N354MC
Service difficulty reports not matched to an aircraft · 17
They name N354MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N354MC' AND registry_match IS NULL 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 = 'N354MC' AND registry_match IS NULL 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 0913200602Fan · failedENCOUNTER SMOKE IN THE COCKPIT AT CRUISE FLIGHT LEVEL 330. PERFORMED PROCEDURES IAW AOM VOL 1. UNSCHEDULE LANDNG. FINDINGS AFTER LANDING. MAINTENANCE FOUND UNSERVICEABLE COOLING FAN. ITEM WAS PLACED ON DMI PER MEL 21-33-2, CAT -C- AND AIRCRAFT RETURNED TO SSDR 0726200601Hydraulic Line · leakingON LANDING (ELLX) SUFFERED COMPLETE LOSS OF NR 1 HYDRAULIC SYSTEM. PERFORMED AFTER LANDING, LOSS OF HYD AND SHUTDOWN CHECKLIST. AT SAFE TAXI SPEED CLEARED RUNWAY, AND TOWED TO GATE WITH NO FURTHER INCIDENT. FOUND HYD, SWIVAL AND HOSE BODY GR DOWNLOCK ACTR HSDR 0609200601Control Unit · failedAPPROXIMATELY ONE HOUR AFTER DEPARTURE FROM ELIX, NR 3 HYD SYSTEM LOSS. AS PER CHECK SHEET NR 3 EDP TO -SUPPLY OFF-, NR 3 ENGINE RUNNING. RETURN TO ELIX, NO FURTHER INCIDENT. FOUND INOPERATIVE RUDDER POWER CONTROL ASSY. REMOVED INOPERATIVE UNIT, AND REPLACSDR 0820200501Engine · leakingABOUT (1) HR AFTER DEPARTURE FROM (ORD), AT CRUISE FLT, NR 3 ENGINE LOSS OIL QTY AND OIL PRESSURE (TO ZERO) ACCOMPANIED BY ENGINE OIL PRESSURE NR 3 LIGHT. ACCOMPLISHED AOM PROCEDURE AND ENGINE FAILURE/SHUTDOWN CKLIST. AIRCRAFT RETURNED TO (ORD) WITHOUT FURTHSDR P5CA0401060Indicator · failedSTANDBY ATTITUDE INDICATOR ROLLS 10 DEG RIGHT AND LEFT IN LEVEL FLIGHT. REMOVED AND REPLACED STBY AI, PERFORMED CHECK PER 34-24-00. SYSTEM OPS CHECKS NORMAL.SDR P5CA0301003Csd · leakingNR 4 ENGINE CSD LIGHT ON. CSD DISCONNECTED. TRANSFERRED TO DMI 31912 PER MEL 24-1 1A CSD AND GENERAL REMOVED PER MM 24-11-00.SDR P5CA0300996Slide · deployedWHILE ATTEMPTING TO INSERT SAFETY PIN IN SLIDE, FOR SLIDE TIME CHANGE, SLIDE INADVERTENTLY DEPLOYED INSIDE A/C. SLIDE MANUALLY DEFLATED/REPLACED WITH SERVICEABLE UNIT.SDR P5CA0300984Strip · wornNR 1 ENG FAN STATOR ASSY ABRADALE STRIP DAMAGE AT 4 TO 5 O'CLOCK POS. ENG CHANGE REPLACEMENT REQ'D PER ATLAS AIR FORM 01-AA-45. ACCOMPLISH PYLON INSP PER CF6-50E2 R/R WORK CARD OK TO INSTALL. REPAIRED ABRADALE STRIP PER MM 72-31-04.SDR P5CA0300954Engine · malfunctionedON START UP NO (N1) INDICATION ON NR 1 ENG RESET C/13 NO HELP. DEFERRED NR 1 ENG (N1) IAW MEL 77-1-2.SDR P5CA0300913Drive System · inoperativeNR 1 AND NR 2 RADAR ANT FAULT WX RADAR INOPERATIVE. REMOVED AND REPLACED WX RADAR ANTENNA DRIVE IAW MM 34-43-03. OPS CK AND FUCTION TEST SAT IS IAW MM 34-43-00.SDR P5CA0300890Antenna · faultyRADAR SYS 1 & 2 ANT FAULT ON BOTH SCREENS INTERMITENT IN BOTH TEST & WX MODE, RETURNED TO GATE. WEATHER RADAR FAIL. REPLACED WEATHER RADAR ANTENNA. UNKNOWN WEATHER RADAR FAILED TO PAINT WEATHER.SDR P5CA0300716Seal · leakingAFTER FUELING WAS COMPLETED, A STEADY DRIPPING OF FUEL ONTO #2 ENGINE FROM #2 PYLON WAS NOTICED. FOUND LEAK COMING FROM SEALANT ON FWD SPAR ON #2 ENGINE PYLON. INSTALLED FUEL LEAK SEAL IAW BMM 28-11-00 & PAC SERVICE FUELING MANUAL 4-05-02, ITEM 7. NO LEAKS NOTSDR P5CA0200709Duct · separatedNR 4 ENG - FIRE INDICATION AFTER TAKEOFF IN CLIMB. PRECAUTIONARY ENGINE SHUTDOWN & FUEL DUMP PERFORMED. FIRE BOTTLE NOT REQUIRED. FOUND 8TH STAGE BLEED CROSSOVER DUCT SEPARATED FROM DUCTING SYSTEM. REPLACED WITH CROSSOVER DUCT & PRECOOLER DOWNSTREAM DUCT. SDR P5CA0200699Compressor · stalledCLIMBING THROUGH 15,000 FT NR 3 ENGINE COMPRESSOR STALLED. EGT WAS 100 DEGREES CELCIUS. LOWER THAN OTHER MOTOR & N2 WAS LOWER WITH NACELLE ANTI-ICE ON. TROUBLESHOT ENGINE PER MM 71-00-43, PERFORMED INSPECTION PER MM 72-00-00 & BORESCOPE OF ENGINE IAW MM 72-SDR P5CA0200695Skin · damagedUPON WALKAROUND IN ANC, FOUND THAT AIRCRAFT TAIL HAD APPARENTLY MADE GROUND CONTACT DURING TAKEOFF FROM ICN, CAUSING DAMAGE TO APU ACCESS DOORS TO BULKHEAD 2764. APPARENT CAUSE: TAKEOFF SPEED LOWER THAN THAT REQUIRED FOR ACTUAL TOGW. PERFORMED INTERIM REPAIRSDR P5CA0200694Adc · failedDUAL CADC FAILURE CAUSING FAILURE IN TRANSPONDER ALTITUDE REPORTING & INACCURATE ALTIMETER & AIRSPEED INDICATIONS. NR 1 & NR 3 INS WOULD NOT UPDATE. REMOVED AND REPLACED NR 1 CADC. CHECKED ALL DRAINS FOR MOISTURE; NONE FOUND. PURGED PITOT/STATIC LINES AND SDR UIEA01105Connector · shortedNR 1 ENGINE START VALVE OPEN LIGHT CAME ON AT TOP OF DESCENT (INTO XXW) ALTITUDE 27,000 FEET. SHUT DOWN ENGINE IAW FHB. NO ENGINE PARAMETERS EXCEEDED. FIRE SWITCH NOT USED. FOUND SHORT AT CONNECTOR DV86B OF START VALVE. REPAIRED CONNECTOR IAW 20-60-00. F
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