Hi,No, am not. Only for add new textures, but that's all. My OS is Windows 7 Ultimate 32b. The program was installed with adm. rights, and without AntiVirus. Use TOPCAT for load the pmdg.This is my aircraft.cfg://///////////////////////////////////////////////////////25APR08//VERSION 1.20// //PMDG 747-400///////////////////////////////////////////////////////[fltsim.0]title=PMDG - 747-400 GE CF6 Enginessim=B747-400model=GEpanel=sound=texture=kb_checklists=PMDG747-400_CHECKatc_id_color=0xffffffffatc_id=N744PMatc_airline=PMDGatc_flight_number=744ui_manufacturer=Boeing-PMDGui_type=747-400 GE-CF6 Enginesui_variation=PMDG House Liverydescription=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=0atc_heavy=1[fltsim.1]title=PMDG - 747-400 RB211 Enginessim=B747-400model=RRpanel=sound=RRtexture=kb_checklists=PMDG747-400_CHECKatc_id_color=0xffffffffatc_id=N744PMatc_airline=PMDGatc_flight_number=744ui_manufacturer=Boeing-PMDGui_type=747-400 RR RB211 Enginesui_variation=PMDG House Liverydescription=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=0atc_heavy=1[fltsim.2]title=PMDG - 747-400 PW4000 Enginessim=B747-400model=PWpanel=sound=PWtexture=kb_checklists=PMDG747-400_CHECKatc_id_color=0xffffffffatc_id=N744PMatc_airline=PMDGatc_flight_number=744ui_manufacturer=Boeing-PMDGui_type=747-400 P&W PW4062 Enginesui_variation=PMDG House Liverydescription=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=0atc_heavy=1[fltsim.3]title=Boeing 747-400 Lufthansa D-ABVCsim=B747-400model=GEpanel=sound=texture=LufthansaDABVCkb_checklists=PMDG747-400_CHECKkb_reference=topcatatc_id_color=0xffffffffatc_id=D-ABVCatc_airline=Lufthansaatc_flight_number=778ui_manufacturer=Boeing-PMDGui_type=747-400 GE-CF6 Enginesui_variation=Boeing 747-400 Lufthansa D-ABVCdescription=Boeing 747-400\nPMDG LUFTHANSA\n10 DEC 2010 09:23 UTC\n\nConfigured by TOPCAT\n\nPassengers\t\t322+4\nCargo\t\t\t6440 kg\n\nDry Operating Weight\t178755 kg\nZero Fuel Weight\t\t210969 kg\nTake-Off Fuel\t\t129551 kg\nTake-Off Weight\t\t340520 kg\nTake-Off MAC\t\t21.8%\nStabilizer Trim\t\t6.0\nvisual_damage=0atc_heavy=1[fltsim.4]title=Boeing 747-400 KLM Asiasim=B747-400model=GEpanel=sound=texture=KLMAsiakb_checklists=PMDG747-400_CHECKkb_reference=topcatatc_id_color=0xffffffffatc_id=PH-BFHatc_airline=KLMatc_flight_number=744ui_manufacturer=Boeing-PMDGui_type=747-400 GE-CF6 Enginesui_variation=Boeing 747-400 KLM Asiadescription=Boeing 747-400 with CF6-80C2B1F 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
[email protected] \nPMDG Developer and Customer Forum available at our website. \nSounds Developed by PMDG \nFSUIPC Commercially Licensed from Pete Downson \KLM Asia Repaint by Guillem Roca nAll Artwork encoded using Digimark Technology \nThank you for supporting PMDG!\nvisual_damage=0atc_heavy=1[fltsim.5]title=Boeing 747-400 British Airways G-BNLGsim=B747-400model=RRpanel=sound=RR1texture=BAirwayskb_checklists=PMDG747-400_CHECKkb_reference=topcatatc_id_color=0xffffffffatc_id=G-BNLGatc_airline=British Airwaysatc_flight_number=744ui_manufacturer=Boeing-PMDGui_type=747-400 RR RB211 Enginesui_variation=Boeing 747-400 British Airways G-BNLGdescription=Repaint made by Guillem Roca for the PMDG 747-400visual_damage=0atc_heavy=1[fltsim.6]title=Boeing 747-400 Virgin Atlantic G-VROCsim=B747-400model=GEpanel=sound=texture=VANCkb_checklists=PMDG747-400_CHECKkb_reference=topcatatc_id_color=0xffffffffatc_id=D-ABVCatc_airline=Virgin