Quote

Отлично смотрится!!!

cow, on 12 Июль 2010 — 00:52, said:

Спасибо! http://f02.cdn.avsim.su/forum/public/style_emoticons/default/clapping.gif

Скоро выложу на сайт, исправил некоторые погрешности (в плане дверей) и добавил эффектов. Ждите. http://f02.cdn.avsim.su/forum/public/style_emoticons/default/biggrin.gif

GixxeR, 12 Июль 2010 — 01:12, сказал(а):

Конечно, а по другому никак, глядишь, несколько мегабайт, да освободится на жестаке. http://f02.cdn.avsim.su/forum/public/style_emoticons/default/sarcastic.gif

GixxeR, 12 Июль 2010 — 01:16, сказал(а):

Это точно))) Хотя у меня жестак один и на 640 ГБ, стоит 2 сима перегруженных, и у меня ещё больше половины места свободно… http://f02.cdn.avsim.su/forum/public/style_emoticons/default/sarcastic.gifhttp://f02.cdn.avsim.su/forum/public/style_emoticons/default/sarcastic.gifhttp://f02.cdn.avsim.su/forum/public/style_emoticons/default/sarcastic.gif

GixxeR, 12 Июль 2010 — 01:33, сказал(а):

А кто вообще знает, авторы Оверлэнда собираются дорабатывать кокпит и панель? Или это уже всё? Релиз?

GixxeR, on 13 Июль 2010 — 01:31, said:

S7, Rossiya, Aeroflot, Armavia, Air Astana — пока всё. Армавиа сделана на оригинальном ките, все текстуры мои, кроме Аэрофлота. Но ещё текстуры будут точно.

serg09, on 12 Июль 2010 — 21:55, said:

Вопрос уже исчерпан :sarcastic: :sarcastic:

[fltsim.0]
title=FSPAP A321 Ural Airlines — VQ-BCX
sim=FeelThere_A321CFM
model=cfm
panel=
sound=
texture=ural airlines
kb_checklists=
kb_reference=a321
atc_id=VQ-BCX
atc_id_color=0xffffffff
atc_airline=SVERDLOVSK AIR
atc_flight_number=236
ui_manufacturer=Simmer’s Sky
ui_type=Airbus A321
ui_variation=Ural Airlines
description=Overland Co.,Ltd. Products — Airbus A321nnTextures and livery by Denis MinaevnnL1 Cabin Door [Shift+E] then [1]nCargo Door Operate with Door Display GaugenL2 Cabin Door Operate with Door Display GaugenL/R After Cabin Door Operate with Door Display Gauge

LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -11.14, -55.2, 3.39, Fx_shockwave_beaconh
light.1=3, -11.14, 55.2, 3.39, Fx_shockwave_beaconh
light.2=2, -11.52, -55.3, 3.39, Fx_shockwave_strobe
light.3=2, -11.52, 55.3, 3.39, Fx_shockwave_strobe
light.4=6, 55.55, 0.0, -4.84, fx_shockwave_landing_light_747_nose // Shockwave light
light.5=1, 6.32, 0.0, 9.45, fx_navredm
light.6=5, 4.15, -6.7, -2.50, fx_Shockwave_landing_light
light.7=5, 4.15, 6.7, -2.50, fx_Shockwave_landing_light
light.8=4, 60.90, 0.0, 6.70, fx_vclight

[SMOKESYSTEM]
smoke.0 = -10, 8, 18, Opensky_revspray
smoke.1 = 10, 8, -18, Opensky_revspray

[General]
atc_type=Airbus
atc_model=A321
editable=1
performance=Cruise Speedt.78 MachnMaximum Ranget2,059 nmnService Ceilingt36,089 ftnMax Takeoff Weightt138,500 lbnSeatingtt147 to 168nCargo Capacityt1,373 CU ftn

[pitot_static]
vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]
max_gross_weight=206100 // (pounds)
empty_weight =106300 // (pounds)

reference_datum_position= 5, 0, -4.4 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position= 0, 0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0 = «155.0, 41.0, -1.5, 0.0, Pilot» //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = «155.0, 41.0, 1.5, 0.0, Co-Pilot» //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = «410.0, 0.0, 0.0, 0.0, Crew» //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = «6640.0, 24.0, 0.0, 0.0, Coach 1 — 9» //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = «8560.0, -2.0, 0.0, 0.0, Coach 10 -20» //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = «6960.0, -30.5, 0.0, 0.0, Coach 21-30» //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=3246600
empty_weight_roll_MOI= 2889520
empty_weight_yaw_MOI= 2963200
empty_weight_coupled_MOI=0

[GROUND_REACTION]
MAX_STEERING_ANGLE=75

[flight_tuning]
cruise_lift_scalar =1.0002
parasite_drag_scalar =1.000
induced_drag_scalar =1.1
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.0
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000

[GeneralEngineData]
engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=3.25, -18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=3.25, 18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0000
min_throttle_limit=-0.499939
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain=0.001 //Gain on fuel flow
inlet_area=30 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920.000000
static_thrust=32000.000000
afterburner_available=0
reverser_available=1 //Thrust reverser available?

