Antonov An-22 Просмотр ZIP-архива
AIRCRAFT/Antonov An-22/Aircraft.cfg
[fltsim.0]
title=ANTONOV AN-22 AEROFLOT
sim=Antonov An-22
model=
panel=V1
sound=
texture=aeroflot
kb_checklists=
kb_reference=An-22_ref
ui_manufacturer=Antonov
ui_type=An-22
ui_variation=Aeroflot
atc_id=RA-09344
atc_heavy=1
atc_flight_number=308
visual_damage=1
atc_parking_codes=AFL
atc_parking_types=CARGO
description= Unveiled to the West in 1965, the Antonov An-22 Antey (Антей in Russian; NATO reporting name Cock) was the world's largest aircraft, until the advent of the Lockheed C-5 Galaxy. Powered by 4 contrarotating turboprops, the design remains the world's largest turboprop-powered airplane. The An-22 was originally built for the Soviet Air Force and Aeroflot, the state airline. Approximately 45 remained in service by the mid-1990s, mostly with the Russian Air Force, but these are slowly being replaced by the bigger turbofan-powered Antonov An-124. Currently one An-22 is in use for civilian cargo duties by Antonov Airlines.
[fltsim.1]
title=ANTONOV AN-22 ANTONOV DESIGN BUREAU
sim=Antonov An-22
model=
panel=V2
sound=
texture=adb
kb_checklists=
kb_reference=An-22_ref
ui_manufacturer=Antonov
ui_type=An-22
ui_variation=Antonov Design Bureau
atc_id=UR-09307
atc_heavy=1
atc_flight_number=307
visual_damage=1
atc_parking_codes=ADB
atc_parking_types=CARGO
description= Unveiled to the West in 1965, the Antonov An-22 Antey (Антей in Russian; NATO reporting name Cock) was the world's largest aircraft, until the advent of the Lockheed C-5 Galaxy. Powered by 4 contrarotating turboprops, the design remains the world's largest turboprop-powered airplane. The An-22 was originally built for the Soviet Air Force and Aeroflot, the state airline. Approximately 45 remained in service by the mid-1990s, mostly with the Russian Air Force, but these are slowly being replaced by the bigger turbofan-powered Antonov An-124. Currently one An-22 is in use for civilian cargo duties by Antonov Airlines.
[GENERAL]
atc_type=ANTONOV
atc_model=AN22
editable=0
performance=Antonov An-22 Antheus\nMaximum Speed: 400 kts/460.3 mph/740.8 km\/h\nCruise Speed: 325 kts/374 mph/601.9 km\/h\nPower: 4x11,185kW (15,000shp) Kuznetsov (Kuibyshev) NK12MA turboprops\nPropeller: Eight blades countra-rotating propellers\nMaximum Range: 5,940 nm/6,835.6 sm/11,000 km - 3100km (max payload)\nService Ceiling: 26,300 ft/8,000 m\nFuel Capacity: 91,000 Kg/126,400 L\nEmpty Weight: 261,793 lbs/118,727 kg\nMaximum Gross Weight: 551,160 lb/250,000 kg\nLength: 190 ft/57.92 m\nWingspan: 211.4 ft/64.49 m\nHeight: 41 ft/12.53 m\nSeating: Up to 29 \nUseful Load: 176,350 lb/80,000 kg
[PITOT_STATIC]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight = 551876 // (pounds)
empty_weight = 251655 // (pounds)
reference_datum_position=0.00,0.00,0.00 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-4.0,0.00,0.00 // (feet) longitudinal, lateral, vertical distance from specified datum
//reference_datum_position = 83.5, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
//empty_weight_CG_position = -90.5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 50000, 5.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 50000, -10.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//MOMENTS OF INERTIA
empty_weight_pitch_MOI = 12000000. //24223159
empty_weight_roll_MOI = 6000000. //15352310
empty_weight_yaw_MOI = 11000000. //39531785
empty_weight_coupled_MOI = 0
[FUEL]
//Center1 = -83.5, 0.0, -7.0, 19545.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//Center2 = -193.5, 0.0, 6.0, 3300.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//LeftMain = -112.0, -35.0, -4.0, 16720.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//LeftAux = -118.5, -52.0, -3.0, 500.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//RightMain = -112.0, 35.0, -4.0, 16720.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//RightAux = -118.5, 52.0, -3.0, 500.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 = 0.00, 0.0, -7.0, 7267.0, 10.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = 0.00, 0.0, 6.0, 7554.0, 10.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = 0.00, -35.0, -4.0, 7083.0, 10.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable gallons)
LeftAux = 0.00, -52.0, -3.0, 3084.0, 10.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.00, 35.0, -4.0, 7083.0, 10.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = 0.00, 52.0, -3.0, 3084.0, 10.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[AIRPLANE_GEOMETRY]
wing_area = 3713.0000 //5825.0 Square feet
wing_span = 211.4000 //Feet
wing_root_chord = 25.0000 //48.8 Feet
wing_dihedral = 2.5000 //1.5 / 7.0 Degrees
wing_incidence = 2.0 //Degrees
wing_twist = 0.0 //-1.0 Degrees
oswald_efficiency_factor= 0.88 //0.98 / 0.68 Measure of lift effeciency of wing
wing_winglets_flag = 0 //1 Are winglets available?
