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[fltsim.0] | ||
title=BAvMM_A333_BAW_EC-NBP | ||
model=RR | ||
texture=BAW_EC-NBP | ||
sim=TFS_A333 | ||
atc_airline= | ||
atc_id= | ||
atc_heavy=1 | ||
ui_manufacturer=Airbus | ||
ui_type=A330-300 | ||
ui_variation=Evelop (British Airways Lease) | ||
atc_parking_types=GATE | ||
atc_parking_codes=BAW | ||
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[General] | ||
atc_type=AIRBUS | ||
atc_model=A333 | ||
editable=0 | ||
performance= | ||
Category=airplane | ||
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||
[pitot_static] | ||
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI | ||
pitot_heat=1.000000 | ||
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[weight_and_balance] | ||
max_gross_weight = 151000 | ||
empty_weight = 103170 | ||
reference_datum_position = 0, 0, 0 | ||
empty_weight_CG_position = 18, 0, 0 | ||
empty_weight_pitch_MOI = 3160000 | ||
empty_weight_roll_MOI = 3262183 | ||
empty_weight_yaw_MOI = 4337024 | ||
empty_weight_coupled_MOI = 0 | ||
max_number_of_stations = 9 | ||
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station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" | ||
station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" | ||
station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" | ||
station_load.3 = "1360.0, 25.5, 0.0, 0.0, First Class" | ||
station_load.4 = "8160.0, 11.0, 0.0, 0.0, Coach 3-10" | ||
station_load.5 = "8160.0, -10.0, 0.0, 0.0, Coach 11-18" | ||
station_load.6 = "7140.0, -30.5, 0.0, 0.0, Coach 19-25" | ||
station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" | ||
station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" | ||
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[lights] | ||
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing | ||
light.0 = 3, -22.71, -93.98, 5.436, fx_navred | ||
light.1 = 2, -22.10, -93.49, 5.423, fx_strobe | ||
light.2 = 3, -22.71, 93.98, 5.436, fx_navgre | ||
light.3 = 2, -22.10, 93.49, 5.423, fx_strobe | ||
light.4 = 3, -101.57, 0, 6.05, fx_navwhi | ||
light.5 = 2, -101.57, 0, 6.05, fx_strobe | ||
light.6 = 1, 25.29, 0, -10.42, fx_beaconb | ||
light.7 = 1, 7.29, 0, 9.84, fx_beaconb | ||
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[GeneralEngineData] | ||
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop | ||
engine_type = 1 | ||
fuel_flow_scalar = 1 | ||
min_throttle_limit = -0.1400 | ||
max_contrail_temperature =-27 | ||
engine.0 = 8.55, -30.47, -8.53, | ||
engine.1 = 8.55, 30.47, -8.53, | ||
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[TurbineEngineData] | ||
fuel_flow_gain=0.002 //Gain on fuel flow.. | ||
inlet_area=19.6 //Square Feet, engine nacelle inlet area | ||
rated_N2_rpm=29920 //RPM, second stage compressor rated value | ||
static_thrust=28000 //Lbs, max rated static thrust at Sea Level | ||
afterburner_available=0 //Afterburner available? | ||
reverser_available=1 //Thrust reverser available? | ||
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[jet_engine] | ||
thrust_scalar=1.0 | ||
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[effects] | ||
wake = fx_wake | ||
water = fx_spray | ||
dirt = fx_tchdrt | ||
concrete = fx_sparks | ||
//(Disabled by FSFX_PFX_Effect)touchdown = fx_tchdwn, 1 | ||
windshield_rain_effect_available = 1 | ||
//(Disabled by FSFX_PFX_Effect)contrail=fx_A_I_Contrail | ||
