Dornier 128-6 Просмотр ZIP-архива
Aircraft/Do_128-6/Aircraft.cfg
[fltsim.0]
title=Dornier 128-6
sim=Do128-6_FS2004
model=
panel=
sound=
texture=
panel_alias = beech_king_air_350\panel
sound_alias = beech_king_air_350\sound
kb_checklists=DO_128-6_WHEELS_CHECK
kb_reference=DO_128-6_WHEELS_REF
atc_id_color=0xffffffffff
atc_id=D IBUF
ui_manufacturer=Dornier
ui_type=128-6
ui_variation=Research Aircraft of TU Braunschweig V5
description=This Dornier Do128-6 currently serves as an airborne lab for the Institute of Flight Guidance and Control of the University of Braunschweig (Germany). It is covered with probes and sensors to allow for precise recording of all relevant flight data.\n
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=DORNIER
atc_model=D28T
editable=1
atc_id_enable=1
atc_id=D IBUF
performance=Length: 11.41 m (37 ft 5 in)\nSpan: 15.55 m (51 ft)\nMax. TO weight: 4350 kg (9590 lbs)\nPower: 2 x P&W Canada PT 6A-110 @ 400shp\nRange: 3740 NM @ 20000 ft, 6614 lbs G.W.\nDate: 3 January 2002\nScale: 3937079\/12000000\nDesigner: Antonis Konstantinidis \/ Mathias Elsaesser\n\n\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 9656.000
empty_weight = 6063.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = -0.139, 0.000, 0.000
max_number_of_stations = 50
station_load.0=18.519000, 9.908103, 1.148000, -2.953000, longitudinal
station_load.1=12.787000, 15.485514, 1.148000, -2.756000, longitudinal
station_load.2=198.416000, 3.674526, -1.312000, 0.000000, longitudinal
station_load.3=209.439000, 3.674526, 1.312000, 0.000000, longitudinal
station_load.4=176.370000, -15.059000, -1.312000, 0.000000, longitudinal
station_load.5=0.000000, -2.198160, -1.312000, 0.000000, longitudinal
station_load.6=0.0, -2.1981597, 1.312, 0.0 //Passenger 3 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7=0.0, -7.1850213, 1.312, 0.0 //Passenger 4 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8=62.611000, 0.721779, 1.312000, 0.000000, longitudinal
station_load.9=62.611000, -4.265083, 1.312000, 0.000000, longitudinal
station_load.10=59.359000, -9.120711, -1.312000, 0.000000, longitudinal
station_load.11=72.091000, -4.691591, 1.312000, 0.000000, longitudinal
station_load.12=41.006000, -12.073458, -0.492000, 0.000000, longitudinal
;Moments of Inertia
empty_weight_pitch_MOI = 30000.000
empty_weight_roll_MOI = 9000.000
empty_weight_yaw_MOI = 36500.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.561
CG_aft_limit= -0.380
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =0.893
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 =0.759
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 5
Engine.0 = 9.333, -6.562, -0.833
Engine.1 = 9.333, 6.562, -0.833
fuel_flow_scalar = 1.240
min_throttle_limit = -0.288 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature=-39.0
[propeller]
thrust_scalar =1.000
propeller_type = 0
propeller_diameter = 7.743
propeller_blades = 3
propeller_moi = 12.000
beta_max = 45.000
beta_min = 12.000
min_gov_rpm = 30000.000
prop_tc = 0.004
gear_reduction_ratio = 19.740
fixed_pitch_beta = 0.000
low_speed_theory_limit = 80.000
prop_sync_available = 0
prop_deice_available = 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather = 50.000
beta_feather = 85.000
power_absorbed_cf = 0.900