wing_sweep = 4.000 //37.5 Degrees, wing leading edge
wing_pos_apex_lon = 8.000 //0.0 / -68.2 Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 10.000 //Feet, vertical distance from reference point, positive going up
htail_area = 670.0 //1470 Square feet
htail_span = 66.0 //72.8 Feet
htail_pos_lon = -90.0 //-210.0 Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 15.0 //37.5 Degrees, horizontal tail leading edge
vtail_area = 800. //Square feet
vtail_span = 37.1 //Feet, tip to body
vtail_sweep = 15.0 //45.0 Degrees, vertical tail leading edge
vtail_pos_lon = -90.000 //-198.5 Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 26.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 100.0 //327 Square feet
aileron_area = 100.0 //225 Square feet
rudder_area = 100.0 //230 Square feet
elevator_up_limit = 25 //Degrees
elevator_down_limit = 15 //Degrees
aileron_up_limit = 25 //Degrees
aileron_down_limit = 15 //Degrees
rudder_limit = 31.5 //Degrees
elevator_trim_limit = 20 //Degrees
spoiler_limit = 45 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[REFERENCE SPEEDS]
flaps_up_stall_speed = 155.0 //Knots True (KTAS)
full_flaps_stall_speed = 125.0 //Knots True (KTAS)
cruise_speed = 325.0 //Knots True (KTAS)
max_indicated_speed = 400.0 //Knots True (KTAS)
max_mach = 0.7000
[FLIGHT_TUNING]
cruise_lift_scalar = 1.6
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.45
elevator_effectiveness = 1.0
aileron_effectiveness = 1.8
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 0.9
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[TURBINEENGINEDATA]
fuel_flow_gain = 0.002300 //Gain on fuel flow
inlet_area =21.380000 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 12920.000000 //RPM, second stage compressor rated value
static_thrust =32630.000000 //56750 Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[TURBOPROP_ENGINE]
power_scalar=1.0
maximum_torque=10614.3602
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=1.1
propeller_type=1
propeller_diameter=20.333333
rotation= -1, -1, -1, -1
propeller_blades=4
propeller_moi=5.706520
beta_max=49.99
beta_min=15.0
min_gov_rpm=13900.00
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=500.000
beta_feather=93.3200000
power_absorbed_cf=1.000000
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=8.0
minimum_reverse_beta=0.0 //19.0 for LSL
rotation=-1 -1
[JET_ENGINE]
thrust_scalar = 0.925
[FLAPS.0]
type= 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 / 1.0
extending-time = 21 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 15 // degrees
flaps-position.2 = 25 // degrees
flaps-position.3 = 35 // degrees
damaging-speed = 230 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 0.99 //0.8
drag_scalar = 0.8 //1.0
pitch_scalar = 1.0 //0.9
system_type = 1 //Hydraulic
[AUTOPILOT]
autopilot_available =1
flight_director_available =1
default_vertical_speed = 1000.0
autothrottle_available =1
autothrottle_arming_required = 0