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touchdown = fsfx_PFX_5451754250764F397544796D3272546754336958544C5A414562734555613368 //FSFX_PFX_Effect | ||
contrail = fsfx_PFX_3263496B6372304972726C58476F30724A6E6642493438546C5369687130724B //FSFX_PFX_Effect | ||
vaportrail_l = fsfx_PFX_34674C5337767A6562726E38486D6958794975646E594E357576646268717151 //FSFX_PFX_Effect | ||
vaportrail_r = fsfx_PFX_34674C5337767A6562726E38486D6958794975646E594E357576646268717151 //FSFX_PFX_Effect | ||
SnowEngineWash = fsfx_PFX_3263496B6372304972726D3730684D4C74476972496C62414973497447333165 //FSFX_PFX_Effect | ||
WetEngineWash = fsfx_PFX_3263496B6372304972726B7A6C552B3438463674612F5544396C754D5A516C55 //FSFX_PFX_Effect | ||
WheelSnowSpray = fsfx_PFX_77755038474E6775336E5979767345506C38564553346F68304B333832395476 //FSFX_PFX_Effect | ||
WheelWetSpray = fsfx_PFX_77755038474E6775336E61444251543245683042306545366578725A326A6E6A //FSFX_PFX_Effect | ||
SkidPavement = fsfx_PFX_77755038474E6775336E5A6C3231714C4F656D4E4E48576F4544356C6F36676F //FSFX_PFX_Effect | ||
[fuel] | ||
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) | ||
fuel_type = 2 | ||
number_of_tank_selectors = 1 | ||
electric_pump = 0 | ||
Center1 = 0, 0, 0, 2313, 0 | ||
LeftMain = -3, -19, 0, 1500, 0 | ||
RightMain = -3, 19, 0, 1500, 0 | ||
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[contact_points] | ||
static_pitch = -0.93 | ||
static_cg_height = 17.56 | ||
tailwheel_lock = 0 | ||
gear_system_type = 0 | ||
max_number_of_points = 7 | ||
point.0 = 1, 80.0300, 0.0000, -16.813, 1574.8, 0, 1.442, 55.92, 0.8, 2.5, 0.6, 6, 6, 0, 220, 250 | ||
point.1 = 1, -4.5822, -18.34, -18.7828, 1574.8, 1, 1.442, 0, 1, 2.5, 0.9, 8.9, 8.9, 2, 220, 250 | ||
point.2 = 1, -4.5822, 18.34, -18.7828, 1574.8, 2, 1.442, 0, 1, 2.5, 0.9, 9.1, 9.1, 3, 220, 250 | ||
point.3 = 2, 6.04, -62.83, -8.15, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 | ||
point.4 = 2, 6.04, 62.83, -8.15, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 | ||
point.5 = 2, -50.8, 0, -8.63, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 | ||
point.6 = 2, 92.81, 0, -6.84, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 | ||
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[keyboard_response] | ||
elevator = 150, 250 | ||
aileron = 150, 250 | ||
rudder = 150, 250 | ||
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[airplane_geometry] | ||
wing_area = 2337.0 | ||
wing_span = 126.46 | ||
wing_root_chord = 28.58 | ||
wing_dihedral = 6.19 | ||
wing_incidence = 1.0 | ||
wing_twist = -0.5 | ||
oswald_efficiency_factor = 0.85 | ||
wing_winglets_flag = 0 | ||
wing_sweep = 28 | ||
wing_pos_apex_lon = 18.58 | ||
wing_pos_apex_vert = 0 | ||
htail_area = 338.0 | ||
htail_span = 50.15 | ||
htail_pos_lon = -59.65 | ||
htail_pos_vert = 0 | ||
htail_incidence = 0.0 | ||
htail_sweep = 34 | ||
vtail_area = 224.0 | ||
vtail_span = 28.77 | ||
vtail_sweep = 42 | ||
vtail_pos_lon = -50.76 | ||
vtail_pos_vert = 5.53 | ||
elevator_area = 70.5 | ||
aileron_area = 26.9 | ||
rudder_area = 56.2 | ||
elevator_up_limit = 22.5 | ||
elevator_down_limit = 19.5 | ||
aileron_up_limit = 20.0 | ||
aileron_down_limit = 20.0 | ||
rudder_limit = 26.0 | ||
elevator_trim_limit = 20.0 | ||
spoiler_limit = 60.0 | ||
aileron_to_spoileron_gain = 3 | ||
spoiler_handle_available = 1 | ||
min_ailerons_for_spoilerons = 10 | ||
min_flaps_for_spoilerons = 0 | ||
spoilerons_available = 1 | ||
auto_spoiler_available=1 | ||
spoiler_extension_time=2.000000 | ||
