N492MC

Service difficulty reports · 205

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 = 'N492MC' 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 UIEA2026100600963Relay · faultedREJECTED TAKE OFF DUE TO #2 ENG REVERSER EICAS MSG(<P>TRANSFER TO DMI 260447 PER MEL 78-31-01A CAT C DUE DATE 16OCT2026</P> / <P>LP 2029709 M5: T/S AND PERFORMED WIRING CHECK. FOUND GRD SAFETY RELAY R8016 DEFECTIVE. REMOVED AND REPLACED RELAY & PERFORMED #2 T/Oct 6, 2026 · N492MC · Boeing 74747UF · Engine Thrust ReverserSDR UIEA2026070900586Compressor · stalledAFTER V1 COMPRESSOR STALL ON #2 ENGINE, RAN QRH CHECKLIST AND RETURNED TO HAN. A/C WAS 265,656KG N1 TARGET 934. NO FUEL DUMPED. MX IN WORK WHILE IN AOGM FOR ATB ENG 2 COMPRESSOR. AOGM ETR: 12JUL26. FERRIED FLIGHT REQ FOR #2 ENG COMPRESSOR STALL. 3 ENGINES FEJul 12, 2026 · N492MC · Boeing 74747UF · Turbine Engine Compressor SectionSDR UIEA2025021800151Tire · failed#8 TIRE FAILURE ON TAKEOFF WITH NO FLIGHT DECK INDICATIONS. NORMAL FLAPS 30 LANDING WAS ACCOMPLISHED. REPLACED MLG TIRE #7 & #8 PER AMM 32-45-01 & IPC 32-45-01-02A. VERIFIED PN PER IPC 32-45-03-02. VERIFIED TIRE PRESSURE 210 PSI. RO INSTALLED. C/W INSPECTION Feb 18, 2025 · N492MC · Boeing 74747UF · TireSDR UIEA2025021000125Frame · damagedFOUND EXISTING REPAIR AT FRAME WEB UPR CHORD STA 560 RBL 13.5.(<P>1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV 102. 2. ACCOMPLISHED EI T2025A53M-234 REV 0. 3. ACCOMPLISHED EI T2025A53M-234 REV 1. 4. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Feb 8, 2025 · N492MC · Boeing 74747UF · Fuselage Main, FrameSDR UIEA2025021000124Bulkhead · misrepairedDEVIATION - PERFORMED STA 2598 BULKHEAD MODIFICATION FOUND DEVIATION AT DOUBLER.(<P>1. PERFORM EI T2025A53M-192 REV 1 AND EI T2025A53M-140 REV 3. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Feb 8, 2025 · N492MC · Boeing 74747UF · Fuselage Main, BulkheadSDR UIEA2025021000123Longeron Splice · damagedDURING PERFORMING EO 4453B761 PART 1-2 (SB747-53A2899), FOUND L/H S-11L LOWER LONGERON SPLICE FITTING AREA ONE HOLE OVERSIZE.(<P>1. ACCOMPLISHED EI T2025A53M-174 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Feb 8, 2025 · N492MC · Boeing 74747UF · Fuselage Main, Longeron/StringerSDR UIEA2025021000122Skin · debondedDISBOND-SKIN, R/H WING INBD AILERON, OUTBD AFT EDGE AREA.(<P>1. PERFORM REPAIR OF R/H WING INBD AILERON, PLEASE REF THE JOB CARD ATTACHING SHEETS FOR THE DETAILED REWORKING INFORMATION. 2. CONDITION CHECK IS SATISFACTORY. B747-400F SRM 57-60-01-0I-1 REV. 102, Feb 8, 2025 · N492MC · Boeing 74747UF · AileronsSDR UIEA2025021000130Feeder Cable · damagedFOUND #1 ENG POWER FEEDER CABLE (W274) DAMAGE NEAR REFUELING STATION.(<P>1. IAW WDM 24-21-11 REV 68 AND SWPM 20-30-13 & 20-10-12 REV 87 REPAIRED #1 ENG POWER FEEDER (W274) NEAR REFUELING STATION. 