N496MC

Service difficulty reports · 195

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N496MC' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UIEA2018060701062Battery · inoperativeFOUND THE EMERGENCY LIGHT FUNCTION ABNORMAL IN THE UPPER DECK AREA. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY M5168 IAW AMM 33-51-04-902-001-001, REV 42 AND PERFORMED AN EMERGENCY LIGHT TEST. RESULT WAS SATISFACTORY.Jun 7, 2018 · N496MC · Boeing 74747UF · Emergency LightingSDR UIEA2017071501224Spoiler · lack of lubeDURING DECENT, 280 AIR SPEED, AT 15,000 FT, WITH RIGHT AUTOPILOT ENGAGED, EXTENDED THE SPEED BRAKES SLOWLY, THE AIRCRAFT TURNED 6 DEGREES TO THE LEFT. PERFORMED OPS CHECK ON SPOILER SYSTEM AND FOUND THE NR 7 SPOILER WAS SLOW TO EXTEND. ACCOMPLISHED LUBRICAJul 14, 2017 · N496MC · Boeing 74747UF · Drag Control SystemSDR UIEA2017070301104Acm · seizedUPON GEAR EXTENSION, EXPERIENCED GRINDING SOUND AND ACRID ODOR IN FLT DECK. FOUND PACK 3 SEIZED. REMOVED AND REPLACED THE ACM IAW AMM REF 21-51-04. OPERATIONAL CHECKED NORMAL IAW AMM 21-00-00-201.Jul 3, 2017 · N496MC · Boeing 74747UF · Cabin Cooling SystemSDR UIEA2016062000449Seat Track · corrodedFOUND SEAT TRACK CORROSION AT STA 2190, RBL 11.35. PERFORMED SEAT TRACK REPAIR IAW EI T2016A53M-1347, REV 3. CONDITION CHECK NORMAL AND JOB COMPLETED.Jun 18, 2016 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2016062000434Angle · corrodedFOUND BRACKET CORROSION AT FUSELAGE LOWER AREA BETWEEN STA 970 AND STA 980, BL3. REPLACED ANGLE IAW DWG 65B06976 ID0002, REV G AND SRM 51-40-02-0G-0, REV 76. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 18, 2016 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2016062000437Bracket · corrodedFOUND BRACKET CORROSION AT FUSELAGE STA 920, BL0. REPLACED BRACKET, PN: 69B01805-3, 2EA IAW SRM 51-40-02-0G-0, REV 76 AND DWG NR 142U0130, SH1 REV A, DWG 65B06704, SH2, REV F. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 18, 2016 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2016062000438Web · corrodedCORROSION ON THE WEB OF RT WING OTBD L/E NEAR OLES 1536. REPAIR DAMAGE AREA IAW EI T2016A57M-1352, REV 1, DWG 65B10652, SHEET 8, REV AND DWG 65B12736, SHEET 4, REV B. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 18, 2016 · N496MC · Boeing 74747UF · Wing Miscellaneous StructureSDR UIEA2016062000439Power Supply · failedFOUND EMERGENCY LIGHTS DID NOT STAY ON FOR 15 MINUTES, X325, X326, M4914, L1382, L5730, L5731, L5732, L5734 IAW AMM 33-51-04-002-009-001 AND 33-51-04-402-012-001, REV 86. REPLACED POWER SUPPLY IAW AMM 33-51-04-402-012-001, REV 86 PERFORMED INSTALLATION TEST OJun 18, 2016 · N496MC · Boeing 74747UF · Emergency LightingSDR UIEA2016062000440Module · faultyFOUND LOWER CARGO FIRE BOTTLE B, CHANNEL 2 CONNECTOR VOLTAGE ABNORMAL DURING TEST IAW AMM 26-21-01-004-001 AND 26-21-01-404-006, REV 86. REPLACED FIRE MODULE AND CONNECTION CHECK NORMAL IAW AMM 26-21-01-734-305, REV 86 PERFORMED FIRE CONTROL MODULE INSTALLATIJun 18, 2016 · N496MC · Boeing 74747UF · Extinguishing SystemSDR UIEA2016062000441Actuator · failedTHE LT WING LANDING GEAR ALTERNATE EXTENSION SYS ELECTRICAL ACTUATOR FUNCTION FAILED IAW AMM 32-36-01-004-001, REV 86, AMM 32-36-01-404-009, REV 86 REPLACED ELECTRICAL