[fltsim.0] title=PSS A330-300 GE PAL ui_variation=PSS A330-300 GE PAL sim=A333 ui_type=A330-300 GE sound=GE model=geNOsat texture=Philippine atc_airline=Philippine panel= checklists= atc_id=AB333 atc_flight_number=PS333 atc_heavy=0 ui_manufacturer=Airbus visual_damage=1 description=PSS A330/A340 Pro Series With R.E.A.L Features. COPYRIGHT 2002 PHOENIX SIMULATION SOFTWARE [fltsim.1] title=PSS A330-300 GE PAL 2 ui_variation=PSS A330-300 GE PAL sim=A333 ui_type=A330-300 GE sound=GE model=geNOsat texture=pal atc_airline=Philippine panel= checklists= atc_id=AB333 atc_flight_number=PS333 atc_heavy=0 ui_manufacturer=Airbus visual_damage=1 description=PSS A330/A340 Pro Series With R.E.A.L Features. COPYRIGHT 2002 PHOENIX SIMULATION SOFTWARE //////////////////////////////////////////////////////////////////// //fc868c4fb4b45a22f8677c4353517b88 [LIGHTS] Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1 = 1, 7.800, 0.000, -5.500, fx_beaconb , light.2 = 1, 0.200, 0.000, 14.500, fx_beaconh , light.3 = 4, 82.500, 0.000, 8.000, fx_vclight , light.4 = 2, -40.200, -93.100, 13.380, fx_strobe320pa, light.5 = 2, -40.200, 93.100, 13.380, fx_strobe320pa, light.6 = 5, 18.000, 27.000, -4.000, Opensky_wing_light, light.7 = 5, 19.933, 8.827, -4.368, Opensky_wing_light, light.8 = 5, 18.000, -27.000, -4.000, Opensky_wing_light, light.9 = 5, 19.933, -8.827, -5.368, Opensky_wing_light, light.10 = 5, 19.700, 19.000, -6.000, Opensky_nacelle_refl, light.11 = 5, 19.700, -19.000, -6.000, Opensky_nacelle_refl, light.12 = 3, -116.000, 0.000, 11.420, Opensky_nav_yellow , light.13 = 2, -116.000, 0.100, 11.300, fx_strobe320pa , [exits] number_of_exits=2 exit_rate.0=0.25 exit_rate.1=0.25 //[Views] //eyepoint=77.0, -1.8, 5.5 [Views] VIEW_FORWARD_WINDOWS=MAIN_PANEL VIEW_FORWARD_DIR=9.0, 0.0, 0.0 ;VIEW_FORWARD_DIR=3.0, 0.0, 0.0 VIEW_FORWARD_ZOOM=1.0 eyepoint=37.729659,-1.307210,3.614050 [General] atc_type=AIRBUS atc_model=A330 performance= [pitot_static] vertical_speed_time_constant=99 [GROUND_REACTION] MAX_STEERING_ANGLE=78 [GeneralEngineData] engine_type=1 Engine.0=12,-30,-6 Engine.1=12, 30,-6 fuel_flow_scalar=0.85 min_throttle_limit=-0.499939 [jet_engine] thrust_scalar = 1.0 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 contrail=fx_A_I_Contrail [direction_indicators] direction_indicator.0=3,0 [Radios] 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 [Flaps.0] type=1 span-outboard=1.0 extending-time=13 system_type=1 flaps-position.0= 0 flaps-position.1= 2 flaps-position.2= 8 flaps-position.3=14 flaps-position.4=22 flaps-position.5=32 damaging-speed = 250 blowout-speed = 2670 lift_scalar = 2.3 drag_scalar = 1.0 pitch_scalar= 1.0 [forcefeedback] // default feedback.. change as you need. //fc868c4fb4b45a22f8677c4353517b88 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 [WEIGHT_AND_BALANCE] //do not change reference_datum_position=0.000000,0.000000,0.000000 max_number_of_stations=50 pss_num_class = THREE_CLASS // Load Editor Cfg Value station_load.0 = 450, 0.0, 0.0, 0.0 //Weight Crew (lbs) LEAVE station_load.1 = 3000, 0.0, 0.0, 0.0 //Weight Galleys (lbs) LEAVE station_load.2 = 33971, 0.0, 0.0, 0.0 //Weight Baggage (lbs) station_load.3 = 11389, 0.0, 0.0, 0.0 //Weight Cargo (lbs) station_load.4 = 1650, 0.0, 0.0, 0.0 //Weight First Class (lbs) station_load.5 = 4950, 0.0, 0.0, 0.0 //Weight Business Class (lbs) station_load.6 = 34200, 0.0, 0.0, 0.0 //Weight Economy Class (lbs) empty_weight = 264995.3 empty_weight_roll_MOI = 4900000 empty_weight_pitch_MOI = 33000000 empty_weight_yaw_MOI = 41500000 empty_weight_coupled_MO I= 0.000000 empty_weight_CG_position =0.000000,0.000000,0.000000 max_gross_weight =509046.8 empty_weight_coupled_MOI=0.000000 *************************************************** [fuel] LeftMain = -5.0, -19.0, 0.0,12060, 949 RightMain = -5.0, 19.0, 0.0,12060, 949 fuel_type=2 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=3892 wing_span=197 wing_root_chord=40 wing_dihedral=6 wing_incidence=0.7 wing_twist=-0.8 oswald_efficiency_factor=0.6 wing_winglets_flag=1 wing_sweep=29.7 wing_pos_apex_lon=45 wing_pos_apex_vert=0 htail_area=333 htail_span=134 htail_pos_lon=-95.0 htail_pos_vert=0 htail_incidence=2.993774 htail_sweep=0 vtail_area=513 vtail_span=134 vtail_sweep=29 vtail_pos_lon=-95.0 vtail_pos_vert=8.5 elevator_area=90.5 aileron_area=36.8 rudder_area=56.2 elevator_up_limit=30 elevator_down_limit=15 aileron_up_limit=25 aileron_down_limit=25 rudder_limit=31.6 elevator_trim_limit=30 spoiler_limit=25 spoilerons_available=1 aileron_to_spoileron_gain=1.5 min_ailerons_for_spoilerons=10 min_flaps_for_spoilerons=0.0 //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=1.0, 65.5, 0.00, -11.4, 1574.803, 0.0, 1.312, 78.0, 1.0, 1.50, 1.957, 17.0, 17.0, 0.00, 0.0, 0.0 point.1=1.0, -25.21, -18.3, -12.8, 1574.803, 1.0, 1.512, 0.0, 1.0, 1.50, 1.988, 18.0, 18.3, 2.00, 0.0, 0.0 point.2=1.0, -25.21, 18.3, -12.8, 1574.803, 2.0, 1.512, 0.0, 1.0, 1.50, 1.988, 18.3, 18.0, 3.00, 0.0, 0.0 point.3=2.0, -14.16, -47.3, 0.00, 787.401, 0.0, 0.000, 0.0, 0.0, 0.00, 0.000, 0.00, 0.00, 5.00, 0.0, 0.0 point.4=2.0, -14.16, 47.3, 0.00, 787.401, 0.0, 0.000, 0.0, 0.0, 0.00, 0.000, 0.00, 0.00, 6.00, 0.0, 0.0 point.5=2.0, -54.00, 0.0, 2.83, 787.401, 0.0, 0.000, 0.0, 0.0, 0.00, 0.000, 0.00, 0.00, 9.00, 0.0, 0.0 point.6=2.0, 42.66, 0.0, -3.75, 787.401, 0.0, 0.000, 0.0, 0.0, 0.00, 0.000, 0.00, 0.00, 4.00, 0.0, 0.0 point.7=5.0, 0.0, 0.0, 0.0, 1600, 0.0, 0.0, 50.0, 0.0, 0.0, 1.00, 1.0, 1.0, 0, 0.0, 0.0 static_pitch=-0.7 static_cg_height=12.114977 gear_system_type=0 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=28.72 rated_N2_rpm=29920 static_thrust=72000.00 afterburner_available=0 reverser_available=1 max_contrail_temperature = -30 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=800 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=8 autothrottle_max_rpm=97 pitch_takeoff_ga=4 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 [Reference Speeds] flaps_up_stall_speed=155 full_flaps_stall_speed=112 cruise_speed=528 max_indicated_speed=350.000000 max_mach=0.861992 [brakes] toe_brakes_scale=0.712497 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [flight_tuning] cruise_lift_scalar = 0.85 parasite_drag_scalar = 1.1 induced_drag_scalar = 0.75 elevator_effectiveness = 1.0 aileron_effectiveness = 1.1 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 0.7 yaw_stability = 1.2 elevator_trim_effectiveness = 1.2 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [fuel] Center1= 0.000, 0.000, -4.000, 16260.000, 0.000 Center2= -83.676, 0.000, 0.000, 1617.000, 3.000 LeftMain= -7.000, -37.983, 0.000, 11147.000, 3.000 RightMain= -7.000, 37.983, 0.000, 11147.000, 3.000 LeftAux= -13.000, -70.269, 0.000, 974.000, 3.000 RightAux= -13.000, 70.269, 0.000, 974.000, 3.000 [SMOKESYSTEM] smoke.0= 90.0,-38.3,-63.0, fx_contrail_320 smoke.1= 90.0,-38.3,63.0, fx_contrail_320 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=1