[fltsim.0]
title=Do_26_gmax
sim=Do26A_4
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=Do-26A_ref
atc_id=DAWDS
ui_manufacturer=Dornier
ui_type=Do 26 A
ui_variation=V 2 - Seefalke D-AWDS
description=Transcontinental Flying Boat, Southatlantic mail service from 1939 for Lufthansa.FS9 version.
atc_heavy=0
atc_airline=Lufthansa
atc_flight_number=1939
prop_anim_ratio=0.8
visual_damage=1
[fltsim.1]
title=Do_26_gmax_DVC
sim=Do26A_4
model=DVC
panel=DVC
sound=
texture=
kb_checklists=
kb_reference=Do-26A_ref
atc_id=DAWDS
ui_manufacturer=Dornier
ui_type=Do 26 A
ui_variation=V 2 - Seefalke D-AWDS DVC
description=Transcontinental Flying Boat, Southatlantic mail service from 1939 for Lufthansa.FS9 version.
atc_heavy=0
atc_airline=Lufthansa
atc_flight_number=1939
prop_anim_ratio=0.8
visual_damage=1
[fltsim.0]
title=Do_26_gmax
sim=Do26A_4
model=Do26DVC
panel=
sound=
texture=
kb_checklists=
kb_reference=Do-26A_ref
atc_id=DAWDS
ui_manufacturer=Dornier
ui_type=Do 26 A
ui_variation=V 2 - Seefalke D-AWDS
description=Transcontinental Flying Boat, Southatlantic mail service from 1939 for Lufthansa.FS9 version.
atc_heavy=0
atc_airline=Lufthansa
atc_flight_number=1939
prop_anim_ratio=0.8
visual_damage=1
[General]
atc_type=DORNIER
atc_model=FLOATPLANE
editable=0
performance=Max Airspeed: 335 Km\/h\nMTOW 15 tons or 33.112 lbs\nEngine Jumo 205 with 4 x 700 hp\nCruise speed 290 km\/h\nLanding speed 110 km\/h\nRange 2600 km
//WARNING !!! do NOT use FSEDIT for changes
//ACHTUNG !!! Nicht mit FSEDIT bearbeiten
// Modifikation 14.12.03 by W. Beckert for FS9, AIR File basic by W.Beckert, real FS2k2
[WEIGHT_AND_BALANCE]
max_gross_weight = 33112.000
//about 15 Tons for nominal water takeoff only! Max 19 Tons = 41942 lbs with catapult launch
empty_weight = 24812.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations = 50
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.0 = 170, 11.5, -1.68, 0.7, Pilot
station_load.1 = 170, 11.5, 1.68, 0.7, Co-Pilot
station_load.2 = 170, 7.2, 2.10, -1.5, Funker
station_load.3 = 170, 5.4, -2.10, -1.8, Bordwart
station_load.4 = 200, 18.5, 0.0, -3.0, Post vorn
station_load.5 = 200, -29.5, 0.0, -3.0, Post hinten
station_load.6 = 800, -12.0, 0.0, -3.0, Fracht
;Moments of Inertia
empty_weight_pitch_MOI = 182170.000
empty_weight_roll_MOI = 188898.000
empty_weight_yaw_MOI = 297950.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 0
Engine.0 = -11.600, 9.800, 1.200 //engine left front, less upwards reduce pitch moment, was 4.4
Engine.1 = -11.600, -9.800, 1.200 //engine left rear
Engine.2 = 11.600, 9.800, 1.200 //engine right front
Engine.3 = 11.600, -9.800, 1.200 // engine right rear
fuel_flow_scalar = 0.800 // adjust for 1400 NM or 2600km range
min_throttle_limit=0.000000
[SMOKESYSTEM] //Vertical (feet),Longitudinal (feet), Lateral (feet)
smoke.0= 2.3,-3.13,-10.33, fx_Do26_smoke1
smoke.1= 2.1,-3.13, -9.35, fx_Do26_smoke1
smoke.2= 2.1,-3.13, 9.35, fx_Do26_smoke1
smoke.3= 2.3,-3.13, 10.33, fx_Do26_smoke1
smoke.4= 2.3,-3.13,-10.33, fx_Do26_smoke2
smoke.5= 2.1,-3.13, -9.35, fx_Do26_smoke2
smoke.6= 2.1,-3.13, 9.35, fx_Do26_smoke2
smoke.7= 2.3,-3.13, 10.33, fx_Do26_smoke2
[piston_engine]
//original Jumo205=169.08 cuin
cylinder_displacement= 169.080
compression_ratio= 12.000 // simulate Diesel engine // was 17
number_of_cylinders= 6
max_rated_rpm= 2500.000
max_rated_hp= 700.000
fuel_metering_type= 1
cooling_type= 1
normalized_starter_torque= 0.100
turbocharged= 1
max_design_mp= 34.000
min_design_mp= 5.000
critical_altitude= 5000.000 // limit ceiling altitude with charger, value not ceiling!
