/////////////////////////////////////////////////////// //25APR08 //VERSION 1.20 // //PMDG 747-400 /////////////////////////////////////////////////////// [fltsim.0] title=PMDG - 747-400 GE CF6 Engines sim=B747-400 model=GE panel= sound= texture= kb_checklists=PMDG747-400_CHECK atc_id_color=0xffffffff atc_id=N744PM atc_airline=PMDG atc_flight_number=744 ui_manufacturer=Boeing-PMDG ui_type=747-400 GE-CF6 Engines ui_variation=PMDG House Livery description=Boeing 747-400 powered with CF6-80C2B1F engines v 1.0\nPrecision Manuals Development Group\nwww.precisionmanuals.com \n\nProduced under license from Boeing Management Company.\n\nBoeing 747, 747-400, the 747 airplane configuration & Boeing are among the trademarks owned by Boeing. visual_damage=0 atc_heavy=1 [fltsim.1] title=PMDG - 747-400 RB211 Engines sim=B747-400 model=RR panel= sound=RR texture= kb_checklists=PMDG747-400_CHECK atc_id_color=0xffffffff atc_id=N744PM atc_airline=PMDG atc_flight_number=744 ui_manufacturer=Boeing-PMDG ui_type=747-400 RR RB211 Engines ui_variation=PMDG House Livery description=Boeing 747-400 powered with RB-211 engines v 1.0\nPrecision Manuals Development Group\nwww.precisionmanuals.com \n\nProduced under license from Boeing Management Company.\n\nBoeing 747, 747-400, the 747 airplane configuration & Boeing are among the trademarks owned by Boeing. visual_damage=0 atc_heavy=1 [fltsim.2] title=PMDG - 747-400 PW4000 Engines sim=B747-400 model=PW panel= sound=PW texture= kb_checklists=PMDG747-400_CHECK atc_id_color=0xffffffff atc_id=N744PM atc_airline=PMDG atc_flight_number=744 ui_manufacturer=Boeing-PMDG ui_type=747-400 P&W PW4062 Engines ui_variation=PMDG House Livery description=Boeing 747-400 powered with PW4062 engines v 1.0\nPrecision Manuals Development Group\nwww.precisionmanuals.com \n\nProduced under license from Boeing Management Company.\n\nBoeing 747, 747-400, the 747 airplane configuration & Boeing are among the trademarks owned by Boeing. visual_damage=0 atc_heavy=1 [fltsim.3] title=747-400 British Airways sim=B747-400 model=RR panel= sound=RR texture=BA kb_checklists=PMDG747-400_CHECK atc_id_color=0xffffffff atc_id=G-BYGE atc_airline=Speedbird atc_flight_number=744 ui_manufacturer=Boeing-PMDG ui_type=747-400 RR RB211 Engines ui_variation=British Airways description=Boeing 747-400 with RB211 engines v 1.0\nPrecision Manuals Development Group\nwww.precisionmanuals.com \nFor use with BOEING 747 by PMDG \nFor Technical Support please visit www.precisionmanuals.com or email support@precisionmanuals.com \n visual_damage=0 atc_heavy=1 [fltsim.4] title=747-400 British Airways 'Change for Good' sim=B747-400 model=RR panel= sound=RR texture=BA2 kb_checklists=PMDG747-400_CHECK atc_id_color=0xffffffff atc_id=G-BNLZ atc_airline=Speedbird atc_flight_number=744 ui_manufacturer=Boeing-PMDG ui_type=747-400 RR RB211 Engines ui_variation=British Airways "Change for Good" description=Boeing 747-400 with RB211 engines v 1.0\nPrecision Manuals Development Group\nwww.precisionmanuals.com \nFor use with BOEING 747 by PMDG \nFor Technical Support please visit www.precisionmanuals.com or email support@precisionmanuals.com \n visual_damage=0 atc_heavy=1 [fltsim.5] title=747-400 Virgin Atlantic sim=B747-400 model=GE panel= sound= Texture=VS kb_checklists=PMDG747-400_CHECK atc_id_color=0xffffffff atc_id=G-VROC atc_airline=Virgin atc_flight_number=744 