2. IAW AMM 24-11-00-70J-001 REV. 112 PERFORMED GENERATOR DRIVE SFeb 8, 2025 · N492MC · Boeing 74747UF · Electrical Power System WiringSDR UIEA2025021000129Hose · missingFOUND #3 ENG FIRE EXTINGUISHER HOSE MISSING.(<P>1. IAW AMM 70-50-00-912-034-J00 REV=112, INSTALLED THE NEW FIRE EXTINGUISHER HOSE ASSY WITH NEW PARTS ON #3 ENG. 2. REFER TO NRC:10591633 (508) PERFORM ENGINE FIRE EXTINGUISHING SYSTEM TEST. 3. CLOSED THIS JOB. NFeb 8, 2025 · N492MC · Boeing 74747UF · Fire Bottle, FixedSDR UIEA2025021000128Fitting · damagedFND ENTRY DOOR FITTING DAMAGE AT L1 DOOR AFT LOWER SIDE.(<P>1. IAW AMM 20-51-01-912-008 REV=112 REPLACE L1 DOOR LATCH FITTING. 2. IAW AMM 52-11-01-735-080 REV=112 ADJUST L1 DOOR LATCH FITTING. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Feb 8, 2025 · N492MC · Boeing 74747UF · Passenger/Crew DoorsSDR UIEA2025021000127Web · misrepairedREPAIR - ONE EXISTING UNDOCUMENTED REPAIR ON LH CENTER WEB (P/N= 65B15071-122) OF KEEL BEAM AT STA 1460.(<P>1. REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0 REV=102. 2. ACCOMPLISHED EI T2025A53M-199 REV=1. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Feb 8, 2025 · N492MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2023062800661Fan · unknownE& E COOLING STATUS MESSAGE(<P>REPLACED FWD EQUIPMET COOLING FAN IAW 21-58-01, OPS CHK IAW AMM 21-58-00. NO DEFECTS NOTED AT THIS TIME. AIPC 21-58-01-01 REV 83 11APR23</P> / <P> </P> / <P> </P>)Jun 29, 2023 · N492MC · Boeing 74747UF · Air Distribution FanSDR UIEA2023013140080Skin · delaminatedRH O/B FORE FLAP I/B L/E FOUND DELAMINATION (28" TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2023013140081Skin · chafedRH O/B FORE FLAP I/B L/E  FOUND 2EA CHAFING (42" TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2023013150082Skin · delaminatedRH I/B AILERON AFT EDGE O/B CORNER FOUND DELAMINATED. PERFORMED COMPOSITE LAYUP REPAIR AS PER SRM 51-70-17 PAR.5G.Jan 30, 2023 · N492MC · Boeing 74747UF · AileronsSDR UIEA2023013150083Skin · delaminatedRH O/B FORE FLAP L/E FOUND DELAM (BETWEEN NO.2 AND NO.3 FORE FLAP LEVER)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5C</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2023013150084Skin · chafedRH I/B FORE FLAP LOWER SURFACE (O/B OF O/B ATT FITTING) FOUND BULGE.(<P>PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4.</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Wing StructureSDR UIEA2023013100085Skin · chafedRH O/B AFT FLAP UPPER O/B PNL FOUND CHAFING.(<P>PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2023012600086Firewall · crackedAPU COMPARTMENT FWD FIRE WALL 7 O'CLOCK POS CRACK FOUND AT 2 LOCATION. APU COMPARTMENT FWD FIRE WALL STA 2658 APU FIREWALL WEB AND STIFFENER CRACK AREA REPAIRED IAW RI-53-83-16041 REV.A .Jan 30, 2023 · N492MC · Boeing 74747UF · APU Cowling/ContainmentSDR UIEA2023013100070Skin · crackedTWO CRACKS FOUND AND 1EA CORROSION FOUND ON LT FUSELAGE SKIN BETWEEN BS 1680 AND 1700, STR 43L. FUSELAGE SKIN CORROSION AND CRACK AREA REPAIRED IAW RI-53-00-16037 REV A.Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2023013140071Lamp · inoperativeDOOR 1 EMERGENCY LIGHT EQUIPMENT NO. L1854 FIND INOP. DOOR #1 EMERGENCY LIGHT NO.L1854 REPLACED AND "OP" TEST "NORMAL" IAW AMM 33-51-05 REV 106, 15 NOV 2022Jan 30, 2023 · N492MC · Boeing 74747UF · Emergency LightingSDR UIEA2023012300073Skin · dentedRH I/B FORE O/B UPPER PNL FOUND DENT(<P>PERFORMED METAL HOT BOND REPAIR AS PER SRM 51-70-10 REPAIR 4 </P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Wing, Plate/SkinSDR UIEA2023012400074Frame · crackedFUS - LH STA 1000 BULKHEAD CHORD BETWEEN S-38 AND S-39 FOUND 1EA CRACKED.(<P>FUS - STA 1000 BULKHEAD CHORD BETWEEN STR 38L AND STR 39L CRACK AREA MODIFICATED IAW EO 4453A506 PART 3.</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Main, BulkheadSDR UIEA2023013140075Skin · delaminatedRHW I/B MID FLAP LOWER SURFACE FOUND DELAMINATION (O/B OF #5 FLAP TRACK)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2023013140076Skin · delaminatedRHW I/B MID FLAP L/E MOST I/B AREA FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2023013140078Skin · delaminatedLHW O/B FORE FLAP I/B L/E FOUND 1EA DELAMINATION (39" TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2023012400079Skin · delaminatedLHW I/B MID FLAP I/B L/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Leading Edge DevicesSDR UIEA2023013170051Seat Track · corrodedM/D STA 1658 TO 1680 LBL 11.33 SEAT TRACK BOTH SIDE FLANGE CORRODED.(<P>M/D STA 1650.45 TO STA 1690.45 LBL 11.33 SEAT TRACK REPAIRED IAW SRM 53-00-52-2R-12 REPAIR 12.</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2023013170053Web · crackedLH STA 1480 WEB FOUND CRACK AFTER REMOVE LONGERON EXTENSION FTG.(<P>FX STA 1480 LH WEB CRACK AREA REPAIRED AND MODIFICATION IAW EO 4453A818 PART 7 AND SB 747-53A2860 R3 FIG 14 AND FIG 15.</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2023013180054Skin · corroded1EA CORROSION FOUND ON STA 1720 STR 43L.(<P>FX - STA 1720 STR 43L FUS SKIN CORROSION AREA REPAIRED IAW RI-53-00-16035 REV.A</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2023012000068Structure · crackedLH - BS 2231 STR 17L, 1EA HOLE FOUND CRACK ON AFT INNER CHORD.(<P>MED - L5 DOOR CUTOUT STA 2231 STR 17L AFT INNER CHORD CRACK AREA REPAIRED IAW RI-53-00-16036 REV A.</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2023013120069Structure · cracked1EA CRACK FOUND ON AFT UPR CORNER OF MAIN ENTER DOOR 5L CUTOUT, CRACK FOUND ON SECOND LAYER RUNNING TO FORWARD.(<P>FX - MAIN ENTER DOOR 5L CUTOUT AFT UPPER CORNER BEAR STRAP AND SKIN CRACK AREA REPAIRED AND MODIFICATION IAW EO 4453A804 PART 3.</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA2023013170052Fitting · crackedLH STA 1480 TO 1540 STR 32-33 LONGERON EXTENSION FITTING FOUND 1EA CRACKED.