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=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=0.300
idle_rpm_friction_scalar=0.100
power_scalar=1.000
[propeller]
propeller_type= 0
propeller_diameter= 11.316 //3.45 m equals average front/rear prop dia
propeller_blades= 3
propeller_moi= 12.100 // fine tune rpm idle and max rpm
beta_max= 45.000 // was 55
beta_min= 5.000 // was 12
min_gov_rpm= 800.000
prop_tc= 0.004
gear_reduction_ratio= 1.580 // real world value
fixed_pitch_beta= 20.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather= 400.000
beta_feather= 88.500
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
thrust_scalar=1.080 // account for 2 pusher props
[contact_points]
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//Class: 1=Rad 4=Schwimmer 2=scrape 5=Wasserruder
//GEAR--0-----1-----2-----3-----4------5----6-----7----8----9---10--11-12-13-14-15
point.0=1, -1.0, -27.6, -1.0, 1100.0, 0.0, 0.0, 0.0, 0.5, 2.5, 0.5, 5, 8, 0, 120, 150 //Schwimmer links-einz.
point.1=1, -1.0, 27.6, -1.0, 1100.0, 0.0, 0.0, 0.0, 0.5, 2.5, 0.5, 7, 9, 0, 120, 150 //Schwimmer rechts-einz.
point.2=4, 23.7, 0.0, -5.8, 1500.0, 0.0, 1.0,30.0, 0.5, 2.5, 0.5, 0, 0, 1, 0, 0 //Rumpf vorn
point.3=4, -8.0, 0.0, -5.5, 1500.0, 0.0, 1.0, 0.0, 0.5, 2.5, 0.7, 0, 0, 3, 0, 0 //Rumpf hinten
point.4=4, -4.0, -27.6, -3.6, 1100.0, 0.0, 1.0, 0.0, 0.5, 2.5, 0.5, 5, 5, 2, 0, 0 //Schwimmer links
point.5=4, -4.0, 27.6, -3.6, 1100.0, 0.0, 1.0, 0.0, 0.5, 2.5, 0.5, 5, 5, 3, 0, 0 //Schwimmer rechts
point.6=4, -1.7, -5.15, -5.5, 1500.0, 0.0, 1.0, 0.0, 0.5, 2.5, 0.5, 0, 0, 2, 0, 0 //Rumpf Stufe links
point.7=4, -1.7, 5.15, -5.5, 1500.0, 0.0, 1.0, 0.0, 0.5, 2.5, 0.5, 0, 0, 3, 0, 0 //Rumpf Stufe rechts
//SCRAPES
point. 8=2,-51.0, 0.0, 4.0, 1500.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0, 4, 0, 0 //Rumpf hinten Heck
point. 9=2, -6.0, -49.2, 4.0, 800.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0, 5, 0, 0 //Tragfläche L
point.10=2, -6.0, 49.2, 4.0, 800.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0, 6, 0, 0 //Tragfläche R
point.11=2, 23.7, 0.0, -1.0, 1500.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0, 4, 0, 0 //Rumpf vorn
point.12=2,-12.0, 0.0, 4.0, 1500.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0, 4, 0, 0 //Rumpf hinten
point.13=1, 20.0, 0.0, -1.5, 1100.0, 0.0, 0.0, 0.0, 0.5, 2.5, 0.5, 5, 5, 0, 120, 150 //Dummy Nose gear, fool tricycle
static_pitch = 0.5 //Degrees
static_cg_height = 5.5 //Feet
gear_system_type=0 // electric
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage=28.0
generator_alternator_voltage=28.0
max_generator_amps=40.0
flap_motor=0, 18 , 18.0
gear_motor=4, 25 , 18.0
autopilot=0, 5 , 18.0
avionics_bus=0, 18, 18.0
avionics=1, 10 , 18.0
pitot_heat=0, 10 , 18.0
additional_system=0, 25, 18.0
marker_beacon=1, 6 , 18.0
gear_warning=0, 6 , 18.0
fuel_pump=0, 8 , 18.0
starter1=0, 20, 18.0
starter2=0, 20, 18.0
starter3=0, 20, 18.0
starter4=0, 20, 18.0
light_nav=0, 6 , 18.0
light_beacon=0, 8 , 18.0
light_landing=0, 8 , 18.0
light_taxi=0, 8 , 18.0
light_strobe=0, 8 , 18.0
light_panel=0, 3 , 18.0
electric_always_available=1
[pitot_static]
vertical_speed_time_constant = 10.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[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
[Views]
eyepoint = 14, -1.68, 0.9 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -4.9, -49.2, 4.7, fx_navred ,