autothrottle_max_rpm = 95
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8.000000
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 = 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
[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)
point.0 = 1, 60.00, 0.0, -17.16, 4000.0, 0, 2.0, 70.0, 1.5, 1.2, 0.700, 9.0, 8.0, 0, 220, 250
point.1 = 1, -11.41, -10.0, -18.0, 3000.0, 1, 2.0, 0.00, 3.0, 1.2, 0.700, 11.0, 9.0, 2, 220, 250
point.2 = 1, -11.41, 10.0, -18.0, 3000.0, 2, 2.0, 0.00, 3.0, 1.2, 0.700, 11.0, 9.0, 3, 220, 250
point.3 = 2, -10.6, -103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0
point.4 = 2, -10.6, 103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0
point.5 = 2, 43.0, 0.0, 0.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0
point.6 = 2, -90.7, 0.0, 0.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
static_pitch = 4.5 //1.5
static_cg_height = 18.6
gear_system_type=0
[GENERALENGINEDATA]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 20.0, -40., -2.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 20.0, -20., -2.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = 20.0, 20., -2.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = 20.0, 40., -2.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.250000
max_contrail_temperature = -39.0
[VIEWS]
eyepoint = -19.05, -1.97, 9.4 //Longitude, Latitude and Vertical position from Reference Point, (FEET)
[ELECTRICAL]
// BusType, MaxAmpLoad, MinVoltage //BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 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
[RADIOS]
// Radio Type: availiable, standby frequency, glide slope
Audio.1 = 1,0
Com.1 = 1,0
Com.2 = 1,0
Nav.1 = 1,0,1
Nav.2 = 1,0,0
Adf.1 = 1,0
Adf.2 = 1,0
Transponder.1 = 1,0
Marker.1 = 1,0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -3.0, -105.5, 4.5, AN22_navred ,
light.1 = 3, -3.0, 105.5, 4.5, AN22_navgre ,
light.2 = 3, -88.2, -22.56, -3.5, AN22_navwhi ,
light.3 = 3, -88.2, 22.56, -3.5, AN22_navwhi ,
light.4 = 2, -3.0, -105.5, 4.5, AN22_strobe ,
light.5 = 2, -3.0, 105.5, 4.5, AN22_strobe ,
light.6 = 1, -54.1, 0.0, 9, AN22_beacon ,
light.7 = 1, 18.0, 0.0, -12.0, AN22_beacon ,
[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
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
windshield_rain_effect_available = 1
[SMOKESYSTEM]
smoke.0=0.00, 2.00, 45.00, FX_C130_SMOKE //fx_smoke_rx1
smoke.1=0.00, 2.00, 22.00, FX_C130_SMOKE //fx_smoke_rx1
smoke.2=0.00, 2.00, -20.00, FX_C130_SMOKE //fx_smoke_rx1
smoke.3=0.00, 2.00, -45.00, FX_C130_SMOKE //fx_smoke_rx1
[EXITS]
number_of_exits = 2
exit_rate.0 = 0.4 //Percent per second
exit_rate.1 = 0.1 //Percent per second
[FORCEFEEDBACK]
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 = 35500 // 0 - 35999 degrees
gear_bump_left_duration = 250000 // in microseconds
gear_bump_right_magnitude = 2700 // 0 - 10000
gear_bump_right_direction = 00500 // 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 = 0.7 //1.241798