ACTUATOR IAW 32-36-06-705-009, REV 86, PFM OPERATION TEST RESULT WAS NORMAL. CONDITION CHEJun 18, 2016 · N496MC · Boeing 74747UF · Landing Gear ActuatorSDR UIEA2016062000444Bracket · damagedFOUND M/D CARGO FLOOR SUBSTITUTE SEAT TRACK BRACKET AT STA 2010, LBL 75.92. ACCOMPLISHED REPAIR DAMAGE AREA IAW SRM 53-00-52. REPAIR REV 76 AND NR 65B38251, SHEET 32, REV AND SRM 51-40-02, REV 76. JOB COMPLETED AND CONDITION CHECK SATISFIED.Jun 18, 2016 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2016062000445Repair · deformedDEFORM ON EXISTING REPAIR AT FORWARD LOWER CORNER OF AFT CARGO DOOR SKIN. REPAIR DAMAGE AFT CARGO DOOR IAW EI T2016A52M-1338, REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.Jun 18, 2016 · N496MC · Boeing 74747UF · Cargo/Baggage DoorsSDR UIEA2016062000446Skin · dentedDENT FOUND ON RT FUSELAGE SKIN AT BS 510 BETWEEN S-40R TO S-41R. REPAIR DAMAGED FUSELAGE SKIN IAW T2016A53M-1325, REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.Jun 18, 2016 · N496MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2016062000447Seat Track · crackedCRACK ON MAIN DECK SEAT TRACK NEAR STA 1800, RBL 98.58. REPAIRED THE CRACKED SEAT TRACK IAW SRM 53-00-52, REPAIR 6, FIG 201, ALTERNATIVE 1, REV 76, EI T2016A53M-1359, REV 1. FASTENER IDENTIFICATION IAW DWG 65B38251, SH66. REV AND DWG 45741062, REV A. CONDIJun 18, 2016 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2016062000448Floorbeam · corrodedFOUND CORROSION AT UPPER CAP OF MAIN DECK FLOORBEAM AT STA 2260, LBL 23. REPAIRED CORROSION AT UPPER CAP OF MAIN DECK FLOORBEAM AT STA 2260, LBL 23 IAW EI T2016A53M-1373, REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.Jun 18, 2016 · N496MC · Boeing 74747UF · Fuselage Main, Floor BeamSDR UIEA2016062000450Floorbeam · corrodedFOUND BEAM M/D, FLOORBEAM UPPER CAP HAD CORROSION AT STA 2160, LBL 2. EI T2016A53M-1372, REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.Jun 18, 2016 · N496MC · Boeing 74747UF · Fuselage Main, Floor BeamSDR UIEA2015032100184Actuator · brokenBLOCK TURN BACK, LT SPOILER INDICATION DOES NOT MOVE FOR FLIGHT CONTROL CHECK. FOUND NR 4 SPOILER ACTUATOR ROD BROKEN. R & R NR 4 SPOILER ACTUATOR. OPERATIONAL & LEAK CHECKED OK IAW MM 27-61-05. LEFT SPOILER INDICATION OPERATES NORMAL.Mar 19, 2015 · N496MC · Boeing 74747UF · Drag Control ActuatorSDR UIEA2014120300627Drive Unit · faultyDURING CRUISE HAD LE FLAP IN-TRANSIT, MAGENTA INDICATION, & 280KT IAS LIMIT OR SPEED DISPLAYED. STATUS MSG FLAP SYS MON. TURNED WAI TO ON, INDICATION WENT AWAY AFTER APPROX 2 MIN, THEN EICAS MSG FLAPS CONTROL & EXPANDED DISPLAY SHOWING LE SENSOR INOPERATIVE.Dec 3, 2014 · N496MC · Boeing 74747UF · Leading Edge Slat ActuatorSDR UIEA2014052700217Lens · defectiveLEFT DOOR 1 CEILING EMERGENCY LIGHT LENS COVER FOUND POOR CONDITION. LT DOOR CEILING EMERGENCY LIGHT LENS COVER REPLACED & OPERATIONS CHECKED FOUND NORMAL IAW AMM 33-51-00.May 27, 2014 · N496MC · Boeing 74747UF · Emergency LightingSDR UIEA2014052700216Light · inoperativeEMERGENCY LIGHT OPERATION TEST FAILED AT MD CARGO L1 DOOR, NEXT TO STAIR WAY. LIGHT BULB REPLACED & OPERATION TEST CARRIED OUT, RESULT NORMAL.May 27, 2014 · N496MC · Boeing 74747UF · Emergency LightingSDR UIEA2013093000510Floor Support · crackedFLOOR SUPPORT