light.1 =3, -4.9, 49.2, 4.7, fx_navgre ,
light.2 =3, -51.5, 0.0, 3.8, fx_navwhi ,
light.3 =4, 12.0, 0.0, 2.7, fx_vclight,
[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 = 150, 250
aileron = 150, 250
rudder = 150, 250
[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=3,0
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//5410 lbs = 2450 kg = 900 USGal nominal for Water takeoff only
//11592 lbs = 4 x 483 = 1932 USGal max possible in tanks (real world value)
LeftMain= 4.000, -2.000, -5.300, 483.000, 1.000
LeftAux= -4.000, -2.000, -5.300, 483.000, 1.000
RightMain= 4.000, 2.000, -5.300, 483.000, 1.000
RightAux= -4.000, 2.000, -5.300, 483.000, 1.000
fuel_type=2
number_of_tank_selectors=2
electric_pump=1
[EFFECTS]
wake=fx_wake_s
//water=fx_spray
water=fx_waterland_wal
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
startup=fx_engstrt_vega // new startup smoke in FS2k4
[Reference Speeds]
flaps_up_stall_speed = 68.000
full_flaps_stall_speed = 58.000
cruise_speed = 175.000 // KTAS at sea level
max_indicated_speed = 190.000 // KIAS red line
[airplane_geometry]
wing_area= 1291.000 // real value = 120 m2
wing_span= 98.417 //real value = 30 m
wing_root_chord= 16.000 //real value = 5 m
wing_dihedral= 3.000
wing_incidence= 1.000 //real value 4.5
wing_twist= -3.000 //real value
oswald_efficiency_factor= 0.75
wing_winglets_flag= 0
wing_sweep= 12.000
wing_pos_apex_lon= 5.700
wing_pos_apex_vert= 3.010
htail_area= 203.000
htail_span= 29.417
htail_pos_lon= -44.500
htail_pos_vert= 6.020
htail_incidence= 1.000
htail_sweep= 11.000
vtail_area= 104.000
vtail_span= 11.628
vtail_sweep= 11.000
vtail_pos_lon= -45.500
vtail_pos_vert= 5.417
elevator_area= 67.970
aileron_area= 74.570
rudder_area= 45.730
elevator_up_limit= 27.985
elevator_down_limit= 19.990
aileron_up_limit= 18.002
aileron_down_limit= 11.994
rudder_limit= 23.985
elevator_trim_limit= 12.000
spoiler_limit= 90.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
// aileron_to_rudder_scale= 0.35 // simulates auto-coordination in FS2004
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 200.0 // keep value low to avoid excess rate at activation of A/P
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=8.000000
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=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
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
[Flaps.0]
//Hauptklappen - Spaltklappe innen
type= 1
span-outboard= 0.410
extending-time= 8.000
system_type= 0
damaging-speed= 172.000
blowout-speed= 190.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 0.300
flaps-position.0= 0.000, 220.000
*flaps-position.1= 10.000, 220.000
flaps-position.1= 24.000, 150.000
*flaps-position.2= 34.000, 130.000
flaps-position.2= 60.000, 110.000
[Flaps.1]
//Querruder als flaperons
type= 1
span-outboard= 0.540
extending-time= 4.000
system_type= 0
damaging-speed= 172.000
blowout-speed= 190.000
lift_scalar= 0.500
drag_scalar= 0.400
pitch_scalar= 0.100
flaps-position.0= 0.000, 220.000
flaps-position.1= 4.000, 150.000
flaps-position.2= 8.000, 130.000
flaps-position.3= 15.000, 110.000
[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
[brakes]
toe_brakes_scale=0.100000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=24.0
flap_limit_idle=34.0
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0