[jet_engine]
thrust_scalar=1.0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 200
electric_always_available = 1
flap_motor = 0, 0 , 17.0
gear_motor = 0, 0 , 17.0
autopilot = 0, 0 , 17.0
avionics_bus = 0, 0 , 17.0
avionics = 0, 0 , 17.0
pitot_heat = 0, 0 , 17.0
additional_system = 0, 0 , 17.0
marker_beacon = 0, 0 , 17.0
gear_warning = 0, 0 , 17.0
fuel_pump = 0, 0 , 17.0
starter1 = 0, 0 , 17.0
starter2 = 0, 0 , 17.0
light_nav = 0, 0 , 17.0
light_beacon = 0, 0 , 17.0
light_landing = 0, 0 , 17.0
light_taxi = 0, 0 , 17.0
light_strobe = 0, 0 , 17.0
light_panel = 0, 0 , 17.0
light_cabin = 0, 0 , 17.0
auto_brakes = 0, 0 , 17.0
standby_vacuum = 0, 0 , 17.0
hydraulic_pump = 0, 0 , 17.0
fuel_transfer_pump = 0, 0 , 17.0
light_recognition = 0, 0 , 17.0
light_wing = 0, 0 , 17.0
light_logo = 0, 0 , 17.0
directional_gyro = 0, 0 , 17.0
directional_gyro_slaving = 0, 0 , 17.0

//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)

[contact_points]
point.0=1, 54.80, 0.00, -10.61, 1500, 0, 1.25, 60.12, 0.50, 2.1, 0.8135,11.0, 13.2, 0, 0.0, 0.0
point.1=1, -3.95, -11.58, -11.56, 2200, 1, 2.15, 0.00, 1.51, 2.0, 0.7470, 9.7, 14.1, 2, 0.0, 0.0
point.2=1, -3.95, 11.58, -11.56, 2200, 2, 2.15, 0.00, 1.51, 2.0, 0.7470, 9.7, 14.1, 3, 0.0, 0.0

point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

max_number_of_points=21

static_pitch=-0.22 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=14.56 //feet, altitude of CG when at rest on the ground
gear_system_type=0

[Views]
eyepoint=61.73, -1.65, 5.25 //(feet) longitudinal, lateral, vertical distance from reference datum

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=20.000000
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=0.0
flaps-position.2=15.0 //nominal value should be10 but we need big effect RY
flaps-position.3=20.0 //ditto to accomodate flap 2
flaps-position.4=26.0 //ditto to accomodate flap 2
flaps-position.5=35.0 //ditto to accomodate flap 2

[Flaps.1]
type=2
span-outboard=0.800
extending-time=20.000
system_type=1
damaging-speed=232.000
blowout-speed=250.000
lift_scalar=0.3
drag_scalar=0.2
pitch_scalar=0.0
flaps-position.0=0
flaps-position.1=18.0
flaps-position.2=18.0
flaps-position.3=22.0
flaps-position.4=22.0
flaps-position.5=27.0 //Hydraulic

[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

[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

[exits]
number_of_exits=2
exit.0 = 0.25, 53.5, -5.5, 2.8, 0
exit.1 = 0.4, -23.5, 5.0, -2.2, 1

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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1700.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=0.8
max_pitch_velocity_lo_alt=1.0
max_pitch_velocity_hi_alt=1.0
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=3.0
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

[fuel]
Center1 = 0, 0, 0, 2118, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = 0, -19, 0, 2001, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain= 0, 19, 0, 2001, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=2
electric_pump=1

[airplane_geometry]
wing_area=1320.000000
wing_span=111.9
wing_root_chord=12.000000
wing_dihedral=5
wing_incidence=1.5
wing_twist=1
oswald_efficiency_factor=0.8723
wing_winglets_flag=1
wing_sweep=22
wing_pos_apex_lon=15.00000
wing_pos_apex_vert=0.000000
htail_area=328.000000
htail_span=40.000000
htail_pos_lon=-50.000000
htail_pos_vert=0.000000
htail_incidence=2.993774
htail_sweep=0.000000
vtail_area=249.000000
vtail_span=17.991665
vtail_sweep=0.000000
vtail_pos_lon=-50.000000
vtail_pos_vert=20.500000
elevator_area=70.500000
aileron_area=26.800000
rudder_area=56.200000
elevator_up_limit=28
elevator_down_limit=22
aileron_up_limit=22
aileron_down_limit=20
rudder_limit=32
elevator_trim_limit=18
spoiler_limit=50
spoilerons_available=1
aileron_to_spoileron_gain=3.000000
min_ailerons_for_spoilerons=9.0
min_flaps_for_spoilerons=0.000000

[Reference Speeds]
flaps_up_stall_speed=180.000000 // at MTW
full_flaps_stall_speed=132.000000// at MTW
cruise_speed=320
max_indicated_speed=352.000000
max_mach=0.84

[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=0.86
parking_brake=1
auto_brakes=4
differential_braking_scale = 1.0

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=10.04

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=2

[turn_indicators]
turn_indicator.0=1,0

[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.12,0.11 ;Percent per second

[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.0

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[deice_system]
structural_deice_type=0