positive_g_limit_flaps_up=4.000000 | ||
positive_g_limit_flaps_down=3.000000 | ||
negative_g_limit_flaps_up=-3.000000 | ||
negative_g_limit_flaps_down=-2.000000 | ||
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[electrical] | ||
max_battery_voltage = 24 | ||
generator_alternator_voltage = 28 | ||
max_generator_alternator_amps = 60 | ||
engine_generator_map = 1,1,0,0 | ||
electric_always_available = 1 | ||
flap_motor = 0, 5, 17 | ||
gear_motor = 0, 5, 17 | ||
autopilot = 0, 5, 17 | ||
avionics_bus = 0, 5, 17 | ||
avionics = 1, 5, 17 | ||
pitot_heat = 0, 2, 17 | ||
additional_system = 0, 2, 17 | ||
marker_beacon = 1, 2, 17 | ||
gear_warning = 0, 2, 17 | ||
fuel_pump = 0, 5, 17 | ||
starter1 = 0, 20, 17 | ||
light_nav = 0, 5, 17 | ||
light_beacon = 0, 5, 17 | ||
light_landing = 0, 5, 17 | ||
light_taxi = 0, 5, 17 | ||
light_strobe = 0, 5, 17 | ||
light_panel = 0, 5, 17 | ||
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[flight_tuning] | ||
cruise_lift_scalar=1.2 | ||
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=0.8 | ||
aileron_trim_effectiveness=1.0 | ||
rudder_trim_effectiveness=1.0 | ||
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[forcefeedback] | ||
gear_bump_nose_magnitude = 3000 | ||
gear_bump_nose_direction = 18000 | ||
gear_bump_nose_duration = 250000 | ||
gear_bump_left_magnitude = 2700 | ||
gear_bump_left_direction = 35500 | ||
gear_bump_left_duration = 250000 | ||
gear_bump_right_magnitude = 2700 | ||
gear_bump_right_direction = 00500 | ||
gear_bump_right_duration = 250000 | ||
ground_bumps_magnitude1 = 1300 | ||
ground_bumps_angle1 = 08900 | ||
ground_bumps_intercept1 = 3.0 | ||
ground_bumps_slope1 = 0.20 | ||
ground_bumps_magnitude2 = 200 | ||
ground_bumps_angle2 = 09100 | ||
ground_bumps_intercept2 = 1.075 | ||
ground_bumps_slope2 = 0.035 | ||
crash_magnitude1 = 10000 | ||
crash_direction1 = 01000 | ||
crash_magnitude2 = 10000 | ||
crash_direction2 = 9000 | ||
crash_period2 = 75000 | ||
crash_duration2 = 2500000 | ||
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[gear_warning_system] | ||
gear_warning_available = 1 //Normal | ||
pct_throttle_limit = 0.1 //Percent throttle that activates warning | ||
flap_limit_idle = 5.0 //Flap angle that activates warning at idle | ||
flap_limit_power = 25.5 //Flap angle that activates warning at above idle | ||
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[brakes] | ||
parking_brake = 1 //Parking brake available | ||
toe_brakes_scale = 0.485 //Brake scalar | ||
auto_brakes=4 | ||
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[hydraulic_system] | ||
normal_pressure = 3000.0 //PSI | ||
electric_pumps = 0 //no electric pumps | ||
engine_map = 1,1,0,0 //pumps on Eng1,2 | ||
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[Views] | ||
eyepoint=43.7, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum | ||
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[flaps.0] //Trailing Edge Flaps | ||
type = 1 // 1 - tail, 2 - lead | ||
span-outboard = 0.8 // 0.0 .. 1.0 | ||
extending-time = 20 // seconds | ||
flaps-position.0 = 0 // degrees | ||
flaps-position.1 = 1 // degrees | ||
flaps-position.2 = 2 // degrees | ||
flaps-position.3 = 5 // degrees | ||
flaps-position.4 = 10 // degrees | ||
flaps-position.5 = 15 // degrees | ||
flaps-position.6 = 25 // degrees | ||
flaps-position.7 = 30 // degrees | ||
flaps-position.8 = 40 // degrees | ||
damaging-speed = 250 // KIAS | ||