parking_brake = 1.0 //1.000000
[GEAR_WARNING_SYSTEM]
gear_warning_available =1
pct_throttle_limit = 0.099976
flap_limit_power = 25.496622
flap_limit_idle = 5.042029
[HYDRAULIC_SYSTEM]
electric_pumps = 0
engine_map = 1,1,1,1
normal_pressure = 3000.000000
[STALL_WARNING]
type = 1
[ATTITUDE_INDICATORS]
attitude_indicator.0 = 1
[TURN_INDICATORS]
turn_indicator.0 = 1
AN-22.zip
| Имя файла | Дата | Размер |
|---|---|---|
| GAUGES/i21_cfg/i21_ppm.cfg_0 | 06.06.2004 16:40 | 1 KB |
| GAUGES/i21_cfg/I21_PPM.CFG.org | 06.01.2005 05:53 | 1 KB |
| GAUGES/i21_cfg/I21_PPM.CFG | 27.08.2006 23:59 | 940 B |
| GAUGES/i21_cfg/I21_PPM.BAK | 12.06.2004 22:55 | 1 KB |
| GAUGES/Pr/kln90b.gau | 13.08.2006 14:22 | 644 KB |
| GAUGES/Active_Engine_Smoke.cab | 05.08.2006 03:30 | 606 B |
| GAUGES/AN22.cab | 26.03.2006 23:23 | 5 KB |
| GAUGES/AN22.apu.gau | 22.05.2006 04:18 | 724 KB |
| GAUGES/AN22.electro.gau | 11.12.2003 13:17 | 248 KB |
| GAUGES/AN22.FUEL_TEMP.cab | 29.07.2006 00:56 | 14 KB |
| GAUGES/AN22.GAU1.gau | 08.12.2003 19:12 | 2 MB |
| GAUGES/AN22.landing_lights.gau | 03.10.1999 16:32 | 86 KB |
| GAUGES/AN22.msrp.gau | 04.02.2004 21:07 | 116 KB |
| GAUGES/AN22.panel_lights.gau | 03.10.1999 09:32 | 86 KB |
| GAUGES/AN22.PNO1.gau | 09.11.2003 23:23 | 1 MB |
| GAUGES/AN22.RADIO.gau | 23.12.2003 21:24 | 2 MB |
| GAUGES/AN22.sau.gau | 05.03.2004 18:18 | 2 MB |
| GAUGES/AN22.strobe_lights.gau | 03.10.1999 16:32 | 86 KB |
| GAUGES/AN22.toggles.cab | 07.11.2002 07:56 | 30 KB |
| GAUGES/AN22.toggles.light.green1.cab | 19.04.2005 06:57 | 25 KB |
| GAUGES/AN22.toggles.light.red1.cab | 25.03.2006 04:53 | 25 KB |
| GAUGES/AN22_ALTIMETER.GAU | 08.06.2006 02:17 | 332 KB |
| GAUGES/AN22_amp.gau | 29.05.2006 13:37 | 100 KB |
| GAUGES/AN22_ANNUN.cab | 03.06.2006 23:46 | 3 MB |
| GAUGES/AN22_CALLSIGN.cab | 27.07.2003 06:15 | 1021 B |
| GAUGES/AN22_Flaps.cab | 15.05.2006 01:57 | 8 KB |
| GAUGES/AN22_fuel.gau | 19.07.2006 00:23 | 602 KB |
| GAUGES/AN22_fuelquantity.cab | 10.04.2006 22:43 | 3 KB |
| GAUGES/AN22_icon.cab | 08.05.2006 23:24 | 11 KB |
| GAUGES/AN22_KI-13.gau | 03.08.2000 07:14 | 176 KB |
| GAUGES/AN22_OIL_PRESSURE.1.GAU | 03.04.2006 00:35 | 48 KB |
| GAUGES/AN22_OIL_PRESSURE.1_0001.GAU | 29.07.2006 01:28 | 48 KB |
| GAUGES/AN22_OIL_PRESSURE.2.GAU | 03.04.2006 00:41 | 48 KB |
| GAUGES/AN22_OIL_PRESSURE.2_0001.GAU | 29.07.2006 01:28 | 48 KB |
| GAUGES/AN22_OIL_PRESSURE.3.GAU | 03.04.2006 00:44 | 48 KB |
| GAUGES/AN22_OIL_PRESSURE.3_0001.GAU | 29.07.2006 01:28 | 48 KB |
| GAUGES/AN22_OIL_PRESSURE.4.GAU | 03.04.2006 00:47 | 48 KB |
| GAUGES/AN22_OIL_PRESSURE.4_0001.GAU | 29.07.2006 01:28 | 48 KB |
| GAUGES/An22_Parking_Brake.GAU | 26.08.1999 04:41 | 68 KB |
| GAUGES/An22_Parking_Brake_0001.GAU | 29.07.2006 01:28 | 68 KB |
| GAUGES/An22_Parking_Brake_0002.GAU | 29.07.2006 01:28 | 68 KB |
| GAUGES/An22_Parking_Brake_0003.GAU | 29.07.2006 01:28 | 68 KB |
| GAUGES/AN22_reverse.cab | 08.08.2006 19:06 | 4 KB |