defeathering_accumulators_available= 0
prop_reverse_available = 1.000
minimum_on_ground_beta = 1.000
minimum_reverse_beta = -14.000
[TurbineEngineData]
fuel_flow_gain = 0.070
inlet_area = 1.000
rated_N2_rpm = 37500.000
static_thrust = 80.000
afterburner_available= 0
reverser_available = 1
[turboprop_engine]
power_scalar =1.000
maximum_torque = 1540.000
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
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 250.0
flap_motor = 3, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10 , 14.0
avionics = 1, 5 , 14.0
pitot_heat = 3, 15 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
starter2 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 10 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
light_cabin = 0, 5 , 17.0
prop_sync = 0, 15 , 17.0
fuel_transfer_pump = 0, 5 , 17.0
propeller_deice = 0, 32 , 17.0
light_wing = 0, 5 , 17.0
[Views]
eyepoint=3.95,-1.25,1.40
[LIGHTS]
//0 Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cabin
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
light.0 = 3, 0.72, -24.96, 3.27, fx_navred ,
light.1 = 3, 0.72, 24.96, 3.27, fx_navgre ,
light.2 = 3, -26.25, 0.00, 1.43, fx_navwhi ,
light.3 = 2, 0.49, -25.07, 3.27, fx_strobe ,
light.4 = 2, 0.49, 25.07, 3.27, fx_strobe ,
light.5 = 1, -22.74, 0.00, 10.5, fx_beacon ,
light.6 = 2, -26.28, 0.00, 1.43, fx_strobe ,
light.7 = 4, 3.95, 0.00, 2.67, fx_vclight,
light.8 = 4, 3.95, -1.3, 1.37, fx_vclighth,
light.9 = 4, 3.95, 1.3, 1.37, fx_vclight,
light.10 = 8, 1.96, -2.7, 1.78, fx_CII_wing ,
light.11 = 8, 1.96, -2.7, 1.78, fx_navwhi ,
light.12 = 5, 0.92, -23.56, 3.27, fx_landing ,
light.13 = 5, 0.92, 23.56, 3.27, fx_landing ,
//0 Class <0 = None, 1 = Wheel, 2 = Scrape, 3 = Skid, 4 = Float, 5 = Water Rudder>
//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 <0 = Center Gear, 1 = Auxiliary Gear, 2 = Left Gear, 3 = Right Gear, 4 = Fuselage Scrape, 5 = Left Wing Scrape, 6 = Right Wing Scrape, 7 = Aux1 Scrape, 8 = Aux2 Scrape, 9 = Tail Scrape.
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0= 1.000, -25.500, 0.000, -2.260, 3000.000, 0.000, 0.558, 180.000, 0.296, 2.500, 0.952, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 2.417, -5.774, -7.090, 2000.000, 1.000, 1.066, 0.000, 0.642, 2.500, 0.815, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 2.417, 5.774, -7.090, 2000.000, 2.000, 1.066, 0.000, 0.642, 2.500, 0.815, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, -1.000, -25.508, 3.270, 1000.000, 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, -1.000, 25.508, 3.270, 1000.000, 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, -23.113, 0.000, -1.600, 3000.000, 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, 9.700, 0.000, -2.900, 3000.000, 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, 11.406, 0.000, -1.356, 3000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.8= 2.000, 3.950, 0.000, 3.000, 3000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.9= 2.000, -22.000, 0.000, 10.000, 3000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.10= 2.000, 2.417, -6.600, -2.400, 3000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.11= 2.000, 2.417, 6.600, -2.400, 3000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