ui_manufacturer=Boeing-PMDG ui_type=747-400 GE-CF6 Engines ui_variation=Virgin Atlantic description=Boeing 747-400 with GE-CF6 engines v 1.0\nPrecision Manuals Development Group\nwww.precisionmanuals.com \nFor use with BOEING 747 by PMDG \nFor Technical Support please visit www.precisionmanuals.com or email support@precisionmanuals.com \n visual_damage=0 atc_heavy=1 [fltsim.6] title=Boeing 747-400 British Airways sim=B747-400 model=RR panel= sound= texture=BAirways kb_checklists=PMDG747-400_CHECK atc_id_color=0xffffffff atc_id=Speedbird atc_airline=British Airways atc_flight_number=744 ui_manufacturer=Boeing-PMDG ui_type=747-400 RR RB211 Engines ui_variation=Boeing 747-400 British Airways description=Repaint made by Guillem Roca for the PMDG 747-400 visual_damage=0 atc_heavy=1 [General] atc_type=BOEING atc_model=B744 editable=0 performance="Cruise: 0.86 Mach/565 mph/910 km/h\nEngine: General Electric CF6-80C2B1F, Rolls Royce RB211 or Pratt & Whitney PW4000\nMaximum Range : 7,325 nm [13,570 km]\nMaximum Certified Altitude : 45,100 ft [13,747 m]\nFuel Capacity : 57,285 gal [216,840 L]\nBasic Operating Weight : 394,088 lb [178,755 kg]\nMax Gross Weight : 875,000 lb [396,893 kg]\nLength : 231 ft 10 in [70.6 m]\nWingspan : 211 ft 5 in [64.4 m]\nHeight : 63 ft 8 in [19.4 m]\nSeating : Typical 3-class configuration - 416\nTypical 2-class configuration - 524" [pitot_static] vertical_speed_time_constant = 99 [WEIGHT_AND_BALANCE] empty_weight = 394088.0 // 3-Class max_gross_weight = 875000.0 // 800, 833, 850, 870, 875 x 10^3 lbs [+2000 for max ramp] max_landing_weight = 630000.0 // 574, 630 x 10^3 lbs max_zerofuel_weight = 542500.0 // 535, 542.5 x 10^3 lbs CG_forward_limit=0.130 // 11% 572000-775000 lbs CG_aft_limit=0.331 // WARNING : DO NOT EDIT ! reference_datum_position = 112.714, 0.0, 5.502 // (feet) Boeing Section2.0 reference position (RefPos) empty_weight_CG_position = -97.85, 0, 0 // (feet) from RefPos 19.75% MAC max_number_of_stations = 50 station_load.0 = 72600.0, -98.41, 0 ,0 ;Moments of Inertia empty_weight_pitch_MOI = 17018677.379279 empty_weight_roll_MOI = 15962454.863936 empty_weight_yaw_MOI = 16890566.121607 empty_weight_coupled_MOI = 2048.0 [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -107.5, -53.3, -6.9 //(feet) from RefPos Engine.1 = -76.0, -30.0, -10.4 //(feet) from RefPos Engine.2 = -76.0, 30.0, -10.4 //(feet) from RefPos Engine.3 = -107.5, 53.3, -6.9 //(feet) from RefPos fuel_flow_scalar = 1.07 // sfc [...] min_throttle_limit = -0.20 // reverse [TurbineEngineData] // // Model : CF6-80C2B1F ~58K // fuel_flow_gain = 0.0036 //Gain on fuel flow inlet_area = 61.283 //Square Feet, engine nacelle inlet area [d=106 in] rated_N2_rpm = 13635.0 //max RPM HPC static_thrust = 58000.0 //Lbs, nominal SLS adjusted thru EEC afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [fuel] // Combi/ER + optional stab (Center2) LeftAux = -112.0, -36.5, -3.0, 4482.0, 0.0 // Main 1 LeftMain = -96.0, -28.0, -4.0, 12546.0, 0.0 // Main 2 RightMain = -96.0, 28.0, -4.0, 12546.0, 0.0 // Main 3 RightAux = -112.0, 36.5, -3.0, 4482.0, 0.0 // Main 4 LeftTip = -130.0, -73.0, 0.0, 1322.0, 0.0 // R2 RightTip = -130.0, 73.0, 0.0, 1322.0, 0.0 // R3 Center1 = -83.5, 0.0, -7.0, 17164.0, 0.0 // CWT Center2 = -193.5, 0.0, 6.0, 3300.0, 0.0 // STAB [Optional] Center3 = -83.5, 0.0, -7.0, 50.0, 0.0 // Other fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 4 