| GAUGES/AN22_Trim.gau | 24.03.2006 02:19 | 133 KB |
| GAUGES/AN22_volt.gau | 29.05.2006 13:51 | 116 KB |
| GAUGES/AN22_WindSpeed.gau | 26.03.2006 17:07 | 173 KB |
| GAUGES/AN22_WindSpeed_0001.GAU | 29.07.2006 01:28 | 173 KB |
| GAUGES/AN22_WindSpeed_0002.GAU | 29.07.2006 01:28 | 173 KB |
| GAUGES/An24_Main_V2.gau | 22.05.2005 20:17 | 11 MB |
| GAUGES/groza_154_4_01.gau | 01.04.2006 13:29 | 784 KB |
| GAUGES/Harrier_pushback2.cab | 13.12.2005 22:23 | 11 KB |
| GAUGES/STT_AN22_N_V1_03.gau | 11.02.2006 16:57 | 1 MB |
| GAUGES/STT_AN22_V1_39.gau | 20.06.2006 07:06 | 18 MB |
| GAUGES/STT_AN22_View_V1_3.gau | 11.02.2006 16:17 | 3 MB |
| GAUGES/STT_ClockNav1_R_V1_0.gau | 16.10.2005 09:58 | 212 KB |
| GAUGES/STT_I21_N1_V1_08.gau | 08.01.2006 14:40 | 744 KB |
| GAUGES/STT_I21_N2_V1_08.gau | 08.01.2006 14:40 | 744 KB |
| GAUGES/STT_RP_TCAS_V0_17L.gau | 11.02.2006 16:36 | 3 MB |
| GAUGES/STT_Tu154_V3_24.gau | 02.06.2005 15:00 | 10 MB |
| Effects/FX_C130_SMOKE.fx | 07.08.2006 23:22 | 2 KB |
| Sound/HarrierPushback2/ENG/Sound.ini | 14.12.2005 00:22 | 797 B |
| Sound/HarrierPushback2/ENG/PB11_Brakes.wav | 06.11.2003 23:50 | 30 KB |
| Sound/HarrierPushback2/ENG/PB08_PushbackRoll.wav | 04.11.2003 23:27 | 121 KB |
| Sound/HarrierPushback2/ENG/PB06_SoftClick.wav | 07.03.2005 15:40 | 551 B |
| Sound/HarrierPushback2/ENG/PB05_Conversation5.wav | 30.10.2003 10:14 | 135 KB |
| Sound/HarrierPushback2/ENG/PB04_Conversation4.wav | 30.10.2003 10:21 | 182 KB |
| Sound/HarrierPushback2/ENG/PB03_Conversation3.wav | 04.11.2003 23:21 | 55 KB |
| Sound/HarrierPushback2/ENG/PB02_Conversation2.wav | 30.10.2003 10:07 | 76 KB |
| Sound/HarrierPushback2/ENG/PB01_Conversation1.wav | 27.10.2003 04:17 | 189 KB |
| Sound/HarrierPushback2/RUS/Sound.ini | 25.12.2005 03:46 | 797 B |
| Sound/HarrierPushback2/RUS/PB11_Brakes.wav | 06.11.2003 23:50 | 30 KB |
| Sound/HarrierPushback2/RUS/PB08_PushbackRoll.wav | 04.11.2003 23:27 | 121 KB |
| Sound/HarrierPushback2/RUS/PB06_SoftClick.wav | 07.03.2005 15:40 | 551 B |
| Sound/HarrierPushback2/RUS/PB05_Conversation5.wav | 02.03.2004 09:32 | 83 KB |
| Sound/HarrierPushback2/RUS/PB04_Conversation4.wav | 02.03.2004 09:36 | 97 KB |
| Sound/HarrierPushback2/RUS/PB03_Conversation3.wav | 09.10.2000 10:54 | 45 KB |
| Sound/HarrierPushback2/RUS/PB01_Conversation1.wav | 02.03.2004 09:27 | 264 KB |
| Sound/IL76/ssos_old.wav | 10.11.2003 04:59 | 54 KB |
| Sound/IL76/ssos.wav | 31.01.2002 02:52 | 37 KB |
| Sound/IL76/AGR_COVER.WAV | 10.11.2003 04:59 | 824 B |
| Sound/IL76/AGR_CLICK.WAV | 10.11.2003 04:59 | 890 B |
| AIRCRAFT/Antonov An-22/Antonov An-22.air | 03.07.2006 20:14 | 9 KB |