(<P>FX STA 1480 TO STA 1540 STR 32L-33L LONGERON EXTENSION FTG CRACK AREA TRIMMED OFF REPAIRED IAW SB 747-53A2860R3 FIG 13 AND FIG 14 AND EO 4453A818 PART 7.</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Main, StructureSDR UIEA2023013140040Support · crackedCOCKPIT - LH RUDDER PEDAL CAVITIES I/B VERTICAL METAL PANEL CORNER FOUND CRACK.(<P>COCKPIT LH FWD PANEL SUPPORT WEB CRACK AREAS REPAIRED IAW RI-53-00-16024 REV.A</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2023011400041Support · crackedCOCKPIT - RH RUDDER PEDAL CAVITIES I/B VERTICAL METAL PANEL CORNER FOUND CRACK.(<P>COCKPIT RH FWD PANEL SUPPORT WEB CRACK AREAS REPAIRED IAW RI-53-00-16024 REV.A</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2023013160044Seat Track · damagedM/D STA 880 AND STA 920 RBL 11.33 SEAT TRACK SLOT HOLE ELONGATED(<P>M/D STA 830.45 TO STA 950.45 RBL 11.33 SEAT TRACK REPAIRED IAW SRM 53-00-52-2R-12 REPAIR 12</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2023011600045Intercostal · crackedRH STA 1000 FRONT SPAR INTERCOSTAL LUG FTG FOUND CRACK(<P>M/D STA 1000 RBL 11.33" FRONT SPAR INTERCOSTAL LUG FTG P/N: 69B14592-10 REPLACED AND INSTALLED IAW EO 4453C024 PART 7 AND SB 747-53A2904 FIG 18</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2023011600050Intercostal · crackedLEFT BS 1000 FRONT SPAR INTERCOSTAL LUG FTG FOUND CRACK M/D BS 1000 LBL 11.33" FRONT SPAR INTERCOSTAL LUG FTG P/N: 69B14592-9 REPLACED AND INSTALLED IAW EO 4453C024 PART 3 AND SB 747-53A2904 FIG 5.</P>)Jan 30, 2023 · N492MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2022080500815Pressure System · low pressureAFTER T/O "HYD QTY 1" EICAS MSG, SHORTLY AFTER "HYD SYS 1"(<P>FOUND #1 ADP PRESSURE HOSE LEAKING. R/R #1 ADP PRESSURE HOSE PER AMM 20-11-18. PERFORMED LEAK CHECK, NO LEAKS NOTED PER AMM 29-11-17. SERVICED HYD SYS #1 PER AMM 12-12-01.</P>)Aug 4, 2022 · N492MC · Boeing 74747UF · Hydraulic Power Accumulator, MainSDR UIEA2022032600242Aoa · failedCREW REPORTED AUTOPILOT FAILURES, SINGLE IRU MODE, MULTIPLE ADC ISSUES, WHICH WERE CONFIRMED IN AHM.(<P ><SPAN>REPLACED LEFT AIR DATA COMPUTER. DURING OPS CHECK, LEFT ANGLE OF ATTACK SENSOR FAILED. REMOVED AND REPLACED LEFT ANGLE OF ATTACK SENSOR IAW AMM 34-12Mar 26, 2022 · N492MC · Boeing 74747UF · Outside Air Temperature Indicator/SensorSDR UIEA2021091302012Mechanism · faultedON CLIMB AILERON CONTROLS LAG AND BIND. REPLACED SPEED BRAKE SEQUENCE MECHANISM IAW AMM 27-62-06.Sep 13, 2021 · N492MC · Boeing 74747UF · Drag Control SystemSDR UIEA2021061001314Terminal · brokenELEC BUS ISLN 1 ADVISORY MSG / CREW REPORTS ELECTRICAL SMELL IN FLT. CREW DID NOT DECLARE AN EMERGENCY(<P ><SPAN>T/S TO BROKEN TERMINAL ON #1 / IDG. DISCONNECTED AND DEFERRED #1 IDG. COMPLETED CHAP 5 CONDITIONAL INSPECTIONS / FOR ODOR IN FLIGHT DECK - NO SMELLJun 10, 2021 · N492MC · Boeing 74747UF · Electrical Power