CRACKED BS 1000, LBL 75.92. REPAIRED CRACK DAMAGE IAW SRM 53-00-52-2R-13, REPAIR 13.Sep 28, 2013 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2013080100422Skin · crackedDURING WALK AROUND A .75" CRACK WAS FOUND ON THE RT SIDE OF THE ACFT. FUSELAGE SKIN AT STATION 1735, S-42R. EO 4453A892 DOCUMENTS A CATEGORY B PERMANENT REPAIR ACCOMPLISHED IAW THE SRM 53-00-0, REPAIR 15, FIG 201. PART 2 OF THE EO REQUIRES AN INITAL HFEC INSPAug 1, 2013 · N496MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2013040900188Transmitter · failedEICAS FLAPS DRIVE, DURING RETRACTION FROM 20 TO 10. OTBD T/E FLAPS STOPPED. SEEMED LT T/E FLAP REMAINED LOWER THAN RT. EXPANDED VIEW AND STATUS T/E FLAPS INDICATED. APPROX 50-55 MIN INTO FLT. EXPANDED VIEW EXTINGUISHED AND SYS APPEARED NORMAL. DURING HOLDApr 9, 2013 · N496MC · Boeing 74747UF · Trailing Edge Flap Control SystemSDR UIEA2013040400171Computer · failedUNABLE TO ENGAGE ANY OF THE THREE AUTOPILOTS, CMC SHOWS AILERON SERVO C/FCC- C /FCC FAIL. R & R CENTER AND LEFT FCC IAW AMM 22-11-01-004-026. PERFORMED CMC TEST ON CENTER AND LT FCC PASSED REF 22-11-01 ALSO PERFORMED AUTOLAND UNIQUE TEST PASSED.Apr 5, 2013 · N496MC · Boeing 74747UF · Autopilot SystemSDR UIEA2013012000015Skin · damagedRT WING INBD AFT T/E FLAP DAMAGED AT WBL 178.46. PREPARED CLEANED AND REPAIRED AREA OF DAMAGE ON RT WING INBD AFT FLAP T/E AT STATION WBL 178.48 IAW SRM 57-51-01-2R1-1. REPAIR 1, FIG 201 SHEET 4 AND 8. IAW 250 DEGREE F; CORE. SRM 51-70-01.Jan 17, 2013 · N496MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2012073000336Roller · looseLT WING INBD FOREFLAP, OTBD TRACK FWD UPPER FLIGHT LOAD ROLLER LOOSE WITH VERTICAL MOVEMENT WHEN TRACK GOES IN AND OUT. R & R BEARINGS IAW SB 747-57-2107; PERFORMED T/E SYSTEM OPS CHECK OK. FLAPS RETRACTION AND EXTENSION SEVERAL TIMES NORMAL IAW AMM 27-51-0Jul 26, 2012 · N496MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2012073000334Skin · chafedRIGHT WING OTBD FOREFLAP LEADING EDGE WITH CHAFING DAMAGE. PREPARED, CLEANED AND REPAIRED RIGHT OTBD FORE FLAP LEADING EDGE DAMAGE IN LOCATIONS WBL 820.750, 818.00 IAW SRM 57-53-01-2R-1. REPAIR 1, FIGURE 201 SHEETS 5, 6, 9, 10 IAW 250 F CORE SRM 51-70-02.Jul 26, 2012 · N496MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2012051500234Intercostal · crackedMAIN DECK, BS 1220, RBL 98-127 INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB REPAIRED IAW SRM 53-40-51, REPAIR 5 AND RS NR R-53-41-37348, REV A.May 8, 2012 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2012051500235Intercostal · crackedMAIN DECK, BS 1220, LBL 98-127 INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB REPAIRED IAW SRM 53-40-51, REPAIR 5 AND RS NR R-53-41-3748, REV A.May 8, 2012 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2012051500236Channel · crackedMAIN DECK, BS 760 RT TENSION TIE AFT CHANNEL CRACKED. CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1.May 8, 2012 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2012051500237Channel · crackedMAIN DECK, BS 740 RT TENSION TIE FWD CHANNEL FOUND CRACKED. CHANNEL FASTENER HOLES REPAIRED IAW EO 4453A301 PART 2, STEP 5 AND SB T47-53A2502, FIG 11.May 2, 2012 · N496MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2012010400002Nozzle · crackedDURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN APPROX THE 10 TO 12 O'CLOCK POSITION (LT SIDE) ON THE NR3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 11" LONG AND IS 13" FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STJan 4, 2012 · N496MC · Boeing 74747UF · Engine Collector/Tailpipe/NozzleSDR UIEA2011112700696Acoustic Liner · damagedDURING MX WALKAROUND AT MX FOUND DAMAGE TO THE NR 3 ENGINE THRUST REVERSER ACOUSTIC MESH. PERMANENT REPAIR WILL BE PERFORMED ON THE LT T/R PRIOR TO THE NEXT C-CHECK OR HIGHER AFTER PART 1.Nov 24, 2011 · N496MC · Boeing 74747UF · Engine Thrust ReverserSDR UIEA2011070600347Structure · damagedDURING LOADING OPERATIONS, THROUGH THE NOSE CARGO DOOR, LOADER DROPPED CAUSING DAMAGE TO BS 260, LBL10.75 & RBL 10.75, WL 195.8 - CANTED BULKHEAD STIFFENERS (2 EA.), CONSISTING IN EDGE CRACKS MEASURING 1.5 AND 2.5 INCHES LONG (REF FIG 1). DAMAGE TO THE STIFFENJul 6, 2011 · N496MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2011061500314Engine · vibrationON TAKE-OFF ROLL, ENGINE VIBE 4 SHOWED 5.2. FELT A VIBRATION WHEN SELECTING MAX THRUST (VISUALLY INSPECTED INLET/EXHAUST OF ENGINE, MAG CHIP DETECTOR AND & NBSP; ENGINE LPT AREA COMPONENTS AMD VIBRATION PICKUP CONNECTOR & NBSP; ALL IAW FIM 71-00. PERFORMED BJun 15, 2011 · N496MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR UIEA2011050900256Sleeve · crackedDURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 9 O'CLOCK POSITION ON THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 3" LONG AND IS APPROX .5" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF TMay 9, 2011 · N496MC · Boeing 74747UF · Engine Collector/Tailpipe/NozzleSDR UIEA2011041100243Floorboard · damagedDURING CARGO LOADING AT HSV; MX FOUND DAMAGE TO THE MAIN DECK FLOORBOARD AT BS 400, RBL 15 (REF FIG 1). THE DAMAGE IS 1.5 INCHES LONG AND ABOUT 0.125 INCH WIDE. (PART 1: REMOVE LOOSE MATERIAL AND CLEAN UP THE EDGES OF THE DAMAGED FLOOR PANEL SRM 51-20-01. SApr 11, 2011 · N496MC · Boeing 74747UF · Fuselage Floor PanelSDR UIEA2011032800160Eec · malfunctionedAFTER ENGINE START, NR 1 ENGINE WENT TO IMMED T/O THRUST UNCOMMAND. ENGINE SHUTDOWN PERFORMED. FAULT CONFIRMED ON GROUND RUN, 101 PERCENT IN EEC NORMAL MODE. EEC ALT MODE SELECTED AND ENG RUN C/O SATIS. NR 1 ENG ECU REPLACED IAW AMM.Mar 28, 2011 · N496MC · Boeing 74747UF · Fuel Controlling SystemSDR UIEA2011021100060Compressor · smokeDURING OFFLOAD, LOADMASTER NOTED SMOKE COMING OUT OF THE RT SIDE VENT AT STA 850. ISOLATED SMOKE TO POTABLE WATER COMPRESSOR, INSPECTED GENERAL AREA AND NO ABNORMALITIES FOUND. POTABLE WATER COMPRESSOR INOPERATIVE AND POTABLE WATER SYS DEACTIVATED.Feb 11, 2011 · N496MC · Boeing 74747UF · Potable Water SystemSDR UIEA2011012000006Structure · dentedDURING WALK-AROUND INSP, DAMAGE WAS FOUND TO THE LOWER LOBE - BS 1820, WL 188 - LOWER AFT CARGO DOOR CONSISTING OF A DENT. LENGTH: 10 IN. WIDTH: 2.0 IN. DEPTH:0.175 (REF. FIG 1). THE DAMAGE IS OUT OF THE SRM 52-30-01, FIG 101, ALLOWABLE DAMAGE 1, DETAILS XI AJan 20, 2011 · N496MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2010121900196Skin · damagedDURING DEICING ON 19DEC2010, THE R STABILIZER FIXED T/E PANEL WAS STRUCK AT STABILIZER BL 418. THE DAMAGE MEASURES APPROX 