static_pitch = 9.400
static_cg_height = 6.000
gear_system_type=4 //Hydraulic
tailwheel_lock = 1
[gear_warning_system]
gear_warning_available = 0 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[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
Adf.2 = 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 = 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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -0.069, -6.562, -1.150, 135.000, 3.000
External1 = -0.013, -14.042, 0.902, 65.000, 3.000
RightMain = -0.069, 6.562, -1.150, 135.000, 3.000
External2 = -0.013, 14.042, 0.902, 65.000, 3.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[airplane_geometry]
wing_area = 312.153
wing_span = 51.017
wing_root_chord = 6.234
wing_dihedral = 6.000
wing_incidence = 4.000
wing_twist = -1.500
oswald_efficiency_factor= 1.000
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 0.272
wing_pos_apex_vert = 2.789
htail_area = 48.368
htail_span = 21.686
htail_pos_lon = -21.129
htail_pos_vert = 0.919
htail_incidence = -0.500
htail_sweep = 0.000
vtail_area = 33.856
vtail_span = 8.202
vtail_sweep = 11.000
vtail_pos_lon = -20.000
vtail_pos_vert = 4.757
elevator_area = 30.000
aileron_area = 13.292
rudder_area = 21.218
elevator_up_limit = 17.000
elevator_down_limit = 16.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 30.000
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 = 70.000
full_flaps_stall_speed = 54.000
cruise_speed = 147.215
max_mach = 0.58
max_indicated_speed= 259.000
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_pitch_mode= 2
default_vertical_speed= 1200.0
use_no_default_bank=1
default_bank_mode =0
autothrottle_available= 0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
pitch_takeoff_ga= 8.000
[forcefeedback]
stick_shaker_magnitude=0 ; 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=0.7
exit_rate.1=3 ;Percent per second
[stall_warning]
type=2
[Flaps.0]
type= 1
span-outboard= 0.540
extending-time= 10.000
system_type= 0
damaging-speed= 120.000
blowout-speed= 140.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 0.900
flaps-position.0= 0.000, 0.000
flaps-position.1= 25.000, 0.000
flaps-position.2= 43.000, 0.000
24447-do1286v5.zip
| Имя файла | Дата | Размер |
|---|---|---|
| Aircraft/Do_128-6/ | 23.08.2008 23:03 | |
| Aircraft/Do_128-6/Aircraft.cfg | 23.08.2008 15:53 | 15 KB |
| Aircraft/Do_128-6/DO_128-6_WHEELS_CHECK.htm | 21.08.2008 21:59 | 59 KB |
| Aircraft/Do_128-6/DO_128-6_WHEELS_REF.htm | 21.08.2008 21:28 | 10 KB |
| Aircraft/Do_128-6/Do128-6_FS2004.air | 01.06.2008 03:01 | 15 KB |
| Aircraft/Do_128-6/do1286P5.gif | 23.08.2008 16:41 | 13 KB |
| Aircraft/Do_128-6/do1286V5.gif | 23.08.2008 15:40 | 9 KB |
| Aircraft/Do_128-6/Documentation/ | 23.08.2008 23:03 | |
| Aircraft/Do_128-6/Documentation/Do128-6_D-IBUF_Documentation.htm | 22.12.2006 03:48 | 2 KB |
| Aircraft/Do_128-6/Documentation/F16 Air Show Tour Panel_V2 Instructions.pdf | 29.04.2008 02:19 | 851 KB |
| Aircraft/Do_128-6/Documentation/files/ | 23.08.2008 23:03 | |
| Aircraft/Do_128-6/Documentation/files/Abbreviations_and_Reference.htm | 23.08.2008 20:04 | 106 KB |
| Aircraft/Do_128-6/Documentation/files/airspeed.gif | 09.05.2001 23:31 | 32 KB |