electric_pump=0 [airplane_geometry] wing_area = 5825.0 //Square feet wing_span = 211.4 //Feet [Jig Position (213.0 at full weight)] wing_root_chord = 47.298 //Feet wing_dihedral = 7.0 //Degrees wing_incidence = 0.0 //Degrees [Inop in FS9] wing_twist = 0.0 //Degrees [Inop in FS9] oswald_efficiency_factor = 0.504 //[...] wing_winglets_flag = 1 //Winglet flag [0:false/1:true] wing_sweep = 37.5 //Degrees at 25% MAC wing_pos_apex_lon = -60.606 //Feet from RefPos wing_pos_apex_vert = 0.0 //Feet from RefPos htail_area = 1470.0 //Square feet htail_span = 75.75 //Feet htail_pos_lon = -210.0 //Feet, from RefPos htail_pos_vert = 7.32 //Feet, from RefPos htail_incidence = 0.0 //Degrees [Inop in FS9] htail_sweep = 37.5 //Degrees, horizontal tail leading edge vtail_area = 1060.0 //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 from RefPos vtail_pos_vert = 26.1 //Feet from RefPos elevator_area = 342.0 //Square feet aileron_area = 225.0 //Square feet rudder_area = 230.0 //Square feet elevator_up_limit = 28.0 //Degrees elevator_down_limit = 20.0 //Degrees aileron_up_limit = 29.5 //Degrees aileron_down_limit = 27.5 //Degrees rudder_limit = 31.5 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit = 70.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 3.2 //Aileron to spoileron gain min_ailerons_for_spoilerons = 4.0 //Degrees min_flaps_for_spoilerons = 0.0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 174.55 //Stall clean KTAS @450,000 lbs full_flaps_stall_speed = 122.0 //Stall flaps KTAS cruise_speed = 485.0 //Cruise KTAS max_mach = 0.920 //Barber pole MACH max_indicated_speed = 372.0 // KIAS / modified provision for CAS->KIAS [flaps.0] type = 1 // Trailing edge span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 60 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 0.00,280 // 1 - no TE flaps-position.2 = 25.0,260 // 5 flaps-position.3 = 27.5,240 // 10 flaps-position.4 = 30.0,230 // 20 flaps-position.5 = 31.5,205 // 25 flaps-position.6 = 33.0,180 // 30 lift_scalar = 1.0 drag_scalar = 0.1 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.1] type = 2 // Inboard/midboard leading edge span-outboard = 0.53333 // 0.0 .. 1.0 extending-time = 12 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 1.0 // 1 damaging-speed = 275 // KIAS blowout-speed = 280 // KIAS lift_scalar = 0.88 drag_scalar = 1.54 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.2] type = 2 // Outboard leading edge span-outboard = 0.2666 // 0.0 .. 1.0 extending-time = 10 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 0.0 // 1 - no effect flaps-position.2 = 5.0 // 5 damaging-speed = 255 // KIAS blowout-speed = 260 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.3] type = 2 // Correct 5-30 / TE LIFT span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 50 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 0.00 flaps-position.2 = 25.0 flaps-position.3 = 21.0 flaps-position.4 = 16.1 flaps-position.5 = 8.7 flaps-position.6 = 4.7 lift_scalar = -1.22 drag_scalar = 0.00 pitch_scalar = -0.12 system_type = 1 //Hydraulic [flaps.4] type = 2 // Correct 10 / TE DRAG span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 60 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 0.0 flaps-position.2 = 0.0 flaps-position.3 = 1.0 flaps-position.4 = 0.1 flaps-position.5 = 3.0 lift_scalar = 0.00 drag_scalar = -1.00 pitch_scalar = 0.00 system_type = 1 //Hydraulic [flaps.5] type = 2 // Correct 30 / TE DRAG span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 60 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 0.0 flaps-position.2 = 0.0 flaps-position.3 = 0.0 flaps-position.4 = 0.0 flaps-position.5 = 0.0 flaps-position.6 = 6.5 lift_scalar = 0.00 drag_scalar = 1.00 pitch_scalar = 0.00 system_type = 1 //Hydraulic [flaps.6] type = 1 // Model span-outboard = 0.7 extending-time = 60 flaps-position.0 = 0.0 flaps-position.1 = 1.0 flaps-position.2 = 5.0 flaps-position.3 = 10.0 flaps-position.4 = 20.0 flaps-position.5 = 25.0 flaps-position.6 = 30.0 lift_scalar = 0.0 drag_scalar = 0.0 pitch_scalar= 0.0 system_type = 1 [autopilot] autopilot_available = 0 autothrottle_available = 0 default_pitch_mode=0 default_bank_mode=0 //Do Not Alter the following line or your 747-400 may cease operating. [AFDSAuth] ---BEGIN SHA1--- c2e80520102f0800e790160704de90760a1b3801 ---END SHA1--- // Do Not Alter the above lines. [contact_points] // point.0 = 1, -24.194, 0.000, -17.546, 1500.0, 0, 1.932, 56.0, 1.45, 0.128, 0.780, 9.0, 12.0, 0, 270, 320 point.1 = 1, -102.496, -16.009, -18.941, 1500.0, 1, 1.932, 0.0, 1.54, 1.171, 0.880, 16.0, 21.0, 2, 270, 320 point.2 = 1, -102.496, 16.009, -18.941, 1500.0, 2, 1.932, 0.0, 1.54, 1.171, 0.880, 15.0, 20.0, 3, 270, 320 point.3 = 1, -115.277, -4.253, -18.598, 1700.0, 1, 1.932, 0.0, 1.50, 1.203, 0.820, 15.0, 18.0, 2, 270, 320 point.4 = 1, -115.277, 4.253, -18.598, 1700.0, 1, 1.932, 0.0, 1.50, 1.203, 0.820, 15.0, 18.0, 2, 270, 320 // point.5 = 2, -153.600, -103.500, 3.000, 1250.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0 point.6 = 2, -153.600, 103.500, 3.000, 1250.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0 point.7 = 2, -2.945, 0.000, -3.312, 1500.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0 point.8 = 2, -156.766, 0.000, -9.961, 1500.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 static_pitch = -0.29 static_cg_height = 12.09 gear_system_type=0 [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 = 31.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.78 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,1,1 //pumps on Eng1,2,3,4 [Views] eyepoint = -19.100, -1.312, 11.122 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) //eyepoint= -18.848, -1.312, 11.122 [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, 5 , 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, 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 Adf.2 = 1 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] light.0 = 3, -225.500, -0.50, 4.745, fx_navwhih, //Position Aft light.1 = 2, -225.500, 0.50, 4.745, fx_strobeh, //Strobe Aft light.2 = 1, -33.596, 0.00, 14.868, fx_pmdg744_beacon, //Beacon Top light.3 = 1, -86.149, 0.00, -11.735, fx_pmdg744_beacon, //Beacon Bottom light.4 = 9, -210.149, 8.00, 35.117, fx_pmdg744_logo, //Logo Right light.5 = 9, -210.149, -8.00, 35.117, fx_pmdg744_logo, //Logo Left light.6 = 8, -77.000, 26.00, -4.000, fx_pmdgwinglight, //Wing Right light.7 = 8, -77.000, -26.00, -4.000, fx_pmdgwinglight, //Wing Left [SMOKESYSTEM] smoke.0 = 0.00, -20.5, 0.00, fx_pmdg744_cockpit, [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [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 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;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 [stall_warning] type=2