| AIRCRAFT/Antonov An-22/AN-22_ref.htm | 24.07.2006 03:16 | 127 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/an22dvigatel.bmp | 29.05.2006 19:29 | 256 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/an22dvigatel_L.bmp | 15.03.2006 05:06 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/an22fyuzelyazh.bmp | 29.05.2006 19:29 | 1 MB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/an22fyuzelyazh_L.bmp | 09.06.2002 00:12 | 1 MB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/an22krylo.bmp | 29.05.2006 19:30 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/an22kryloPrav.bmp | 29.05.2006 19:30 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/an22stabilizator.bmp | 29.05.2006 19:31 | 128 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/an22vnutriGruzOtseka.bmp | 29.05.2006 19:31 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/an22vnutriGruzOtseka_LM.bmp | 29.05.2006 19:31 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/descript.ion | 14.06.2002 07:43 | |
| AIRCRAFT/Antonov An-22/texture.aeroflot/panelz.bmp | 29.05.2006 19:31 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/prop_cessna_182s.bmp | 20.03.2003 04:24 | 256 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/shiny.bmp | 25.02.2003 16:17 | 128 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/Thumbs.db | 13.06.2006 07:47 | 49 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/trans.bmp | 15.03.2006 05:10 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.aeroflot/vint.bmp | 13.02.2003 11:55 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.adb/an22dvigatel.bmp | 29.05.2006 19:24 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.adb/an22dvigatel_L.bmp | 15.03.2006 05:06 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.adb/an22fyuzelyazh.bmp | 29.05.2006 19:25 | 1 MB |
| AIRCRAFT/Antonov An-22/texture.adb/an22fyuzelyazh_L.bmp | 29.05.2006 19:25 | 1 MB |
| AIRCRAFT/Antonov An-22/texture.adb/an22krylo.bmp | 29.05.2006 19:26 | 256 KB |
| AIRCRAFT/Antonov An-22/texture.adb/an22kryloPrav.bmp | 29.05.2006 19:26 | 256 KB |
| AIRCRAFT/Antonov An-22/texture.adb/an22stabilizator.bmp | 29.05.2006 19:26 | 128 KB |
| AIRCRAFT/Antonov An-22/texture.adb/an22vnutriGruzOtseka.bmp | 29.05.2006 19:27 | 256 KB |
| AIRCRAFT/Antonov An-22/texture.adb/an22vnutriGruzOtseka_LM.bmp | 29.05.2006 19:27 | 256 KB |
| AIRCRAFT/Antonov An-22/texture.adb/panelz.bmp | 29.05.2006 19:27 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.adb/propSlow.bmp | 20.03.2003 04:24 | 256 KB |
| AIRCRAFT/Antonov An-22/texture.adb/prop_cessna_182s.bmp | 20.03.2003 04:24 | 256 KB |
| AIRCRAFT/Antonov An-22/texture.adb/shiny.bmp | 25.02.2003 21:17 | 128 KB |
| AIRCRAFT/Antonov An-22/texture.adb/Thumbs.db | 09.06.2006 20:06 | 41 KB |
| AIRCRAFT/Antonov An-22/texture.adb/trans.bmp | 15.03.2006 05:10 | 64 KB |
| AIRCRAFT/Antonov An-22/texture.adb/vint.bmp | 29.05.2006 19:28 | 256 KB |
| AIRCRAFT/Antonov An-22/panel.V2/NAV_FRONT_V2.bmp | 27.06.2006 10:40 | 2 MB |
| AIRCRAFT/Antonov An-22/panel.V2/panel.cfg | 28.08.2006 23:34 | 29 KB |
| AIRCRAFT/Antonov An-22/panel.V1/ENGINEER.bmp | 28.08.2006 21:35 | 5 MB |
| AIRCRAFT/Antonov An-22/panel.V1/I21.bmp | 30.05.2006 14:06 | 516 KB |
