N499MC
Service difficulty reports · 267
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 = 'N499MC' 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.
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 = 'N499MC' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA2026072900665Shutoff Valve · faultedDURING TAKEOFF ROLL, BLEED 2 ADVISORY MESSAGE CAME ON. TRANSFER TO DMI 256295 PER MEL 36-11-03 CATC DUE DATE 02AUG26. REMOVED AND REPLACE HPSOV IAW B747 AMM 36-11-03 AND OPS CHECK GOOD.SDR UIEA2026063000560Clamp · leakingEQUIPMENT COOLING EICAS MESSAGE IN FLIGHT. REPLACED FLIGHT DECK LOW FLOW DETECTOR & OPS CHECKED GOOD IAW AMM 21-58-02/201. REMOVED AND REPLACED FLIGHT DECK FLOW REGULATOR VALVE & OPS CHECKED GOOD IAW AMM 21-61-09/501. DURING TROUBLESHOOTING, FOUND FOD INSIDESDR UIEA2025052700699Lug · cracked1EA CRACK WAS FOUND ON LH STA 1000 LBL 11.33 FRONT SPAR INTERCOSTAL LUG FITTING.(<P>FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO: 4453C024 REV 4 PART 3 STEP 3. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052700700Lug · cracked1EA CRACK WAS FOUND ON RH STA 1000 RBL 11.33 FRONT SPAR INTERCOSTAL LUG FITTING.(<P>FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO: 4453C024 REV 4 PART 7 STEP 3. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052900703Panel · crackedCOCKPIT CTR CONSOLE LH FWD VERTICAL METAL PNL LWR CORNER NEAR I/B RUDDER PEDAL FOUND CRACK.(<P>PANEL CRACK AREA REPAIRED AS PER RI-25-10-17662 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025052900704Panel · crackedCOCKPIT - CTR CONSOLE RH FWD VERTICAL METAL PANEL LWR CORNER NEAR I/B RUDDER PADAL FOUND CRACK.(<P>PANEL CRACK AREA REPAIRED AS PER RI-25-10-17662 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100708Skin · dentedLHW I/B MID FLAP FAIRING EXTERIOR SURFACE FOUND DENT.(<P>PERFORMED REPAIR AT DENT AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100709Skin · delaminatedLHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100710Skin · delaminatedLHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100711Skin · delaminatedLHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100712Skin · delaminatedRHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060200713Structure · damagedLHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(<P>PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060200714Structure · damagedLHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(<P>PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060200715Structure · damagedRHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(<P>PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060300719Thrust Reverser · delaminated#4 ENG O/B T/REV INNER WALL FOUND DELAMINATED AT FWD 3 O'CLOCK POSITION(<P>DELAMINATE AREA REPAIRED AS PER ATLAS AIR EA-1978A219 REV O FIG 2. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060300720Longeron · cracked1 EA CRACK WAS FOUND ON RH BS 1480 LONGERON EXTENSION FITTING RADIUS AREA.(<P>LONGERON EXTENSION FITTING MOD CARRIED OUT AS PER ATLAS AIR EO NO: 4453A818 REV 20 PART 8. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060300721Frame · cracked1 EA CRACK WAS FOUND AT FASTENER HOLE 6 O'CLOCK POSITION AT RH BS 1480 B/HEAD FRAME WEB I/B UPPER AREA. FRAME WEB REPAIRED AS PER ATLAS AIR EO 4453A818 REV 20 PART 8. NO FURTHER DEFECTS NOTED.SDR UIEA2025060600730Skin · damagedNOSE CARGO DOOR (P/N: 65B13016-10, S/N: 000123) BIRD STRIKE DAMAGE STA 140 AND STA 200, BETWEEN S31R AND S42AR NOSE CARGO DOOR SKIN, FRAMES AND STRINGERS - CAT B PERMANENT REPAIRS.(<P>NOSE CARGO DOOR SKIN DENT #1 AND DENT #2 REPAIRED AS PER RI-52-30-17671 REV SDR UIEA2025060600731Stringer · damagedNOSE CARGO DOOR BIRD STRIKE DAMAGE REPETITION INSPECTION FINDING STA 160 STR 36R, FOUND DENT. STRINGER REPAIRED AS PER RI-52-30-17671 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060600732Door · damagedNOSE CARGO DOOR BIRD STRIKE DAMAGE REPETITION INSPECTION FINDING STA 180 BTN STR 31AR AND STA 34R. DOUBLER FOUND TOOL MARK. FRAME TOOL MARK AREA REPAIRED AS PER RI-52-30-17671 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025060800737Plate · crackedLH BLG I/B W/W DOOR CHAFE PLATE FOUND CRACK.(<P>LH BLG I/B W/W DOOR CHAFE PLATE REPLACE AS PER HX RI-32-14-17675 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025021300134Seat Track · corrodedCORROSION AT SEAT TRACK/FLOOR BEAM AT LBL 11.33 AND STA 1635 AFT CARGO COMPARTMENT.<BR>(<P STYLE="MARGIN-BOTTOM: .0001PT; LINE-HEIGHT: NORMAL;"><SPAN>REPAIRED SEAT TRACK/FLOOR BEAM FROM STA 1590 TO STA. 1650 PER B747 SRM 53-00-52-2R-12 REPAIR 12 AFT CARGO COMSDR UIEA2025021300135Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR BEAM AT RBL 11.33 AMD STA 1710 AFT CARGO COMPARTMENT.(<P STYLE="MARGIN-BOTTOM: .0001PT; LINE-HEIGHT: NORMAL;">REPLACED 2 SECTIONS OF SEAT TRACKS FROM PREVIOUS REPAIR STA. 1610 TO 1766.5 TO FACTORY SPLICE AND SECOND SECTION FROM 17SDR UIEA2025021300136Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR AT RBL 11.33 AND STA. 1675 AFT CARGO COMPARTMENT.(<P STYLE="MARGIN-BOTTOM: .0001PT; LINE-HEIGHT: NORMAL;">REPLACED TWO EACH SECTIONS OF SEAT TRACKS FROM PREVIOUSLY REPAIR STA 1610 TO 1766.5 TO FACTORY SPLICE AND 2ND SECTION FROM SSDR UIEA2025021300137Seat Track · corrodedCORROSION ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 770 TO 785 AT MAIN CARGO DECK.(<P>CLEANED AREA ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 770-785 AT MAIN DECK CARGO DECK. NO CORROSION NOTED. PER BSOPM 20-30-80 PAR. 1.A. REV 153. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025021300138Seat Track · corrodedCORROSION ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 760-770 MAIN DECK CARGO.(<P>CLEANED AREA ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 760-770 AT MAIN CARGO DECK, NO CORROSION NOTED PAR. 1.A REV 153 SOPM 30-20-80. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025021300139Bushing · corrodedCORROSION FOUND AT INNER FACE ON LH BODY LANDING GEAR LOWER BUSHING (INNER BEARING CAP).<BR>(<P>REMOVED AND REPLACED BUSHING PER B747 SRM 53-40-90-2R-1 REPAIR 1 AND B747 AMM 32-13-01-004-001 AND 32-13-01-404-022. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025021300140Bearing Cap · corrodedCORROSION FOUND ON FLANGE OF LH BODY LANDING GEAR BEARING CAP.