6.310, -9.900, -4.550, 1300.000, 0.000, 0.000, 45.000, 0.400, 2.500, 0.750, 0.000, 0.000, 2.000, 0.000, 0.000
point.12= 4.000, -6.310, 9.900, -4.550, 1300.000, 0.000, 0.000, 45.000, 0.400, 2.500, 0.750, 0.000, 0.000, 3.000, 0.000, 0.000
static_pitch= -0.180
static_cg_height= 4.850

[Views]
eyepoint=12.52, -1.65, 0.18

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= -0.500, 0.000, 0.000
max_number_of_stations=50
station_load.0= 180.000, 12.370, -1.265, -0.330, Pilot
station_load.1= 180.000, 12.370, 1.265, -0.330, Co pilot
station_load.2= 180.000, 6.350, -1.366, -1.640, Navigator
station_load.3= 180.000, 1.400, 1.366, -1.640, Engineer
station_load.4= 600.000, -15.900, 0.000, -1.640, Payload rear
station_load.5= 1600.000, -3.000, 0.000, -0.640, Payload center
empty_weight= 12948.000
empty_weight_roll_MOI= 41453.000
empty_weight_pitch_MOI= 53084.000
empty_weight_yaw_MOI= 62255.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 22060.000
// 10 Tonnen
CG_forward_limit= 0.200
CG_aft_limit= -0.500

[fuel]
LeftMain= -0.730, -4.270, -3.400, 268.000, 2.000
LeftAux= -6.640, -6.562, -5.143, 98.000, 0.000
RightMain= -0.730, 4.270, -3.400, 268.000, 2.000
RightAux= -6.640, 6.562, -5.143, 98.000, 0.000
Center1= 1.000, 0.000, -1.900, 312.000, 2.000
fuel_type=1.000000
number_of_tank_selectors=1
//Total fuel 1044 USGal=3951 Liter= 6264 lbs
electric_pump=1

[flight_tuning]
cruise_lift_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.300
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.215
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
rudder_effectiveness=1.000
p_factor_on_yaw          = 0.5
torque_on_roll           = 0.2
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

[pitot_static]
vertical_speed_time_constant=100
pitot_heat=1.000000
//Increasing this value will cause a more instantaneous reaction in the VSI

[airplane_geometry]
wing_area= 1206.000
wing_span= 89.240
wing_root_chord= 13.121
wing_dihedral= 0.300
wing_incidence= 1.700
wing_twist= 0.000
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 130.000
htail_span= 24.000
htail_pos_lon= -36.330
htail_pos_vert= 2.750
htail_incidence= -0.800
htail_sweep= 0.000
vtail_area= 49.000
vtail_span= 8.100
vtail_sweep= 25.000
vtail_pos_lon= -37.830
vtail_pos_vert= 3.330
elevator_area= 40.860
aileron_area= 49.930
rudder_area= 24.310
elevator_up_limit= 26.000
elevator_down_limit= 23.000
aileron_up_limit= 24.001
aileron_down_limit= 18.999
rudder_limit= 38.000
elevator_trim_limit= 21.000
spoiler_limit= 1.450
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
oswald_efficiency_factor= 0.700
auto_spoiler_available=0
spoiler_extension_time=12.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000

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

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=400.000000
autothrottle_available=1
pitch_takeoff_ga=8.000000
//use_no_default_pitch=1
//use_no_default_bank=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=95.000000
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=2000.000000
max_pitch_velocity_hi_alt_breakpoint=8000.000000
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

[EFFECTS]
wake=fx_wake_s
water=fx_waterland_wal
waterspeed=fx_waterland
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_wtrspray_s, 1
startup=fx_engstrt_vega

[direction_indicators]
direction_indicator.0=1,0

[GeneralEngineData]
engine_type= 0
Engine.0= 7.700, -1.000, 5.340
Engine.1= -8.100, -1.00, 4.670
//Motorseitenzug
fuel_flow_scalar= 0.950
min_throttle_limit=0.000000

[piston_engine]
cylinder_displacement= 233.100
compression_ratio= 6.500
number_of_cylinders= 12
max_rated_rpm= 1680.000
max_rated_hp= 750.000
fuel_metering_type= 1
cooling_type= 1
normalized_starter_torque= 0.095
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
power_scalar=1.000

[propeller]
propeller_type= 1
propeller_diameter= 11.495
propeller_blades= 4
propeller_moi= 22.000
beta_max= 0.500
beta_min= 0.500
min_gov_rpm= 800.000
prop_tc= 0.010
gear_reduction_ratio= 1.000
fixed_pitch_beta= 22.400 // was 21.5
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
thrust_scalar=1.050

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

[Reference Speeds]
flaps_up_stall_speed= 66.000
full_flaps_stall_speed= 66.000
cruise_speed= 105.000
max_indicated_speed=129.000000

[Flaps.0]
// please do not change this values, even if they appear crazy.
// This will be used for special effect with FSUIPC
type= 1
span-outboard= 0.500
extending-time= 0.100
system_type= 4
damaging-speed= 500.000
blowout-speed= 500.000
lift_scalar= 1.000
drag_scalar= 10.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 70.000, 0.000

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 0.68

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1
stick_shaker=0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=4.900000
engine_map=1,1,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