| Aircraft/Do_128-6/Documentation/files/Altmuehltal_digital.jpg | 05.06.2001 12:32 | 8 KB |
| Aircraft/Do_128-6/Documentation/files/anig.gif | 08.03.2000 18:49 | 38 KB |
| Aircraft/Do_128-6/Documentation/files/background.jpg | 11.01.2002 02:53 | 27 KB |
| Aircraft/Do_128-6/Documentation/files/contact.gif | 23.08.2008 18:58 | 2 KB |
| Aircraft/Do_128-6/Documentation/files/D-IBUF_compare.gif | 30.03.2008 03:36 | 183 KB |
| Aircraft/Do_128-6/Documentation/files/D-IBUF_compare_panel.jpg | 04.04.2008 02:43 | 129 KB |
| Aircraft/Do_128-6/Documentation/files/D-IBUF_compare_rollout.jpg | 04.11.2002 01:11 | 78 KB |
| Aircraft/Do_128-6/Documentation/files/D-IBUF_computer_racks.jpg | 27.05.2001 03:35 | 9 KB |
| Aircraft/Do_128-6/Documentation/files/D-IBUF_Demonstrator2.jpg | 13.10.2001 23:23 | 52 KB |
| Aircraft/Do_128-6/Documentation/files/D-IBUF_Homepage_screenshot.jpg | 30.03.2008 01:51 | 27 KB |
| Aircraft/Do_128-6/Documentation/files/D-IBUF_ski.jpg | 30.05.2001 02:59 | 23 KB |
| Aircraft/Do_128-6/Documentation/files/do128_bi.gif | 17.01.2002 05:09 | 161 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_annunciator.gif | 06.04.2008 02:27 | 20 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_boost_pump.gif | 17.04.2001 02:27 | 5 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_CHECK_LEGAL_FS9.HTM | 23.08.2008 19:44 | 43 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_CHECK_LEGAL_FS9_d.HTM | 23.08.2008 19:15 | 49 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_cond_lever_range.jpg | 02.11.2002 18:14 | 6 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_crossfeed.gif | 17.04.2001 05:18 | 4 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_flap_handle.jpg | 12.07.2002 21:53 | 8 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_FS9.htm | 23.08.2008 18:49 | 7 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_FS9_d.htm | 23.08.2008 20:00 | 7 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_History_FS9.HTM | 24.08.2008 16:55 | 17 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_History_FS9_d.HTM | 25.08.2008 01:22 | 18 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_LP_cock.gif | 12.07.2002 22:11 | 11 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_Main_Panel_FS9.HTM | 25.08.2008 00:49 | 45 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_Main_Panel_FS9_d.htm | 25.08.2008 01:06 | 50 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_main_panel_overview3.jpg | 25.08.2008 00:05 | 131 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_main_panel_overview3_d.jpg | 25.08.2008 00:34 | 132 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_Pedestal_Panel_FS9.HTM | 09.06.2008 02:20 | 23 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_Pedestal_Panel_FS9_d.HTM | 09.06.2008 02:20 | 26 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_power_lever_range.jpg | 02.11.2002 18:09 | 17 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_PREREQUISITS_FS9.HTM | 22.08.2008 03:09 | 3 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_PREREQUISITS_FS9_d.HTM | 22.08.2008 03:09 | 3 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_prop_lever_range.jpg | 02.11.2002 18:11 | 11 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_Throttle-Fuel-Start.jpg | 05.11.2002 