N487MC
Service difficulty reports · 181
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 = 'N487MC' 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 = 'N487MC' 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 UIEA2026072400648Floorbeam · damagedCORROSION DAMAGE ON FLOORBEAM UPPER TEE BS 2240 NEAR LBL 36. REPAIRED DAMAGE FLOORBEAM IAW EI T2026A53M-1294, REV 0, AND W/O 60480, SRM 53-00-51-1R-3, REV 107. ACCOMPLISHED EI T2026A53M-1294 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2026072400649Pin · damagedFOUND NR 3 PYLON UPPER LINK FWD PIN AND BUSHING DAMAGE AND PYLON SIDE LUG BUSHING DAMAGE. IAW AMM 54-51-01-004-001 REV 116 AND AMM 54-51-02-004-001-005 REV 116, REMOVED NR 3 PYLON NACELLE STRUT AND ATTACH PIN BOLT. REPAIRED NR 3 PYLON UPPER SPAR LUG BUSHINGSDR UIEA2026072400650Link · damagedFOUND NR 1 PYLON LINK AFT SIDE BOLT, WASHER, NUT DAMAGE, AND WING LUG BUSHING DAMAGE. IAW AMM 54-51-01-004-001 REV 116 AND AMM 54-51-02-004-001-005 REV 116, REMOVED NR 1 PYLON NACELLE STRUT AND ATTACH PIN BOLT. REPAIRED WING FRONT SPAR LUG BUSHING. IAW AMM 5SDR UIEA2026072400651Bushing · gougedFOUND NR 2 PYLON UPPER LINK FWD AND AFT SIDE PIN AND BUSHING, BEARING GOUGE AND WING LUG, PYLON LUG BISHING GOUGE. IAW AMM 54-51-01-004-001 REV 116 AND AMM 54- 51-02-004-001-005 REV 116 AND REFER TO JOB CARD, REMOVED NR 2 PYLON NACELLE STRUT AND ATTACH PIN SDR UIEA2026072400652Retainer · corrodedCORROSION RETAINER R/H WING L/G W/W FWD OUTBD SIDE LWR SUPPORT NEAR WBL 128.45. REMOVED DAMAGE PART IAW SRM 51-40-02-06-0 REV 107. INSTALLED NEW PART IAW SRM 51-40-02-06-0 REV 107 AND BOEING DWG #65B11631 SHEET 2 REV 7. JOB COMPLETED, AND CONDITION CHECK SDR UIEA2026072400653Battery · no testFOUND EMERGENCY LIGHT BATTERY M5170 FUNCTION FAIL(<P>1. IAW AMM 33-51-04-902-001-001 REV 107 REPLACED EMERGENCY LIGHT BATTERY PACK (M5170) AT UPPER DECK, CONDITION CHECK NORMAL, AND PERFORMED POWER SUPPLY TEST, RESULT WAS SATISFACTORY</P>)SDR UIEA2026051300313Oxygen Bottle · low pressureCREW OXY LOW EICAS MESSAGE. OXY LEVEL SHOWS 250. TRANSFER TO DMI 252465 PER MEL 35-11-02 CAT C DUE DATE 23MAY26. DETERMINED IT WAS AN INDICATION PROBLEM.SDR UIEA2026050500294Transducer · faultedCREW OXYGEN LOW IN FLIGHT. FOUND 2 EA CONNECTORS AT BOTTLE LOOSE, SECURED AND VERIFIED INDICATION WAS OPERATIONAL. DEFERRED O2 INDICATION SYSTEM AS PRECAUTION. TRANSFER TO DMI 252018 PER MEL 35-11-02. R/R CREW LOWER TRANSDUCER AND C/O LEAK CHK, RESULT SATIS SDR UIEA2026042900264Engine · power lossUPON SETTING TAKEOFF THRUST, ENGINE 4 DID NOT SPOOL UP. FOLLOWED FIM 71-00 TO BLOCK 43, ENGINE OPERATED NORMAL, NO DAMAGE FOUND TO ABRADABLE SHROUD OR FAN BLADES. C/W MPA AND ACCELERATION ENGINE RUN IAW AMM 71-00-00. OPS CHECK GOOD.SDR UIEA2025122401357Skin · puncturedLEFT WING INBD AFT FLAP LE ENGINE LOWER SURFACE HAS A PUNCTURE. 36" OUTBD OF ACCORDION SEAL. REPAIRED SMALL PUNCTURE 1/2" ON LH INBD AFT FLAP LEADING EDGE 501/2" FROM ACCORDION SEAL AND 361/4" FROM TRAILING EDGE PER B747-400 SRM 51-70-07-0G-0 PG. 15 A. NO FURSDR UIEA2025122401358Skin · damagedLT WING OTBD FORE FLAP OTBD END LOWER SURFACE L/E DAMAGED ABOUT 6 INCHES INBD OF OTBD EDGE(<P>PERMANENT COMPOSITE REPAIR MADE TO LH WING OTBD FORE FLAP LOWER SURFACE 9" FORM OTBD EDGE AND 19" FORM LOWER EDGE. SIZE AFTER REPAIR L 5" W 4" PER B747-400 SRM 51-70-SDR UIEA2025113001331Valve · faultedBLEED 4 CAUTION MSG ON CLIMB OUT. MSG 36229. REPLACED NR 4 PRVC AND CHECKED NORMAL PER AMM 36-11-20/401 & IPC 36-11-19-01</P>)SDR UIEA2025081401123Audio Panel · odorSTRONG SMELL OF BURNING WIRE IN COCKPIT DURING PREFLIGHT. PERFORMED SMOKE OR FUME IN CABIN INSPECTION IAW FIM 21-00TASK 810. FOUND F/O CONTROL AUDIO PANEL BAD WITH ODOR. R/R PANEL IAW AMM 23-51-11. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. HAPPENED ON GRSDR UIEA2025062600815Web · crackedLEFT WING T/E CAVITY SUPPORT RIB WEB AT NR 5 SPOILER INBD LWR WBL 432.65 FOUND CRACKED. LT WING T/E CAVITY SUPPORT RIB WEB (P/N: 6565B10865-26) AT NR 5 SPOILER INBD LWR WBL 432.65 REPLACED IAW RI-57-70-17735 REV. A. NO FURTHER DEFECTS NOTED.SDR UIEA2025011900089Packing · leakingENG 2 OIL QTY DROPPED FROM 20Q TO 9Q, FOLLOWED BY A DROP FROM 8 TO 7 TO 6 ABOUT EVERY HALF HOUR. FOUND ENG #2 LOW PRESSURE WARNING SWITCH PACKING INSTALLED IN WRONG POSITION. INSTALLED NEW PACKING PER AMM 79-33-01 PERFORMED ENG #2 POWER PER AMM 71-00-00. AMM SDR UIEA2024112501112Window · leakingCLIMBING THROUGH 18,000' AND 6 PSI DIFFERENTIAL. A LOUD SQUEAL BEGAN FROM ONE OF THE CAPTAIN SIDE WINDOWS. DIFFICULT TO ASCERTAIN WHICH WINDOW BUT IT SEEMINGLY IS LOUDEST FROM THE L2 WINDOW. FUEL JETTISON ACCOMPLISHED AND RETURN TO ZAZ.(<P>WINDOW NO 2 LH REPLASDR UIEA2024072700756Smoke Detector · faultedDURING CRUISE FL310 EICAS CAUTION EQUIPMENT COOLING PERFORMED NNC, MESSAGE BLANKED, SMELLED ELECTRICAL BURNING, DIVERTED TO CTS.(<P>CMC REPORTED MX MSG 21422. R/R E/E COOLING SMOKE DET AND GND TEST PASSED. SET THE A/C TO AIR MODE AND KEPT THIS MODE FOR 3 HOURSSDR UIEA2024062000561Skin · dentedFUSELAGE SECTION 41 DENT/NICK DAMAGE FOUND ON FUSELAGE SKIN (PN 65B12874) AT STA 284 APPROXIMATELY NEAR STR 10R(<P>DAMAGE AREA REPAIRED AS PER RI-53-10-16982 REV.A (CAT A). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024062000562Frame · cracked#2 ENG L/H CORE COWL #2 FRAME (COUNT FROM FWD) FOUND CHAFING MARK.(<P>#2 FRAME CHAFING MARK AREA REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG 201. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024062000563Frame · cracked#2 ENG L/H CORE COWL MOST AFT FRAME FOUND CRACK.(<P>FRAME CRACK AREA REPAIRED AS PER SRM 54-45-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024070600586Skin · delaminatedLHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024070600587Skin · delaminatedLHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024070600588Skin · delaminatedLHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024070600589Skin · delaminatedLHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024070600590Skin · delaminatedLHW I/B FORE FLAP FOUND DELAMINATION. PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.SDR UIEA2024070600591Skin · delaminatedLHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024070600592Skin · delaminatedLHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024070600593Skin · delaminatedLHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024070600594Skin · delaminatedLHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024070600595Skin · delaminatedLHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024070600596Skin · delaminatedLHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024071000622Skin · delaminatedLHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024071000623Skin · delaminatedLHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024071000624Skin · delaminatedLHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000625Skin · delaminatedLHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000626Skin · delaminatedRHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024071000627Skin · delaminatedRHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000628Skin · delaminatedRHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024071000629Skin · delaminatedRHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000630Skin · delaminatedRHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000631Skin · delaminatedRHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000632Skin · delaminatedRHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000633Skin · delaminatedRHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000634Skin · delaminatedRHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000635Skin · delaminatedRHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000636Skin · delaminatedLHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000637Skin · delaminatedLHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REAPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000638Skin · delaminatedLHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000639Skin · delaminatedLHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071000640Skin · delaminatedLHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)
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