(<P>REMOVED AND REPLACED LH BODY GEAR BEARING CAP PER B747 SRM 53-40-90-2R-1 REPAIR 1 FIG. 201. <SPAN>NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025021300141Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR BEAM AT RBL 11.33 AT STA 1900.(<P>REPLACED 2 SECTIONS OF SEAT TRACKS FROM PREVIOUS REPAIR STA 1610 TO STA 1766.5 TO FACTORY SPLICE AND 2ND SECTION FROM STA 1766-.5 TO STA. 1910 TO PREVIOUS REPAIR SPLICE RBL 11.33 PER B747-400F SRMSDR UIEA2025021300142Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR BEAM AT RBL 11.33 STA. 1820.(<P>REPLACED 2 EACH SECTIONS OF SEAT TRACKS FROM PREVIOUS REPAIR STA. 1610-1766.5 TO FACTORY SPLICE AND 2ND SECTON FROM STA. 1766.5 TO STA. 1910 TO PREVIOUS REPAIR SPLICE RBL 11.33 PER B747-400F SRM 53-SDR UIEA2025021300143Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR BEAM AT LBL 11.33 AT STA. 1740.(<P>CLEANED AREA ON SEAT TRACK/FLOOR BEAM AT LBL 11.33 AT STA. 1740 AT MAIN CARGO DECK. NO CORROSION NOTED PER SOPM 20-30-03 PAR. 1.A. REV 153 & SRM 53-60-52-001-1 FIG. 001 REV 102. NO FURTHER DEFECTSDR UIEA2025021300144Seat Track · corrodedCORROSION ON SEAT TRACK/FLOOR BEAM AT LBL 11.33 AT STA. 1620,<BR>(<P>REPAIRED SEAT TRACK FROM STA 1590-1650 LBL PER B747-400 SRM 53-00-52-2R-12 REPAIR 12. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025021300145Bearing Cap · corrodedCORROSION FOUND ON FLANGE ON RH SIDE BODY LANDING GEAR BEARING FITTING CAP.(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;">REMOVED AND REPLACED RH SIDE BODY LANDING GEAR BEARING FITTING CAP PER B747 AMM 32-13-01-004-001 AND 32-13-01-404-022. SRM 53-40-90-2R-1SDR UIEA2024110901083Clamp · failedFL320 EICAS MESSAGE EQUIP COOLING. RETURNED TO MIA. REPEAT WRITE UP. AFTER LANDING, EICAS MESSAGE RETURNED(<P>INSTALLED CLAMP ON WATER SEPERATOR IAW AMM 21-51-05-402-025. REACTIVATED PACK 2. OPS CHECK GOOD. DMI 220071 CLOSED.</P>)SDR UIEA2023100700892Brake · unknownSUSPECTED LIGHTNING STRIKE DEPARTING UIO, RETURNED TO UIO, HEAVY WEIGHT LANDING, BRAKE TEMPERATURE CAUSED TIRE FUSE PLUGS TO MELT ON MAIN LANDING GEAR TIRES #1, 2, 3, 4, 5, 6, 7, 8 AND 10.(<P>UPON LANDING, COMPLETED LIGHTING STRIKE INSP IAW AMM 05-51-13, OVERWSDR UIEA2023093000861Unknown · unknownLIGHTNING STRIKE DURING CLIMB, AIR TURN BACK. OVERWEIGHT LANDING AND HIGH ENERGY STOP RESULTED IN 9 MELTED MAIN LANDING GEAR TIRE FUSE PLUGS AND DEFLATION OF TIRES.(<P>AXLES NEED REPLACEMENT. MX CURRENTLY IN WORK PER AMM 05-51-10.</P>)SDR UIEA2023052200463Unknown · unknownCRACKON LH UPPER DECK FLOOR BEAM AFTER CHANNEL OF STA 820(<P>1) REMOVE THE DAMAGE AREA IAW SRM 51-40-02-0G-0 & 53-20-30-2R-2 REV 97. 2) REPAIR THE TENSION TIE AFTER CHANNEL IAW SRM 53-20-30-2R-2 REV 97. 3) CONDITION CHECK NORMAL & JOB COMPLETED</P>)SDR UIEA2023052200464Unknown · unknownDEVIATION - DURING PFM 4453A087 PART 2, FOUND 2 EXISTING FASTENERS NO CONNECT WITH FRAME AT STA 500 RH SIDE(<P>1) PFM EI T2023A53M-875 SEQUENCE A REV 0. 2) ACCOMPLISHED EI T2023A53M-875 REV 1 AND CONDITION CHECK NORMAL</P>)SDR UIEA2023052200465Unknown · unknownCORROSION ON THE FUSELAGE SKIN AT 2-42L BETWEEN STA 1720 & STA 1740(<P>1) REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORMED EI T2023A53M-834 SEQUENCE A REV 0. 3) ACCOMPLISHED EI T2023A53M-834 REV 1 & CONDITION CHECK NORMAL. 