N485MC
Service difficulty reports · 141
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 = 'N485MC' 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 = 'N485MC' 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 UIEA2026063000557Tension Tie · crackedRH STA 820 UPPER DECK TENSION TIE FWD 2EA FASTENER HOLES CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026063000558Doubler · crackedRH STA 820 U/D TENSION TIE ATT. FRAME DOUBLER 2EA FASTENER HOLES CRACKED. FRAME DOUBLER REPLACED AS PER SRM 51-10-02 AND NEW FRAME DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FRAME DOUBLER INSTALLED AS PER SRM 51-40-02.& NO FURTHER DEFECTS NOTED.SDR UIEA2026070100566Channel · crackedLH STA 920 UPPER DECK TENSION TIE FWD CHANNEL 1EA FASTENER HOLE CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026070300569Stiffener · crackedLHW L/E CAVITY APPROX ILES 620 SUPPORT RIB ATT #3 STIFFENER FOUND CRACK ( COUNT FROM FWD )(<P>STIFFENER FABRICATED AS PER BOEING DWG 65B15696 PL REV LTR B AND RI 57-41-18367 REV A AND NEW STIFFENER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW STIFFENER INSTALSDR UIEA2026070300570Stiffener · crackedRHW L/E CAVITY APPROX ILES 620 SUPPORT RIB I/B #3 STIFFENER FOUND CRACK ( COUNT FROM FWD ) NEAR #3 PYLON I/B(<P>STIFFENER FABRICATED AS PER BOEING DWG 65B15696 PL REV LTR B AND RI-57-41-18368 REV A AND NEW STIFFENER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NESDR UIEA2026070700575Spar · crackedLWH UPPER WING T/E MOST I/B FIXED PNL SUPPORT P/N 65B11532-47 CRACK(<P>SUPPORT P/N 65B11532-47 REPLACED AS PER RI-57-20-18405 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026070700576Frame · crackedLH STA 880 UPPER DECK FRAME FOUND 1EA FASTENER HOLE CRACK(<P>FRAME CRACK AREA REPAIRED AS PER RI-53-20-18366 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026070700577Channel · crackedLH STA 880 UPPER DECK TENSION TIE FWD CHANNEL 1EA FASTENER HOLE CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 AND RI-53-20-18366 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026070700578Frame · crackedRH STA 880 UPPER DECK FRAME FOUND 2EA FASTENER HOLES CRACK(<P>FRAME REPAIRED AS PER RI-53-20-18365 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026070700579Channel · crackedRH STA 880 UPPER DECK TENSION TIE FWD CHANNEL 2EA FASTENER HOLES CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 AND RI-53-20-18365 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026070700580Channel · crackedLH STA 840 UPPER DECK TENSION TIE FWD CHANNEL FOUND CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 AND RI-53-20-18364 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026070700581Frame · crackedLEFT BS 840 UPPER DECK FRAME ONE EACH FASTENER HOLE CRACKED. FRAME CRACK AREA REPAIRED AS PER RI-53-20-18364 REV A. NO FURTHER DEFECTS NOTEDSDR UIEA2026070800582Skin · damaged6EA EXISTING FASTENER HOLES SIZE LARGER THAN BOEING SB 747-53A2651 R1, FASTENERS INSTALL HOLES SIZE AT FX RH TOP SKIN APPROX STA 2537(<P>6EA FASTENERS INSTALLED AS PER RI-53-80-18417 REV A. NO FURTHER DEFECTS NOTED </P>)SDR UIEA2026071200589Bushing · damagedREWORK RH BLG I/B TRUNNION BUSHINGS(<P>PERMANENT REPAIR TO USE BAC5701 TYP 11 CL2 IN LIEU OF SOPM 20-42-05 TYP 11 CL2 AS PER RI-32-13-18363 REV B. NO FURTHER DEFECTS NOTED </P>)SDR UIEA2026071200591Bushing · damagedREWORK LH BLG I/B TRUNNION BUSHING(<P>PERMANENT REPAIR TO USE BAC5701 TYP 11 CL2 IN LIEU OF SOPM 20-42-05 TYP 11 CL2 AS PER RI-32-18362 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026071200592Bearing Race · damagedREWORK LH BLG O/B TRUNNION BEARING RACE(<P>PERMANENT REPAIR TO USE BAC5701 TYP 11 CL2 IN LIEU OF SOPM 20-42-05 TYP 11 CL2 AS PER RI-32-13-18385 REV B. NO FURTHER DEFECTS NOTED </P>)SDR UIEA2026071300600Floor Support · crackedLOWER CHORD ( 2EA ) FASTENER HOLES CRACK AT M/D STA 1220 LH O/B BELOW FLOOR INTERCOSTAL WEB FWD LOWER.(<P>LOWER CHORD REPAIRED AS PER RI-53-40-18378 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026071300601Floor Support · crackedLOWER CHORD 3EA FASTENER HOLE CRACK AT M/D STA 1200 RH BELOW FLOOR INTERCOSTAL WEB FWD LOWER AREA(<P>LOWER CHORD REPAIRED AS PER RI-53-40-18382 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026071400605Support · damagedFX AIR COND BAY #2 PACK HEAT EXCHANGER FWD I/B SUPPORT TRIANGLE PLATE MOUNT BOLT HOLE ELONGATED(<P>LOCAL FABRICATED PLATE P/N 69B40167-1 AS PER RI-21-52-18421 REV A AND BOEING DRAWING 69B40167. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026071600609Fitting · crackedM/D BS 1920 LBL 107" TO LBL 116" SUPPORT WATER DAM FTG CRACK(<P>SUPPORT WATER DAM FTG REPAIRED AS PER RI-53-60-18432 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026071900611Floor Support · crackedLOWER CHORD 2EA FASTENER HOLES CRACK AT M/D STA 1220 RH O/B BELOW FLOOR INTERCOSTAL WEB FWD LOWER AREA(<P>LOWER CHORD REPAIRED AS PER RI-53-40-18381 REV A.NO FURTHER DEFECTS NOTED </P>)SDR UIEA2026072000612Web · crackedM/D STA 1200 LBL 105 - LBL 109 BELOW FLOOR INTERCOSTAL WEB FWD LWR CHORD ( 2EA ) FASTENER HOLES CRACK(<P>LOWER CHORD REPAIRED AS PER RI-53-40-18377 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000613Frame · crackedSTA 900 LH UPPER DECK FRAME 1EA FASTENER HOLE CRACK(<P>FRAME REPAIRED AS PER RI-53-20-18410 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000614Channel · crackedSTA 900 LH UPPER DECK TENSION TIE AFT CHANNEL EA FASTENER HOLE CRACK(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 AND RI-53-20-18410 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000615Skin · debondedRHW I/B AFT FLAP UPPER O/B PANEL PREVIOUS REPAIR DOUBLER FOUND DISBOND(<P>PERFORMED METAL HOT BOND REPAIR AT DISBOND AREA AS PER HX RI-57-53-18374 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000616Skin · debondedLHW #1 SPOILER FOUND DISBOND(<P>PERFORMED METAL HOT BOND REPAIR AT DISBOND AREA AS PER HX RI NO.RI-57-73-18361 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000617Skin · delaminatedLHW I/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000618Skin · delaminatedLEFT WING INBD FORE FLAP UPPER T/E FOUND DELAMINATED PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000619Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000620Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000621Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000622Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000623Fairing · delaminatedLHW I/B MID FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000624Skin · delaminatedLHW O/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000625Skin · delaminatedRHW O/B FORE FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000626Skin · delaminatedRHW O/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000627Skin · delaminatedRHW I/B MID FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000628Skin · delaminatedRHW I/B MID FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000629Skin · delaminatedRHW I/B MID FLAP UPPER T/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000630Fairing · delaminatedRHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072000631Fairing · delaminatedRHW I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOT BOND REPAIR AT DELAMINATION AREA AS PER SRM 51-70-07 PAR 5A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072100635Skin · damagedVERTICAL STABILIZER THE TOP AFT TIP FOUND ELECTRICAL ARCING DAMAGE APPROX 4CM IN DIAMETER(<P>FAIRING DAMAGE AREA REPAIRED AS PER RI-55-31-18434 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026072600656Web · corrodedLOWER CHORD FASTENER HOLE CRACK AT M/D BS 1180 LH O/B BELOW FLOOR INTERCOSTAL WEB LOWER AREA(<P>LOWER CHORD REPLACED AS PER SRM 51-10-02 AND NEW CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.SDR UIEA2026070800583Fitting · damaged3EA FASTENER HOLES OVERSIZED TO 0.437" LARGER THAN SB 747-53A2651 R1 FASTENER HOLES SIZE 0.391" - 0.395"(<P>FTG 3EA FASTENER INSTALLED AS PER RI-53-80-18417 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026061400478Beam · crackedRHW L/E NEAR NO.3 PYLON O/B D-BEAM UPPER CHORD FOUND CRACK(<P>UPPER CHORD REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201.</P>)SDR UIEA2026040900180Valve · faultedDIVERSION FOR BLEED #4 STATUS MESSAGE, #3 BLEED DEFFERED. REPLACED BROKEN TERMINAL (EICAS BLEED 4) ON #4 HIGH PRESS BLEED VALVE #1 STUD IAW SWP 20-30-00. R/R #3 ENG PRV IAW AMM 36-11-19. OPS AND LEAK CHECK PASSED, PERFORMED HP ENG RUN PER 71-00-00. OPS CHSDR UIEA2026040200119Aileron Sys · deflectionUPON LANDING, ACFT REQUIRED NEARLY FULL RT AILERON DEFLECTION DURING ROLLOUT TO KEEP WINGS LEVEL. WINDS WERE SUCH THAT LT AILERON DEFLECTION SHOULD HAVE BEEN REQUIRED. SUSPECT A POSSIBLE SPOILER OR LE FLAP ISSUE. PERFORMED C/B RESET & SPEED BRAKE GROUND OPS SDR UIEA2025120301333Thermal Switch · faultedCLIMBING OUT OF 8000FT BLD DUCT LEAK L CAUTION MSG/ BLEED FAMV ENG 4. REF FIM 36-11 TASK 985 & WDM 26-18-13. T/S & WIRE CHK, FOUND THERMAL SW S907 AT FAULT. R & R THERMAL SWITCH IAW AMM 26-18-02 & IPC 26-18-02-01, ITEM 420. FIRE TEST RESULT PASSED, APU RUNNISDR UIEA2025100701258Bulkhead Web · crackedCRACK - PFM MOD PER SB 747-53A2837 AT STA 2598 FND BULKHEAD RH SIDE WEB AND AFTER CHORD FASTENER HOLE CRACK(<P>1. ACCOMPLISHED EI NO.T2025A53M-2100 REV. 4. 2. JOB COMPLETED AND CONDITION CHK NORMAL</P>)SDR UIEA2025061100738Panel · crackedRH NWW SIDE PANEL WL150, BETWEEN STA 300 AND STA 320 FOUND 1 EA FASTENER HOLE CRACKED.(<P>NWW STA 320 WL150 SIDE PANEL 1 EA FASTENER HOLE CRACK AREA REPAIRED AND 1 EA STIFFENER REPLACED IAW RI-53-10-17693 REV. A. NO FURTHER DEFECTS NOTED.</P>)
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