00:40 | 134 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_Throttle-Fuel-Start_d.jpg | 05.11.2002 01:26 | 154 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_D-IBUF_transfer_pump.gif | 17.04.2001 02:29 | 5 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_VC_FS9.HTM | 12.05.2008 01:30 | 7 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_VC_FS9_d.HTM | 12.05.2008 01:31 | 8 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_VIRTUAL_HISTORY_FS9.HTM | 12.05.2008 14:21 | 8 KB |
| Aircraft/Do_128-6/Documentation/files/DO128-6_D-IBUF_VIRTUAL_HISTORY_FS9_d.HTM | 12.05.2008 14:20 | 9 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_master_warning_lights.gif | 01.03.2003 17:18 | 11 KB |
| Aircraft/Do_128-6/Documentation/files/Do128-6_three_view.jpg | 05.06.2001 23:15 | 52 KB |
| Aircraft/Do_128-6/Documentation/files/Do28B1.jpg | 05.06.2001 23:07 | 16 KB |
| Aircraft/Do_128-6/Documentation/files/Do28D-X5_Turbo-Skyservant.jpg | 05.06.2001 12:38 | 17 KB |
| Aircraft/Do_128-6/Documentation/files/Do28D-X5_Turbo-Skyservant_+_Do28D.jpg | 27.05.2001 03:35 | 27 KB |
| Aircraft/Do_128-6/Documentation/files/Dornier_128-6.gif | 05.06.2001 23:19 | 28 KB |
| Aircraft/Do_128-6/Documentation/files/FF.gif | 13.05.2001 22:10 | 15 KB |
| Aircraft/Do_128-6/Documentation/files/Flapindicator.gif | 02.11.2002 18:20 | 3 KB |
| Aircraft/Do_128-6/Documentation/files/FP.gif | 13.05.2001 22:20 | 15 KB |
| Aircraft/Do_128-6/Documentation/files/fuel_left.gif | 13.07.2002 03:47 | 19 KB |
| Aircraft/Do_128-6/Documentation/files/fueltotalizer.gif | 06.01.2002 19:32 | 35 KB |
| Aircraft/Do_128-6/Documentation/files/germany.gif | 28.08.2002 02:30 | 6 KB |
| Aircraft/Do_128-6/Documentation/files/HSI_overview.gif | 27.05.2001 03:35 | 52 KB |
| Aircraft/Do_128-6/Documentation/files/HSI_Uebersicht.gif | 04.08.2002 02:20 | 57 KB |
| Aircraft/Do_128-6/Documentation/files/Icon_SPEEDS.bmp | 11.08.2008 13:01 | 1 KB |
| Aircraft/Do_128-6/Documentation/files/ITT.gif | 13.05.2001 22:10 | 17 KB |
| Aircraft/Do_128-6/Documentation/files/lb244.gif | 17.12.2002 00:28 | 44 KB |
| Aircraft/Do_128-6/Documentation/files/NG.gif | 25.05.2001 20:46 | 15 KB |
| Aircraft/Do_128-6/Documentation/files/overhead_panel.jpg | 05.04.2008 22:43 | 55 KB |
| Aircraft/Do_128-6/Documentation/files/POH p5-21 Stall speeds engines idling.jpg | 29.07.2008 03:26 | 374 KB |
| Aircraft/Do_128-6/Documentation/files/POH p5-23 Takeoff speeds flaps up.jpg | 29.07.2008 03:36 | 391 KB |
| Aircraft/Do_128-6/Documentation/files/POH p5-24 Takeoff speeds flaps 1.jpg | 29.07.2008 03:42 | 391 KB |
| Aircraft/Do_128-6/Documentation/files/POH p5-41 Best rate-of-climb speeds two engines.jpg | 29.07.2008 03:46 | 338 KB |
| Aircraft/Do_128-6/Documentation/files/POH p5-43 Best rate-of-climb speeds one engine.jpg | 11.08.2008 21:14 | 304 KB |
| Aircraft/Do_128-6/Documentation/files/POH p9-15 VHF Homing System Becker ZVG2002.jpg | 01.05.2008 04:13 | 326 KB |
| Aircraft/Do_128-6/Documentation/files/POH p9-16 VHF Homing System Becker ZVG2002.jpg | 01.05.2008 04:13 | 225 KB |
| Aircraft/Do_128-6/Documentation/files/POH p9-17 VHF Homing System Becker ZVG2002.jpg | 01.05.2008 15:21 | 118 KB |
| Aircraft/Do_128-6/Documentation/files/POH p9-59 Radio Altimeter System Sperry AA-300.jpg | 01.05.2008 03:12 | 245 KB |