Atlanticatc_flight_number=454ui_manufacturer=Boeing-PMDGui_type=747-400 GE-CF6 Enginesui_variation=Boeing 747-400 Virgin Atlantic G-VROCdescription=Boeing 747-400\n\n29 NOV 2010 11:06 UTC\n\nConfigured by TOPCAT\n\nPassengers\t\t333+33\nCargo\t\t\t6660 kg\n\nDry Operating Weight\t178755 kg\nZero Fuel Weight\t\t212162 kg\nTake-Off Fuel\t\t116279 kg\nTake-Off Weight\t\t328441 kg\nTake-Off MAC\t\t33.0%\nStabilizer Trim\t\t3.2\nvisual_damage=0atc_heavy=1[fltsim.7]title=PMDG - 747-400 EC-KSMsim=B747-400model=PWpanel=sound=PW1texture=pullmanturairkb_checklists=PMDG747-400_CHECKkb_reference=topcatatc_id_color=0xffffffffatc_id=EC-KSMatc_airline=Pullmantur Airatc_flight_number=702ui_manufacturer=Boeing-PMDGui_type=747-400 P&W PW4062 Enginesui_variation=Boeing 747-400 EC-KSMdescription=Boeing 747-400\nPMDG Pullmantur Air\n16 NOV 2010 16:25 UTC\n\nConfigured by TOPCAT\n\nPassengers\t\t311+9\nCargo\t\t\t6220 kg\n\nDry Operating Weight\t178755 kg\nZero Fuel Weight\t\t207586 kg\nTake-Off Fuel\t\t18200 kg\nTake-Off Weight\t\t225786 kg\nTake-Off MAC\t\t21.3%\nStabilizer Trim\t\t3.7\nvisual_damage=0atc_heavy=1[fltsim.8]title=747-400 Corsair F-GTUIsim=B747-400model=PWpanel=sound=PW1texture=CRL_GTUIkb_checklists=PMDG747-400_CHECKatc_id_color=0xffffffffatc_id=F-GTUIatc_airline=Corsairatc_flight_number=860ui_manufacturer=Boeing-PMDGui_type=747-400 P&W PW4062 Enginesui_variation=Corsair F-GTUIdescription=Boeing 747-400\nPMDG CorsairFly\n05 DEC 2010 15:24 UTC\n\nConfigured by TOPCAT\n\nPassengers\t\t416+13\nCargo\t\t\t16420 kg\n\nDry Operating Weight\t180300 kg\nZero Fuel Weight\t\t230782 kg\nTake-Off Fuel\t\t102200 kg\nTake-Off Weight\t\t332982 kg\nTake-Off MAC\t\t24.5%\nStabilizer Trim\t\t5.6\nvisual_damage=0atc_heavy=1kb_reference=topcat[fltsim.9]title=747-400 Corsair F-HSEXsim=B747-400model=PWpanel=sound=PW1Texture=CRL_HSEXkb_checklists=PMDG747-400_CHECKatc_id_color=0xffffffffatc_id=F-HSEXatc_airline=Corsairatc_parking_types=GATEatc_parking_codes=CRLatc_flight_number=1255ui_manufacturer=Boeing-PMDGui_type=747-400 P&W PW4062 Enginesui_variation=Corsair F-HSEXdescription=Boeing 747-400\nPMDG CorsairFly\n02 DEC 2010 04:25 UTC\n\nConfigured by TOPCAT\n\nPassengers\t\t531+16\nCargo\t\t\t10620 kg\n\nDry Operating Weight\t180300 kg\nZero Fuel Weight\t\t233466 kg\nTake-Off Fuel\t\t16600 kg\nTake-Off Weight\t\t250066 kg\nTake-Off MAC\t\t21.0%\nStabilizer Trim\t\t4.8\nvisual_damage=0atc_heavy=1kb_reference=topcat[fltsim.10]title=747-400 Corsair F-HSEAsim=B747-400model=PWpanel=sound=PW1Texture=F-HSEAkb_checklists=PMDG747-400_CHECKatc_id_color=0xffffffffatc_id=F-HSEAatc_airline=Corsairatc_parking_types=GATEatc_parking_codes=CRLatc_flight_number=744ui_manufacturer=Boeing-PMDGui_type=747-400 P&W PW4062 Enginesui_variation=Corsair F-HSEAdescription=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
[email protected] \nvisual_damage=0atc_heavy=1[fltsim.11]title=747-400 Corsair F-HSUNsim=B747-400model=PWpanel=sound=PW1Texture=F-HSUNkb_checklists=PMDG747-400_CHECKatc_id_color=0xffffffffatc_id=F-HSUNatc_airline=Corsairatc_parking_types=GATEatc_parking_codes=CRLatc_flight_number=938ui_manufacturer=Boeing-PMDGui_type=747-400 P&W PW4062 Enginesui_variation=Corsair F-HSUNdescription=Boeing 747-400\nPMDG CorsairFly\n03 DEC 2010 18:14 UTC\n\nConfigured by TOPCAT\n\nPassengers\t\t582+3\nCargo\t\t\t14070 kg\n\nDry Operating Weight\t180200 kg\nZero Fuel Weight\t\t242521 kg\nTake-Off Fuel\t\t104700 kg\nTake-Off Weight\t\t347221 kg\nTake-Off