[fltsim.0] title=Saudia B747SP-68 HZ-AIF sim=fsp747sp model=rr panel= sound= texture=aif atc_id=HZ-AIF atc_airline=Saudia atc_flight_number=020 atc_heavy=1 ui_manufacturer=Boeing ui_type=747-SP ui_variation=HZ-AIF description=A fim de atender as necessidades das companhias aéreas de voar longas distâncias, da costa Leste dos EUA até a Ásia, ou da Oeste até a Austrália, os engenheiros da Boeing desenvolveram o Boeing 747 SP (Special Performance), retirando 14,60 m da fuselagem e fazendo algumas pequenas mudanças aerodinâmicas, como aumentar a altura da deriva. Foram construídas 45 aeronaves desse modelo. Seu primeiro vôo foi no dia 04\/07\/75. [fltsim.1] title=Saudia B747SP-68 HZ-AIJ sim=fsp747sp model=rr panel= sound= texture=aij atc_id=HZ-AIJ atc_airline=Saudia atc_flight_number=021 atc_heavy=1 ui_manufacturer=Boeing ui_type=747-SP ui_variation=HZ-AIJ description=A fim de atender as necessidades das companhias aéreas de voar longas distâncias, da costa Leste dos EUA até a Ásia, ou da Oeste até a Austrália, os engenheiros da Boeing desenvolveram o Boeing 747 SP (Special Performance), retirando 14,60 m da fuselagem e fazendo algumas pequenas mudanças aerodinâmicas, como aumentar a altura da deriva. Foram construídas 45 aeronaves desse modelo. Seu primeiro vôo foi no dia 04\/07\/75. [fltsim.2] title=Saudia B747SP-68 HZ-HM1 sim=fsp747sp model=rr panel= sound= texture=hm1 atc_id=HZ-HM1 atc_airline=Saudia atc_flight_number=022 atc_heavy=1 ui_manufacturer=Boeing ui_type=747-SP ui_variation=HZ-HM1 description=A fim de atender as necessidades das companhias aéreas de voar longas distâncias, da costa Leste dos EUA até a Ásia, ou da Oeste até a Austrália, os engenheiros da Boeing desenvolveram o Boeing 747 SP (Special Performance), retirando 14,60 m da fuselagem e fazendo algumas pequenas mudanças aerodinâmicas, como aumentar a altura da deriva. Foram construídas 45 aeronaves desse modelo. Seu primeiro vôo foi no dia 04\/07\/75. [fltsim.3] title=Saudia B747SP-68 HZ-HM1B sim=fsp747sp model=rr panel= sound= texture=hm1b atc_id=HZ-HM1B atc_airline=Saudia atc_flight_number=023 atc_heavy=1 ui_manufacturer=Boeing ui_type=747-SP ui_variation=HZ-HM1B description=A fim de atender as necessidades das companhias aéreas de voar longas distâncias, da costa Leste dos EUA até a Ásia, ou da Oeste até a Austrália, os engenheiros da Boeing desenvolveram o Boeing 747 SP (Special Performance), retirando 14,60 m da fuselagem e fazendo algumas pequenas mudanças aerodinâmicas, como aumentar a altura da deriva. Foram construídas 45 aeronaves desse modelo. Seu primeiro vôo foi no dia 04\/07\/75. [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 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 [General] visual_damage=1 // 0=off, 1=on editable=1 atc_type=BOEING atc_model=B744 performance=Length: 184.9 ft.\nWing span: 195.8 ft.\nHeight: 65.5 ft.\nMax Takeoff Weight: 667'000 lbs..\nMax Taxi Weight:700'000 lbs.\nMax Landing Weight: 450'000 lbs.\nPower: 4 x Rolls Royce RB211-524D4. [WEIGHT_AND_BALANCE] 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=79000, -80.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) max_gross_weight=701000 // (pounds) empty_weight=330400 // (pounds) ;Moments of Inertia empty_weight_roll_MOI = 15352310 empty_weight_pitch_MOI = 24223159 empty_weight_yaw_MOI = 39531785 empty_weight_coupled_MOI = 0 [fuel] Center1=-83.5, 0.0, -7.0, 13200.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2=-193.5, 0.0, 6.0, 0.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-112.0, -35.0, -4.0, 17200.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=-118.5, -52.0, -3.0, 1320.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-112.0, 35.0, -4.0, 17200.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=-118.5, 52.0, -3.0, 1320.