| Aircraft/Do_128-6/Documentation/files/POH p9-60 Radio Altimeter System Sperry AA-300.jpg | 01.05.2008 15:45 | 206 KB |
| Aircraft/Do_128-6/Documentation/files/POH Page 7-7 Instrument Panel.jpg | 01.05.2008 21:37 | 344 KB |
| Aircraft/Do_128-6/Documentation/files/PT6A-110.jpg | 05.06.2001 12:46 | 39 KB |
| Aircraft/Do_128-6/Documentation/files/Radar.jpg | 01.05.2008 22:11 | 34 KB |
| Aircraft/Do_128-6/Documentation/files/Radar_d.jpg | 12.05.2008 01:23 | 35 KB |
| Aircraft/Do_128-6/Documentation/files/Realism_Settings.jpg | 04.04.2008 03:10 | 64 KB |
| Aircraft/Do_128-6/Documentation/files/Realism_Settings_d.jpg | 23.06.2008 01:55 | 61 KB |
| Aircraft/Do_128-6/Documentation/files/RPM.gif | 13.05.2001 22:03 | 16 KB |
| Aircraft/Do_128-6/Documentation/files/schema-pt6a.gif | 17.12.2002 00:29 | 7 KB |
| Aircraft/Do_128-6/Documentation/files/Speedcharts.htm | 20.08.2008 16:52 | 2 KB |
| Aircraft/Do_128-6/Documentation/files/start.gif | 08.05.2001 23:34 | 12 KB |
| Aircraft/Do_128-6/Documentation/files/Synthetic_Vision_Approach.jpg | 30.05.2001 02:55 | 40 KB |
| Aircraft/Do_128-6/Documentation/files/torque.gif | 13.05.2001 22:08 | 17 KB |
| Aircraft/Do_128-6/Documentation/files/uk.gif | 28.08.2002 02:30 | 9 KB |
| Aircraft/Do_128-6/Documentation/files/Wiperspeed.gif | 07.01.2002 01:13 | 5 KB |
| Aircraft/Do_128-6/Documentation/Info.txt | 27.04.2006 16:29 | 9 KB |
| Aircraft/Do_128-6/Documentation/Legal Notice.txt | 13.01.2006 18:10 | 608 B |
| Aircraft/Do_128-6/Documentation/RadarApproaches.doc | 27.04.2006 17:29 | 84 KB |
| Aircraft/Do_128-6/INSTALL.txt | 26.08.2008 01:35 | 7 KB |
| Aircraft/Do_128-6/Installation_Deutsch.txt | 26.08.2008 01:35 | 8 KB |
| Aircraft/Do_128-6/model/ | 23.08.2008 23:03 | |
| Aircraft/Do_128-6/model/DO 128-6 D-IBUF FS2K2 v1.mdl | 06.03.2004 19:40 | 2 MB |
| Aircraft/Do_128-6/model/model.cfg | 22.08.2008 22:56 | 43 B |
| Aircraft/Do_128-6/panel/ | 23.08.2008 23:03 | |
| Aircraft/Do_128-6/panel/dfd_hsi70.gau | 07.11.2001 02:35 | 692 KB |
| Aircraft/Do_128-6/panel/dfd_hsi70_0001.GAU | 09.08.2005 01:08 | 692 KB |
| Aircraft/Do_128-6/panel/dfd_i_omi.gau | 02.03.2000 14:09 | 40 KB |
| Aircraft/Do_128-6/panel/dfd_i_omi_0001.GAU | 09.08.2005 01:03 | 40 KB |
| Aircraft/Do_128-6/panel/dfd_i_omi_0002.GAU | 09.08.2005 01:08 | 40 KB |
| Aircraft/Do_128-6/panel/dfd_m_omi.gau | 02.03.2000 14:12 | 40 KB |
| Aircraft/Do_128-6/panel/dfd_m_omi_0001.GAU | 09.08.2005 01:03 | 40 KB |
| Aircraft/Do_128-6/panel/dfd_m_omi_0002.GAU | 09.08.2005 01:08 | 40 KB |
| Aircraft/Do_128-6/panel/dfd_o_omi.gau | 02.03.2000 14:13 | 40 KB |
| Aircraft/Do_128-6/panel/dfd_o_omi_0001.GAU | 09.08.2005 01:03 | 40 KB |
| Aircraft/Do_128-6/panel/dfd_o_omi_0002.GAU | 09.08.2005 01:08 | 40 KB |
| Aircraft/Do_128-6/panel/D-IBUF main.BMP | 15.01.2005 04:29 | 285 KB |
| Aircraft/Do_128-6/panel/D-IBUF overhead complete.bmp | 12.05.2006 01:56 | 1 MB |
| Aircraft/Do_128-6/panel/D-IBUF radio sm.bmp | 31.10.2002 21:04 | 53 KB |
| Aircraft/Do_128-6/panel/D-IBUF throttle-fuel-start.BMP | 21.09.2002 22:44 | 477 KB |
| Aircraft/Do_128-6/panel/D-IBUF upper.BMP | 01.11.2002 13:51 | 204 KB |
| Aircraft/Do_128-6/panel/Do128-6.wiper.gau | 09.09.2002 23:15 | 396 KB |