MAC\t\t24.3%\nStabilizer Trim\t\t5.7\nvisual_damage=0atc_heavy=1kb_reference=topcat[fltsim.12]title=747-400 Corsair F-HKISsim=B747-400model=PWpanel=sound=PW1Texture=F-HKISkb_checklists=PMDG747-400_CHECKatc_id_color=0xffffffffatc_id=F-HKISatc_airline=Corsairatc_parking_types=GATEatc_parking_codes=CRLatc_flight_number=862ui_manufacturer=Boeing-PMDGui_type=747-400 P&W PW4062 Enginesui_variation=Corsair F-HKISdescription=Boeing 747-400\nPMDG CorsairFly\n16 DEC 2010 13:41 UTC\n\nConfigured by TOPCAT\n\nPassengers\t\t531+7\nCargo\t\t\t14425 kg\n\nDry Operating Weight\t180300 kg\nZero Fuel Weight\t\t238300 kg\nTake-Off Fuel\t\t102600 kg\nTake-Off Weight\t\t340900 kg\nTake-Off MAC\t\t24.4%\nStabilizer Trim\t\t5.7\nvisual_damage=0atc_heavy=1kb_reference=topcat[fltsim.13]title=747-400 Corsair F-HLOVsim=B747-400model=PWpanel=sound=PW1Texture=F-HLOVkb_checklists=PMDG747-400_CHECKatc_id_color=0xffffffffatc_id=F-HLOVatc_airline=Corsairatc_parking_types=GATEatc_parking_codes=CRLatc_flight_number=744ui_manufacturer=Boeing-PMDGui_type=747-400 P&W PW4062 Enginesui_variation=Corsair F-HLOVdescription=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
[email protected] \nvisual_damage=0atc_heavy=1[General]atc_type=BOEINGatc_model=B744editable=0performance="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 =394087.3max_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 lbsmax_zerofuel_weight = 542500.0 // 535, 542.5 x 10^3 lbsCG_forward_limit=0.130 // 11% 572000-775000 lbsCG_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 =-97.850000, 0, 0 // (feet) from RefPos 19.75% MACmax_number_of_stations =50;Moments of Inertiaempty_weight_pitch_MOI = 17018677.379279empty_weight_roll_MOI = 15962454.863936empty_weight_yaw_MOI = 16890566.121607empty_weight_coupled_MOI = 2048.0station_load.0=0, -95.55, 0.00, 0.00, First Deckstation_load.1=9769, -97.85, 0.00, 8.00, Upper Deckstation_load.2=8322, -97.85, 0.00, 0.00, Busn Deckstation_load.3=77975, -98.00, 0.00, 0.00, Econ Deckstation_load.4=31802, -97.11, 0.00, -8.00, Cargo Deck[GeneralEngineData]engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=TurbopropEngine.0 = -107.5, -53.3, -6.9 //(feet) from RefPosEngine.1 = -76.0, -30.0, -10.4 //(feet) from RefPosEngine.2 = -76.0, 30.0, -10.4 //(feet) from RefPosEngine.3 = -107.5, 53.3, -6.9 //(feet) from RefPosfuel_flow_scalar = 1.07 // sfc [...]min_throttle_limit = -0.20 // reverse[TurbineEngineData]//// Model : CF6-80C2B1F ~58K//fuel_flow_gain = 0.0036 //Gain on fuel flowinlet_area = 61.283 //Square Feet, engine nacelle inlet area [d=106 in]rated_N2_rpm = 13635.0 //max RPM HPCstatic_thrust = 58000.0 //Lbs, nominal SLS adjusted thru EECafterburner_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 1LeftMain = -96.0, -28.0, -4.0, 12546.0, 0.0 // Main 2RightMain = -96.0, 28.0, -4.0, 12546.0, 0.0 // Main 3RightAux = -112.0, 36.5, -3.0, 4482.0, 0.0 // Main 4LeftTip = -130.0, -73.0, 0.0, 1322.0, 0.0 // R2RightTip = -130.0, 73.0, 0.0, 1322.0, 0.0 // R3Center1 = -83.5, 0.0, -7.0, 17164.0, 0.0 // CWTCenter2 = -193.5, 0.0, 6.0, 3300.0, 0.0 // STAB [Optional]Center3 = -83.5, 0.0, -7.0, 50.0, 0.0 // Otherfuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetAnumber_of_tank_selectors = 4 electric_pump=0[airplane_geometry]wing_area = 5825.0 //Square feetwing_span = 211.4 //Feet [Jig Position (213.0 at full weight)]wing_root_chord = 47.298 //Feetwing_dihedral = 7.0 //Degreeswing_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% MACwing_pos_apex_lon = -60.606 //Feet from RefPoswing_pos_apex_vert = 0.0 //Feet from RefPoshtail_area = 1470.0 //Square feethtail_span = 75.75 //Feethtail_pos_lon = -210.0 //Feet, from RefPoshtail_pos_vert = 7.32 //Feet, from RefPoshtail_incidence = 0.0 //Degrees [inop in FS9]htail_sweep = 37.5 //Degrees, horizontal tail leading edgevtail_area = 1060.0 //Square feetvtail_span = 37.1 //Feet, tip to bodyvtail_sweep = 45.0 //Degrees, vertical tail leading edgevtail_pos_lon = -198.5 //Feet from RefPosvtail_pos_vert = 26.1 //Feet from RefPoselevator_area = 342.0 //Square feetaileron_area = 225.0 //Square feetrudder_area = 230.0 //Square feetelevator_up_limit = 28.0 //Degreeselevator_down_limit = 20.0 //Degreesaileron_up_limit = 29.5 //Degreesaileron_down_limit = 27.5 //Degreesrudder_limit = 31.5 //Degreeselevator_trim_limit = 20.0 //Degreesspoiler_limit = 70.0 //Degreesspoilerons_available = 0 //Spoilerons Available?aileron_to_spoileron_gain = 3.2 //Aileron to spoileron gainmin_ailerons_for_spoilerons = 4.0 //Degreesmin_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 lbsfull_flaps_stall_speed = 122.0 //Stall flaps KTAScruise_speed = 485.0 //Cruise KTASmax_mach = 0.920 //Barber pole MACHmax_indicated_speed = 372.0 // KIAS / modified provision for CAS->KIAS[flaps.0]type = 1 // Trailing edgespan-outboard = 0.7 // 0.0 .. 1.0extending-time = 60 // secondsflaps-position.0 = 0 // pseudo-degreesflaps-position.1 = 0.00,280 // 1 - no TEflaps-position.2 = 25.0,260 // 5flaps-position.3 = 27.5,240 // 10flaps-position.4 = 30.0,230 // 20flaps-position.5 = 31.5,205 // 25flaps-position.6 = 33.0,180 // 30lift_scalar = 1.0drag_scalar = 0.1pitch_scalar= 1.0system_type = 1 //Hydraulic[flaps.1]type = 2 // Inboard/midboard leading edgespan-outboard = 0.53333 // 0.0 .. 1.0extending-time = 12 // secondsflaps-position.0 = 0 // pseudo-degreesflaps-position.1 = 1.0 // 1damaging-speed = 275 // KIASblowout-speed = 280 // KIASlift_scalar = 0.88drag_scalar = 1.54pitch_scalar= 1.0system_type = 1 //Hydraulic[flaps.2]type = 2 // Outboard leading edgespan-outboard = 0.2666 // 0.0 .. 1.0extending-time = 10 // secondsflaps-position.0 = 0 // pseudo-degreesflaps-position.1 = 0.0 // 1 - no effectflaps-position.2 = 5.0 // 5damaging-speed = 255 // KIASblowout-speed = 260 // KIASlift_scalar = 1.0drag_scalar = 1.0pitch_scalar= 1.0system_type = 1 //Hydraulic[flaps.3]type = 2 // Correct 5-30 / TE LIFTspan-outboard = 0.7 // 0.0 .. 1.0extending-time = 50 // secondsflaps-position.0 = 0 // pseudo-degreesflaps-position.1 = 0.00flaps-position.2 = 25.0flaps-position.3 = 21.0flaps-position.4 = 16.1flaps-position.5 = 8.7flaps-position.6 = 4.7lift_scalar = -1.22drag_scalar = 0.00pitch_scalar = -0.12system_type = 1 //Hydraulic[flaps.4]type = 2 // Correct 10 / TE DRAGspan-outboard = 0.7 // 0.0 .. 1.0extending-time = 60 // secondsflaps-position.0 = 0 // pseudo-degreesflaps-position.1 = 0.0flaps-position.2 = 0.0flaps-position.3 = 1.0flaps-position.4 = 0.1flaps-position.5 = 3.0lift_scalar = 0.00drag_scalar = -1.00pitch_scalar = 0.00system_type = 1 //Hydraulic[flaps.5]type = 2 // Correct 30 / TE DRAGspan-outboard = 0.7 // 0.0 .. 