1.375 INCH DEEP BY 1.500 INCH WIDE AS SHOWN IN FIG 1. (THE REPAIR IAW PART 1, THE REPETITIVE INSP IAW PART 2 ARE APPROVED BY DER ON THE 8Dec 19, 2010 · N496MC · Boeing 74747UF · Horizontal Stabilizer, Plate/SkinSDR UIEA2010112000182Floorboard · gougedDURING WALK AROUND INSP, MX FOUND GOUGES/DAMAGE TO THE MAIN DECK - FLOORBOARDS (2 EA) BS1520 - BS1580, LBL68.0 (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPETITIVE DVIS AT EVERY 1000Nov 20, 2010 · N496MC · Boeing 74747UF · Fuselage Floor PanelSDR UIEA2010080400130Rib · brokenDURING A-CHECK, THE 69B12755-5 STIFFENER ON THE LT WING T/E RIB WBL515 WAS FOUND TO HAVE A BROKEN OUT SECTION DUE TO INTERFERENCE WITH THE LT WING OTBD MID-FLAP INBD END GUIDE ROLLER. (THE STIFFENER IS MADE FROM 0.063 INCH CLAD 2024-T3 IAW DWG 69B12755. PART Aug 4, 2010 · N496MC · Boeing 74747UF · Wing, Rib/BulkheadSDR UIEA2010060200023Skin · damagedDURING D-CHECK IN TPE, WRINKLES WERE FOUND IN THE 65B02697-122, BS 2360-2484, S-23L TO -46L SKIN (SEE FIG 1 AND 2) WHILE THE TAIL WAS UNSUPPORTED. (FASTENERS WERE REMOVED FROM THE WRINKLED AREA AND SHIMS WERE INSTALLED TO REMOVE THE WRINKLES.)Jun 2, 2010 · N496MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA200900053Unknown · unknownFLYING WITH AUTOPILOT OFF, EXTENDED SPEEDBRAKES TO FLIGHT DETENT, ACFT ROLLED HARD LEFT, INTERMITTENT. WITH AUTOPILOT ENGAGED, EXTENDED SPEEDBRAKES TO FLIGHT DETENT, YOKE MOVES RIGHT APPROX 2 UNITS TO MAINT WING LEVEL, ALSO INTERMITTENT. ACCOMPLISHED VISUAL ISep 2, 2009 · N496MC · Boeing 74747UF · Flight Control SystemSDR UIEA200900050Skin · crackedRT NR3 CORE COWL UPPER AFT AREA FAIRING OUTER SKIN AT NAC STATION 296.25 TO 304.5 HAS A 8.250 INCH CRACK. TIME LIMITED REPAIR WAS ACCOMPLISHED IAW SRM 51-40-02-06-0 AND EO 4471A043. TO INSPECT OR ACCOMPLISH PERMANENT REPAIR NEXT A-CHECK.Aug 14, 2009 · N496MC · Boeing 74747UF · Nacelle/Pylon, Plate/SkinSDR UIEA200900049Seat Track · crackedMAIN DECK SIDE DOOR AREA AT LT, FS 1806.95 TO 1809.95, LBL99 SEAT TRACK CROWN LUG HAS A 3.0 INCH CRACK. PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-00-52-2R-6 REPAIR 6 AND EO 4453A271.Aug 14, 2009 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA201000177Fairing · crackedENG 3 OTBD CORE COWL UPPER AFT AREA FAIRING HAS A CRACK. ON THE AFT UPPER EDGE. DUE TO NO STOCK FOR THE PANEL, DISPOSITION WAS TO ACCOMPLISH A TIME LIMITED REPAIR BY WELDING THE CRACK IAW STANDARD PRACTICES AND REPLACEMENT OF FAIRING WITHIN THE NEXT 2A CHECK.Aug 13, 2009 · N496MC · Boeing 74747UF · Nacelle/Pylon Miscellaneous StructureSDR UIEA201000176Fairing · crackedENG 3 OTBD CORE COWL UPPER AFT AREA FAIRING HAS A CRACK. ON THE AFT UPPER EDGE. DUE TO NO STOCK FOR THE PANEL, DISPOSITION WAS TO ACCOMPLISH A TIME LIMITED REPAIR BY WELDING THE CRACK IAW STANDARD PRACTICES AND REPLACEMENT OF FAIRING WITHIN THE NEXT 2A CHECK.Aug 13, 2009 · N496MC · Boeing 74747UF · Nacelle/Pylon, Main FrameSDR UIEA201000176ASeat Track · crackedMAIN CARGO SIDE DOOR AREA - SEAT TRACK LUG CRACKED AT FS 1806.95 LBL 99 NEXT TO ROLLOUT STOP ASSY. NR 1 POSITION."PERMANENT REPAIR PERFORMED IAW THE SRM 53-00-52-2R-6, REPAIR 6."Aug 13, 2009 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings
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