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area=5825.0 //Square feet wing_span=211.4 //Feet wing_root_chord=48.8 //Feet wing_dihedral=7.0 //Degrees wing_incidence=2.0 //Degrees wing_twist=-1.0 //Degrees oswald_efficiency_factor=0.68 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=37.5 //Degrees, wing leading edge wing_pos_apex_lon=-68.2 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0 //Feet, vertical distance from reference point, positive going up htail_area=1470 //Square feet htail_span=72.8 //Feet htail_pos_lon=-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=37.5 //Degrees, horizontal tail leading edge vtail_area=1060 //Square feet vtail_span=37.1 //Feet, tip to body vtail_sweep=45.0 //Degrees, vertical tail leading edge vtail_pos_lon=-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=327 //Square feet aileron_area=225 //Square feet rudder_area=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=0 //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 [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [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, -25.0, 0.0, -17.9, 1000.0, 0, 2.0, 70.0, 0.5, 3.5, 0.900, 9.0, 8.0, 0, 220, 250 point.1=1, -114.0, -18.0, -19.9, 2000.0, 1, 2.0, 13.0, 3.0, 2.5, 0.900, 11.0, 9.0, 2, 220, 250 point.2=1, -114.0, 18.0, -19.9, 2000.0, 2, 2.0, 13.0, 3.0, 2.5, 0.900, 11.0, 9.0, 3, 220, 250 point.3=2, -152.6, -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, -152.6, 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, 3.0, 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, -222.7, 0.0, 4.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 static_pitch=-0.5 static_cg_height=18.6 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=25 // seconds flaps-position.0=0=0.000000,0.000000 // degrees flaps-position.1=7.998491,0.000000 // degrees flaps-position.2=15.996982,0.000000 // degrees flaps-position.3=23.995472,0.000000 // degrees flaps-position.4=31.993963,0.000000 // degrees flaps-position.5=39.992454,0.000000 // degrees damaging-speed=200 // KIAS blowout-speed=250 // KIAS lift_scalar=0.7 drag_scalar=0.9 pitch_scalar=0.9 system_type=1 //Hydraulic [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=2 // seconds flaps-position.0=0 // degrees flaps-position.1=1.0 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=0.3 drag_scalar=0.1 pitch_scalar=0.1 system_type=1 //Hydraulic [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-107.5, -69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-76.0, -38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2=-76.0, 38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3=-107.5, 69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=60.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=56750 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 [Reference Speeds] flaps_up_stall_speed=140.0 //Knots True (KTAS) full_flaps_stall_speed=112.0 //Knots True (KTAS) cruise_speed=505.0 //Knots True (KTAS) [flight_tuning] cruise_lift_scalar=1.0 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=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [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 [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 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [autopilot] use_no_default_bank=1 use_no_default_pitch=1 autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; [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 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Com.2 = 0, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [SMOKESYSTEM] smoke.0=-40.00,-135.00,70.00, fx_smoke_rx smoke.1=-37.00,-118.00,38.00, fx_smoke_rx smoke.2=-37.00,-118.00, -38.00, fx_smoke_rx smoke.3=-40.00,-135.00, -70.00, fx_smoke_rx [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -118.30, -106.56, 1.59, fx_navredh , light.1=3, -118.30, 106.56, 1.59, fx_navgreh , light.2=3, -160.35, 0.00, 5.15, fx_navwhih , light.3=2, -120.30, -107.56, 1.59, fx_strobeh , light.4=2, -120.30, 107.56, 1.59, fx_strobeh , light.5=1, -15.05, 0.00, 15.00, fx_beaconh , light.6=1, -50.22, 0.00, -13.00, fx_beaconb ,