1.0extending-time = 60 // secondsflaps-position.0 = 0 // pseudo-degreesflaps-position.1 = 0.0flaps-position.2 = 0.0flaps-position.3 = 0.0flaps-position.4 = 0.0flaps-position.5 = 0.0flaps-position.6 = 6.5lift_scalar = 0.00drag_scalar = 1.00pitch_scalar = 0.00system_type = 1 //Hydraulic[flaps.6]type = 1 // Modelspan-outboard = 0.7extending-time = 60 flaps-position.0 = 0.0flaps-position.1 = 1.0flaps-position.2 = 5.0flaps-position.3 = 10.0flaps-position.4 = 20.0flaps-position.5 = 25.0flaps-position.6 = 30.0lift_scalar = 0.0drag_scalar = 0.0pitch_scalar= 0.0system_type = 1[autopilot]autopilot_available = 0autothrottle_available = 0default_pitch_mode=0default_bank_mode=0//Do Not Alter the following line or your 747-400 may cease operating.[AFDSAuth]---BEGIN SHA1---73C308142039120B762F9AB01E2BD026ACDE7B1D---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, 320point.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, 320point.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, 320point.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, 320point.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, 0point.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, 0point.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, 0point.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, 0static_pitch = -0.29static_cg_height = 12.09gear_system_type=0[gear_warning_system]gear_warning_available = 1 //Normalpct_throttle_limit = 0.1 //Percent throttle that activates warningflap_limit_idle = 5.0 //Flap angle that activates warning at idleflap_limit_power = 31.5 //Flap angle that activates warning at above idle[brakes]parking_brake = 1 //Parking brake availabletoe_brakes_scale = 0.78 //Brake scalar[hydraulic_system]normal_pressure = 3000.0 //PSIelectric_pumps = 0 //no electric pumpsengine_map = 1,1,1,1 //pumps on Eng1,2,3,4[Views]eyepoint = -19.100, -1.312, 11.102 ; 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 , 17.0avionics_bus = 0, 5 , 17.0avionics = 1, 5 , 17.0gear_warning = 0, 2 , 17.0fuel_pump = 0, 5 , 17.0light_nav = 0, 5 , 17.0light_beacon = 0, 5 , 17.0light_landing = 0, 5 , 17.0light_taxi = 0, 5 , 17.0light_strobe = 0, 5 , 17.0light_panel = 0, 5 , 17.0[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.1 = 1Com.1 = 1, 1Com.2 = 1, 1Nav.1 = 1, 1, 1Nav.2 = 1, 1, 0Adf.1 = 1Adf.2 = 1Transponder.1 = 1Marker.1 = 1[LIGHTS]light.0 = 3, -225.90, 0.30, 4.72, fx_navwhih, //Position Aftlight.1 = 3, -225.90,-0.30, 4.72, fx_navwhih, //Position Aftlight.2 = 1, -33.596, 0.00, 14.868, fx_shockwave_beacon_rotating_red, //Beacon Toplight.3 = 1, -86.149, 0.00,-11.735, fx_shockwave_beacon_rotating_red, //Beacon Bottomlight.4 = 9, -210.149, 8.00, 35.117, fx_pmdg744_logo, //Logo Rightlight.5 = 9, -210.149, -8.00, 35.117, fx_pmdg744_logo, //Logo Leftlight.6 = 6,-21.7, 0,-11.5, fx_shockwave_landing_light_747_nose //Landing noselight.7 = 5,-77.0,19,-3.7, fx_shockwave_landing_light_747_rw //Landing right winglight.8 = 5,-77.0,-19.0,-3.7, fx_shockwave_landing_light_747_lw //Landing left winglight.9 = 2, -225.52, 0.00, 4.20, fx_shockwave_strobe_l, //Strobe Aft [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 = 4direction_indicator.0=3,0[attitude_indicators]//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyroattitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators]//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyroturn_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, 250aileron = 150, 250rudder = 150, 250[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[exits]number_of_exits = 2exit_rate.0 = 0.4 ;Percent per secondexit_rate.1 = 0.4 ;Percent per second[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[stall_warning]type=2Thanks in advance.