blowout-speed = 300 // KIAS | ||
lift_scalar = 0.1 | ||
drag_scalar = 0.0 | ||
pitch_scalar= 1.0 | ||
system_type = 1 //Hydraulic | ||
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[flaps.1] //Inboard Leading Edge Flaps | ||
type = 2 // 1 - tail, 2 - lead | ||
span-outboard = 0.8 // 0.0 .. 1.0 | ||
extending-time = 4 // seconds | ||
flaps-position.0 = 0 // | ||
flaps-position.4 = 0.5 | ||
flaps-position.5 = 1.0 // | ||
damaging-speed = 250 // KIAS | ||
blowout-speed = 300 // KIAS | ||
lift_scalar = 0.1 | ||
drag_scalar = 0.0 | ||
pitch_scalar= 1.0 | ||
system_type = 1 //Hydraulic | ||
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[flaps.2] //Outboard Leading Edge Slat | ||
type = 2 // 1 - tail, 2 - lead | ||
span-outboard = 0.8 // 0.0 .. 1.0 | ||
extending-time = 7 // seconds | ||
flaps-position.0 = 0 // | ||
flaps-position.4 = 0.5 | ||
flaps-position.5 = 1.0 // | ||
damaging-speed = 250 // KIAS | ||
blowout-speed = 300 // KIAS | ||
lift_scalar = 0.1 | ||
drag_scalar = 0.0 | ||
pitch_scalar= 1.0 | ||
system_type = 1 //Hydraulic | ||
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[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 | ||
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[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 | ||
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[attitude_indicators] | ||
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro | ||
attitude_indicator.0 = 1 | ||
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[turn_indicators] | ||
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro | ||
turn_indicator.0=0,0 | ||
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[exits] | ||
number_of_exits = 2 | ||
exit_rate.0 = 0.4 ;Percent per second | ||
exit_rate.1 = 0.4 ;Percent per second | ||
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[autopilot] | ||
autopilot_available=1 | ||
flight_director_available=1 | ||
default_vertical_speed=1800 | ||
autothrottle_available=1 | ||
autothrottle_arming_required=1 | ||
autothrottle_max_rpm = 90 | ||
autothrottle_takeoff_ga=1 | ||
pitch_takeoff_ga=8 ; | ||
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=33.0 | ||
max_bank_acceleration=1.8 | ||
max_bank_velocity=3.00 | ||
max_throttle_rate=0.10 | ||
nav_proportional_control=12.00 | ||
nav_integrator_control=0.25 | ||
nav_derivative_control=0.00 | ||
nav_integrator_boundary=2.50 | ||
nav_derivative_boundary=0.00 | ||
gs_proportional_control=25.0 | ||
gs_integrator_control=0.53 | ||
gs_derivative_control=0.00 | ||
gs_integrator_boundary=0.70 | ||
gs_derivative_boundary=0.00 | ||
yaw_damper_gain = 1.0 | ||
yaw_slip_control_gain=0.000000 | ||
yaw_control_uses_trim=0.000000 | ||
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[Reference Speeds] | ||
flaps_up_stall_speed=150.0 //Knots True (KTAS) | ||
full_flaps_stall_speed=120.0 //Knots True (KTAS) | ||
cruise_speed=494.0 //Knots True (KTAS) | ||
max_mach = 0.85 | ||
max_indicated_speed = 330 //Red line (KIAS) | ||
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[stall_warning] | ||
type=2 | ||
stick_shaker=1 | ||
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[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 |
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[models] | ||
normal=TFS_A333_RR_P3Dv4 |
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[FLTSIM] | ||
alias=..\Airplanes\B737_800\soundai |
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