System WiringSDR UIEA2021040200788Stud · crackedFOUND NO. 7 MAIN CARRIAGE SPINDLE STUD CRACK. IAW AMM 27-51-28-004-001 REV 100 AND AMM 27-51-28-404-006 REV 100 REPLACED NO. 7 FLAP MAIN CARRIAGE. CONDITION CHECK SATIS.Apr 1, 2021 · N492MC · Boeing 74747UF · Trailing Edge Flap Control SystemSDR UIEA2021040200789Panel · no testELT REMOTE PANEL FUNCTION TEST FAIL. IAW AMM 23-24-01 TEMPORARY REVISION REMOVED ELT REMOTE PANEL. IAW PWG NO EG-224-3110-00 REV -, PERFORMED THE WIRE OUTPUT CHECK, THE RESULT WAS SATISFACTORY. IAW AMM 23-24-01 TEMPORARY REVISION INSTALLED ELT REMOTE PANEL. TRApr 1, 2021 · N492MC · Boeing 74747UF · Emergency Locator BeaconSDR UIEA2021040200790Bolt · missingFAULT HISTORY REPEAT FAULT LAV SMOKE DETECTOR INOP. IAW SSM26-13-07 REV 52, WDM 26-13-11 REV 52, PERFORMED WIRING CHK, THE RESULT WAS SATISFACTORY, BUT FOUND CONNECTOR SLIDE LATCH BOLT MISSING. REPLACED SLIDE LATCH IAW SWPM 20-72-08 REV 76. IAW AMM 26-13-00-7Apr 1, 2021 · N492MC · Boeing 74747UF · Cabin Equipment/FurnishingsSDR UIEA2021040200791Battery · no testFOUND EMER LIGHT NOT STAYING MORE THAN 5 MIN. IAW AMM 33-51-04-902-001-001 REV 100 REPLACED BATTERIES AT M5168, M5169, AND M5170. IAW AMM 33-51-04-902-001--001 REV 100 PERORMED TEST OF NEW BATTERIES AND THE RESULT WAS SATISFACTORY.(OFF PARTS: PN 2013-1A, SN635Apr 1, 2021 · N492MC · Boeing 74747UF · Emergency LightingSDR UIEA2021040200792Spar · corrodedCORROSION - DAMAGE ON UPPER CHORD OF LH WING INBD MID FLAP REAR SPAR, AT FS 205.390. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02 REV 91. BLENDED OUT THE DAMAGED AREA IAW SRM 51-10-02 REV 91. PFM NDT INSP REFER TO JOB CARD ATTACHING SHEET NO 0263122. ACCOMPLApr 1, 2021 · N492MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA2021040200793Floor Support · corrodedFOUND MAIN DECK CGO FLOOR STRUCTURE CORROSION. LOC: STA 1410, LBL 11 (UPPER CHORD). REMOVE DAMAGED PART IAW SRM 51-40-02 REV 91. INSTALL NEW PART IAW SRM 51-40-02 REV 91 AND DWG NO 65B24600 SH19, REV C, SH20 REV B, 14448204 SH1 REV -, SH5 REV - 144U8703 SH5 REApr 1, 2021 · N492MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA2021040200794Plate · corrodedCORROSION - PLATE, LH WING INBD REAR SPAR TANK NO. 2 AFT M223 PUMP MOTOR.. REMOVE DAMAGE PART IAW SRM 51-40-02 REV 91. INSTALL NEW PART IAW SRM 51-40-02 REV 91 AND BOWING DWG NO 11241001 SHEET 3 REV F. CONDITION CHK NORMAL AND JOB COMPLETED.Apr 1, 2021 · N492MC · Boeing 74747UF · Wing Main, Frame StructureSDR UIEA2021040200795Hinge · corrodedCORROSION - HINGE, AIR CONDITION BAT PANEL 141EL FWD MID AFT HINGE, UPPER HALF X1 (AFT), LOWER HALF X1 (AFT), LOWER ANGLE X2 (MID, AFT) UPPER ANGLE X3 (FWD, MID, AFT). IAW SMM 20-51-01-902-008 REV 100, RMV LOWER ANGLE 2EA (MID AFT) AT PNL 191EL. IAW EI NO T202Apr 1, 2021 · N492MC · Boeing 74747UF · Fuselage, Door Hinge
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