| AIRCRAFT/Antonov An-22/panel.V1/MAIN.bmp | 15.07.2006 05:46 | 5 MB |
| AIRCRAFT/Antonov An-22/panel.V1/NAVIGATOR.bmp | 15.07.2006 05:42 | 5 MB |
| AIRCRAFT/Antonov An-22/panel.V1/NAVIGATOR2.bmp | 08.07.2006 04:41 | 2 MB |
| AIRCRAFT/Antonov An-22/panel.V1/NAVMINI.bmp | 24.06.2006 03:10 | 181 KB |
| AIRCRAFT/Antonov An-22/panel.V1/NAV_FRONT_V1.bmp | 21.06.2006 21:26 | 2 MB |
| AIRCRAFT/Antonov An-22/panel.V1/panel.cfg | 28.08.2006 23:33 | 29 KB |
| AIRCRAFT/Antonov An-22/panel.V1/SAU.BMP | 10.02.2006 04:50 | 64 KB |
| AIRCRAFT/Antonov An-22/panel.V1/Thumbs.db | 15.07.2006 12:16 | 164 KB |
| AIRCRAFT/Antonov An-22/panel.V1/UPPER.bmp | 25.06.2006 00:24 | 990 KB |
| AIRCRAFT/Antonov An-22/model/Antonov An-22.mdl | 04.03.2006 04:08 | 895 KB |
| AIRCRAFT/Antonov An-22/model/Model.cfg | 22.02.2003 01:52 | 32 B |
| AIRCRAFT/Antonov An-22/sound/bearflaph.wav | 27.12.1997 02:38 | 2 KB |
| AIRCRAFT/Antonov An-22/sound/bearflapl.wav | 27.12.1997 18:57 | 67 KB |
| AIRCRAFT/Antonov An-22/sound/bearflapt.wav | 25.12.1997 22:21 | 7 KB |
| AIRCRAFT/Antonov An-22/sound/beargrdn.wav | 12.12.1997 21:59 | 151 KB |
| AIRCRAFT/Antonov An-22/sound/beargrup.wav | 12.12.1997 21:59 | 138 KB |
| AIRCRAFT/Antonov An-22/sound/bearjb4.wav | 25.04.2000 02:46 | 170 KB |
| AIRCRAFT/Antonov An-22/sound/bearovspd.wav | 25.12.1997 22:25 | 38 KB |
| AIRCRAFT/Antonov An-22/sound/bearstall.wav | 25.12.1997 22:23 | 35 KB |
| AIRCRAFT/Antonov An-22/sound/beartchc.wav | 25.12.1997 22:23 | 10 KB |
| AIRCRAFT/Antonov An-22/sound/beartchl.wav | 25.12.1997 22:23 | 9 KB |
| AIRCRAFT/Antonov An-22/sound/beartchr.wav | 25.12.1997 22:23 | 11 KB |
| AIRCRAFT/Antonov An-22/sound/bearwarn.wav | 25.12.1997 22:24 | 70 KB |
| AIRCRAFT/Antonov An-22/sound/Sound.cfg | 11.05.2005 03:09 | 1 KB |
| AIRCRAFT/Antonov An-22/sound/xbearjb4.wav | 25.04.2000 14:37 | 171 KB |
| AIRCRAFT/Antonov An-22/sound/xrumblebear.wav | 30.01.2002 22:53 | 384 KB |
| README_An22.txt | 29.08.2006 13:37 | 11 KB |
| GAUGES/T154Kln90B.cab | 06.11.2005 21:22 | 618 B |
| GAUGES/TC_154b_14.cab | 19.06.2005 01:57 | 176 KB |
| Startup.doc | 29.08.2006 13:42 | 424 KB |
| Effects/AN22_beacon.fx | 12.02.2002 17:14 | 3 KB |
| Effects/AN22_navgre.fx | 15.01.2002 11:45 | 3 KB |
| Effects/AN22_navred.fx | 14.01.2002 23:52 | 3 KB |
| Effects/AN22_navwhi.fx | 28.10.2001 06:06 | 3 KB |
| Effects/AN22_strobe.fx | 12.12.2001 14:44 | 5 KB |
| AIRCRAFT/Antonov An-22/Aircraft.cfg | 29.08.2006 15:08 | 18 KB |
| avsim_ru.diz | 29.08.2006 23:07 | 620 B |
| Итого: | 101 MB | |
Antonov An-22
| Rating: 4.9!
This package contains not only the panel, but also a complete set of files needed for the Antonov 22. This panel is designed for FS2004 (FS9) only. We do not guarantee proper operation in any other version. To install, just follow carefully the instructions in the README.txt
→ Size:
22 MB
→ Date:
20 years ago (29.08.2006 18:40)
→ Author:
→ License:
Freeware - Free version, Unlimited Distribution
→ Downloaded:
7027 time(s)