4) RECORD THSDR UIEA2023052200466Unknown · unknownDEFORM - FOUND MAIN DECK SEAT TRACK FLOOR COVER DEFORM STA 1730 RBL 75(<P>1) REPAIR DAMAGE AREA IAW SRM 53-00-52-2R-13 REV 97 & BOEING DWG 65B38251 SH 75 REV - & 65B38251 SH 32 REV -. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023052200467Unknown · unknownFOUND M/D FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT STA 1485 RBL 75.92(<P>1) REPAIR DAMAGE AREA IAW SRM 53-00-52-2R-13 REV 97 & BOEING DWG 144U0882 SH 3 REV B & 65B38251 SH 32 REV -. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023052200468Unknown · unknownFOUND M/D FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT STA 990 RBL 75.92(<P>1) REPAIR DAMAGE AREA IAW SRM 53-00-52-2R-13 REV 97 REV 97 AND DWG 65B16004 SH 4 REV A. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023052200469Unknown · unknownFOUND M/D FLOOR STRUCTURE SUBSTITUTE TRACK CRACK AT STA 990 LBL 75.92(<P>1) REPAIR DAMAGE IAW SRM 53-00-52-2R-13 REV 97 AND DWG 65B16004 SH 4 REV A. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023052200470Unknown · unknownBROKEN - SKIN AND CAP, RH WING INBD AILERON T/E WEDGE OUTBD END(<P>1) PERFORM REPAIR OF BROKEN SKIN DAMAGE FOUND ON RH WING INBD AILERON T/E OUTBD SIDE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFO. 2) CONDITION CHECK IS GOOD.</P>)SDR UIEA2023052200471Unknown · unknownDEVIATION - DURING PERFORM 4453A087 PART 2 FOUND EXISTING STRAP HOLES SEM 5 EACH AT STA 480 RH SIDE(<P>1) PERFORM DEVIATION AND PERFORM REPAIR IAW EI T2023A53M-835 REV 1. 2) ACCOMPLISHED EI T2023A53M-835 REV 2. 3) JOB COMPLETED</P>)SDR UIEA2023052200472Unknown · unknownFOUND M/D CARGO FLOOR STRUCTURE CORROSION AT STA 2240 LBL 88 TO 85(<P>1) REPAIR DAMAGE AREA IAW EI T2023A53M-900 REV 0 AND SRM 53-00-51-02R-3 REPAIR 3 REV 97. 2) INSTALL REPAIR PARTS IAW EI T2023A53M-900 REV 0 AND SRM 53-00-51-2R-3 REPAIR 3 REV 97 & BOEING DWGSDR UIEA2023052200473Unknown · unknownFOUND M/D CGO FLOOR STRUCTURE CORROSION AT STA 2240 RBL 59 TO 80(<P>1) REPAIR DAMAGE AREA IAW EI T2023A53M-902 REV 0 AND SRM 53-00-51-2R-3 REPAIR 3 REV 97. 2) INSTALL REPAIR PARTS IAW EI T2023A53M-902 REV 0 AND SRM 53-00-51-2R-3 REPAIR 3 REV 97 AND BOEING DWG SDR UIEA2023052200474Shear Tie · unknownCRACK ON SHEAR TIE AT STA 1000 RBL 57.50 WL195(<P>1) REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 97. 2) REPAIR DAMAGE AREA IAW EI T2023A53M-1018 SEQUENCE A REV 0. 3) INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 97 AND EI T2023A53M-1018 SEQUENCE A REV 0. 4)SDR UIEA2023052200475Shear Tie · unknownCRACK ON SHEAR TIE AT STA 1000 RBL 33.99 WL195(<P>1) REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 97. 2) REPAIRED DAMAGE AREA IAW EI T2023A53M-1018 SEQUENCE A REV 0. 3) INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 97 AND EI T2023A53M-1018 SEQUENCE A REV 0. SDR UIEA2023052200476Unknown · unknownFND M/D BEAM CORROSION AT STA 2100 RBL 100(<P>1) REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REV 97 AND EI T2023A53M-1103 SEQUENCE A REV 0 AND BOEING DWG 65B38105 SH12 REV -, 65B38251 SH 62 REV A, 65B38251 SH 33 REV -, 65B38251 SH 67 REV A, 65B38406 SH 48 REV A.
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