| Aircraft/Do_128-6/panel/Do128-6_V2.gau | 22.08.2008 02:16 | 2 MB |
| Aircraft/Do_128-6/panel/Do128-6_V2_XML.cab | 11.08.2008 13:27 | 416 KB |
| Aircraft/Do_128-6/panel/F16_AST_Radar80.cab | 22.08.2008 23:03 | 22 KB |
| Aircraft/Do_128-6/panel/hghb.txt | 22.08.2008 23:23 | 4 KB |
| Aircraft/Do_128-6/panel/hghb_bu_brake.gau | 16.03.1998 01:44 | 52 KB |
| Aircraft/Do_128-6/panel/HGHB_HW_ATTITUDE.gau | 07.11.2001 02:34 | 322 KB |
| Aircraft/Do_128-6/panel/HGHB_HW_ATTITUDE_0001.GAU | 09.08.2005 01:08 | 322 KB |
| Aircraft/Do_128-6/panel/HGHB_PC9_STBY_AI.gau | 10.12.1998 19:30 | 303 KB |
| Aircraft/Do_128-6/panel/HGHB_PC9_STBY_AI_0001.GAU | 09.08.2005 01:08 | 303 KB |
| Aircraft/Do_128-6/panel/hghb_uni_altimeter.gau | 18.12.2003 01:15 | 206 KB |
| Aircraft/Do_128-6/panel/Icon_SPEEDS.bmp | 11.08.2008 13:01 | 1 KB |
| Aircraft/Do_128-6/panel/panel.cfg | 22.08.2008 23:18 | 12 KB |
| Aircraft/Do_128-6/panel/VC_CPmain.bmp | 08.08.2005 20:59 | 188 KB |
| Aircraft/Do_128-6/panel/VC_ENGmain.bmp | 08.08.2005 21:01 | 185 KB |
| Aircraft/Do_128-6/panel/VC_Fuel-Start.bmp | 10.08.2005 22:16 | 321 KB |
| Aircraft/Do_128-6/panel/VC_Overhead_panel.bmp | 10.08.2005 15:08 | 821 KB |
| Aircraft/Do_128-6/panel/VC_Pmain.bmp | 08.08.2005 21:00 | 188 KB |
| Aircraft/Do_128-6/panel/VC_Radios.bmp | 08.08.2005 21:01 | 96 KB |
| Aircraft/Do_128-6/panel/ZVG2002.cab | 22.08.2008 23:00 | 21 KB |
| Aircraft/Do_128-6/sound/ | 23.08.2008 23:03 | |
| Aircraft/Do_128-6/sound/CASTALL.WAV | 03.03.2001 03:00 | 80 KB |
| Aircraft/Do_128-6/sound/door_large_close.wav | 10.04.2003 02:06 | 132 KB |
| Aircraft/Do_128-6/sound/door_large_open.wav | 10.04.2003 02:06 | 116 KB |
| Aircraft/Do_128-6/sound/kan1shut.wav | 09.03.2005 22:25 | 341 KB |
| Aircraft/Do_128-6/sound/kan1strt.wav | 09.03.2005 22:25 | 435 KB |
| Aircraft/Do_128-6/sound/kan2strt.wav | 09.03.2005 22:25 | 354 KB |
| Aircraft/Do_128-6/sound/kapr.wav | 18.04.2001 08:19 | 37 KB |
| Aircraft/Do_128-6/sound/kbn1shut.wav | 09.03.2005 22:25 | 341 KB |
| Aircraft/Do_128-6/sound/kbn1strt.wav | 09.03.2005 22:25 | 435 KB |
| Aircraft/Do_128-6/sound/kbn2strt.wav | 09.03.2005 22:25 | 354 KB |
| Aircraft/Do_128-6/sound/kbpr.wav | 18.04.2001 08:19 | 24 KB |
| Aircraft/Do_128-6/sound/left_idle_prop.wav | 05.04.2003 20:35 | 38 KB |
| Aircraft/Do_128-6/sound/left_idle_turb.wav | 05.04.2003 20:35 | 39 KB |
| Aircraft/Do_128-6/sound/leftmax_prop.wav | 05.04.2003 20:36 | 58 KB |
| Aircraft/Do_128-6/sound/leftmax_turb.wav | 05.04.2003 20:36 | 58 KB |
| Aircraft/Do_128-6/sound/mmflaps.wav | 18.04.2001 08:20 | 49 KB |
| Aircraft/Do_128-6/sound/Readme_LM_KASndEnhPck_v31.txt | 13.03.2005 02:46 | 3 KB |
| Aircraft/Do_128-6/sound/right_idle_prop.wav | 21.04.2003 14:32 | 44 KB |
| Aircraft/Do_128-6/sound/right_idle_turb.wav | 21.04.2003 14:33 | 45 KB |
| Aircraft/Do_128-6/sound/rightmax_prop.wav | 21.04.2003 14:33 | 61 KB |
| Aircraft/Do_128-6/sound/rightmax_turb.wav | 21.04.2003 14:33 | 55 KB |
| Aircraft/Do_128-6/sound/sound.cfg | 23.06.2007 03:48 | 6 KB |
| Aircraft/Do_128-6/sound/xkan1shut.wav | 20.02.2005 15:56 | 225 KB |
| Aircraft/Do_128-6/sound/xkan1strt.wav | 20.02.2005 15:56 | 228 KB |
| Aircraft/Do_128-6/sound/xkan2strt.wav | 20.02.2005 15:56 | 81 KB |
| Aircraft/Do_128-6/sound/xleft2.wav | 12.10.2002 01:33 | 65 KB |
| Aircraft/Do_128-6/sound/xleft3.wav | 12.10.2002 01:29 | 97 KB |
| Aircraft/Do_128-6/sound/xright2.wav | 12.10.2002 01:34 | 65 KB |
| Aircraft/Do_128-6/sound/xright3.wav | 12.10.2002 01:30 | 97 KB |
| Aircraft/Do_128-6/texture/ | 23.08.2008 23:03 | |
| Aircraft/Do_128-6/texture/blades_L.bmp | 27.01.2004 03:26 | 512 KB |
| Aircraft/Do_128-6/texture/blades_t.bmp | 08.12.2003 21:15 | 256 KB |
| Aircraft/Do_128-6/texture/Eng_Pylons_L.bmp | 27.01.2004 02:34 | 128 KB |
| Aircraft/Do_128-6/texture/Eng_Pylons_T.bmp | 27.01.2004 02:31 | 64 KB |
| Aircraft/Do_128-6/texture/Engines_L.bmp | 27.01.2004 02:51 | 512 KB |
| Aircraft/Do_128-6/texture/Engines_t.bmp | 16.12.2005 01:51 | 1 MB |
| Aircraft/Do_128-6/texture/EXT_TANKS_L.bmp | 27.01.2004 02:45 | 128 KB |
| Aircraft/Do_128-6/texture/EXT_TANKS_T.bmp | 10.12.2003 23:16 | 64 KB |
| Aircraft/Do_128-6/texture/fuselage_L.bmp | 27.01.2004 01:46 | 2 MB |
| Aircraft/Do_128-6/texture/fuselage_t.bmp | 06.03.2004 20:53 | 1 MB |
| Aircraft/Do_128-6/texture/LDN_GEARS_T.bmp | 11.01.2004 20:30 | 64 KB |
| Aircraft/Do_128-6/texture/LIGHTS_T.bmp | 29.02.2004 21:26 | 16 KB |
| Aircraft/Do_128-6/texture/LND_GEARS_L.bmp | 27.01.2004 03:21 | 128 KB |
| Aircraft/Do_128-6/texture/ROD_T.bmp | 01.03.2004 01:06 | 4 KB |
| Aircraft/Do_128-6/texture/spin_prop.bmp | 17.09.2005 04:20 | 85 KB |
| Aircraft/Do_128-6/texture/Spiner_L.bmp | 31.12.2002 20:24 | 2 KB |
| Aircraft/Do_128-6/texture/Spiner_t.bmp | 24.10.2003 00:12 | 21 KB |
| Aircraft/Do_128-6/texture/Tail_L.bmp | 27.01.2004 02:01 | 2 MB |
| Aircraft/Do_128-6/texture/Tail_T.bmp | 28.01.2004 23:40 | 1 MB |
| Aircraft/Do_128-6/texture/tires_L.bmp | 27.01.2004 03:24 | 128 KB |
| Aircraft/Do_128-6/texture/tires_t.bmp | 08.12.2003 16:04 | 64 KB |
| Aircraft/Do_128-6/texture/WIN_L.bmp | 27.01.2004 03:48 | 8 KB |
| Aircraft/Do_128-6/texture/WIN_L_show.bmp | 01.09.2005 01:41 | 8 KB |
| Aircraft/Do_128-6/texture/WIN_T.bmp | 27.01.2004 03:46 | 4 KB |
| Aircraft/Do_128-6/texture/WIN_T_show.bmp | 01.09.2005 01:44 | 12 KB |
| Aircraft/Do_128-6/texture/WINGS_L.bmp | 29.02.2004 19:39 | 2 MB |
| Aircraft/Do_128-6/texture/WINGS_T.bmp | 06.03.2004 20:17 | 1 MB |
| Effects/fx_CII_wing.fx | 25.07.2005 03:09 | 1 KB |
| Sound/1000Hz.wav | 27.03.2001 00:47 | 15 KB |
| Sound/click.wav | 21.12.1998 17:05 | 2 KB |
| Sound/Click3.wav | 01.04.1999 04:54 | 604 B |
| Sound/Click4.wav | 01.04.1999 04:54 | 680 B |
| Sound/dfd_audiopanel.wav | 14.02.2000 17:47 | 482 B |
| Sound/HGHB_Click2.wav | 08.04.1999 13:45 | 5 KB |
| Sound/HGHB_Click3.wav | 01.04.1999 04:54 | 2 KB |
| Sound/hghb_rsw_cl1.wav | 01.04.1999 04:54 | 1 KB |
| Sound/hghb_rsw_cl2.wav | 01.04.1999 04:54 | 680 B |
| Aircraft/Do_128-6/Documentation/files/audio-control-panel.jpg | 24.08.2008 20:07 | 3 KB |
| avsim_su.diz | 17.10.2009 00:21 | 406 B |
| Итого: | 36 MB | |
Dornier 128-6
| Rating: 5!
Aircraft used in the armed forces for more than ten countries around the world as a coherent and patrol. Equipped with two Pratt & Whitney turboprop RT6A-110 400 hp In my opinion worthy of attention plane.
→ Size:
12 MB
→ Date:
16 years ago (16.10.2009 20:46)
→ Author:
Mathias Elsaesser
→ Approved by moderator:
Lenya69
→ License:
Freeware - Free version, Unlimited Distribution
→ Downloaded:
2235 time(s)