N937MC, cancelled Mar 21, 2013
Service difficulty reports · 28
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 = 'N937MC' AND deregistration_id = 'N937MC-2013-03-21' 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 = 'N937MC' AND deregistration_id = 'N937MC-2013-03-21' 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 CALA9901041Release Mech · out of adjustTHE FORCE REQUIRED TO RELEASE TAILCONE USING BOTH THE INTERIOR TAILCONE RELEASE HANDLE AND THE AFT PASSENGER DOOR EXCEEDED LIMITS. THE TAILCONE RELEASE MECHANISM WAS RIGGED AND TESTED IAW MM 53-53-00.SDR CALA9900990Pan · crackedINSPECTION FOUND A .25 INCH CRACK IN MAIN BAGGAGE BIN DOOR PAN AFT EDGE BETWEEN 2ND AND 3RD STOPS FROM BOTTOM. THE CRACK WAS ROUTED OUT AND A DOUBLER WAS INSTALLED IAW SRM 51-10-1 AND ECRA 5330-02819.SDR CALA9900988Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK IN BELTFRAME AT STA 1418 UNDER LONGERON 2L. THE BELTFRAME WAS REPAIRED IAW DOUGLAS DRAWING NR SR095300003.SDR CALA9900987Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD ENTRY DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9900956Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 229 ABOVE LONGERON 18L. REPAIRED IAW ECRA 5330-02445.SDR CALA9900945Seat Track · corrodedINSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 1155-1160. A NEW SECTION OF SEAT TRACK AND A SPLICE PLATE WERE INSTALLED IAW SRM 53-05, FIGURE 4F.SDR CALA9900882Seat Track · corrodedINSPECTION FOUND LEFT I/B SEAT TRACK CORROSION FROM STA 1105-1202. THE SEAT TRACK FROM STA 1050-1300 WAS REMOVED AND REPLACED IAW SRM 53-05-04.SDR CALA9900875Skin · dentedINSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 69.550 I/B OF F/O'S PITOT TUBE ON AIRCRAFT NOSE. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.SDR CALA9900865Casting · crackedINSPECTION FOUND A 3 CRACK IN FORWARD BAGGAGE BIN DOOR AFT UPPER STOP SUPPORT CASTING. THE STOP SUPPORT CASTING WAS REMOVED AND REPLACED IAW SRM 51-30-1.SDR CALA9800196Apu · low oilWHILE OPERATING THE APU IN FLIGHT WITH THE AC CROSSTIE RELAY PLACARDED INOPERATIVE. THE APU AUTO SHUTDOWN. MAINTENANCE SERVICED THE APU WITH OIL, NO LEAKS WERE DETECTED.SDR CALA9701400Oil Filter · cloggedTHE RIGHT ENGINE OIL STRAINER CLOGGING LIGHT ILLUMINATED AFTER TAKEOFF. THE RIGHT ENGINE OIL TEMPERATURE WAS IN THE YELLOW RANGE. THE RIGHT ENGINE WAS REDUCED TO IDLE AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CSDR CALA9701044Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN DOOR SKIN LOWER CORNER. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 37.SDR CALA9701048Membrane · corrodedINSPECTION FOUND LT CUSP MEMBRANE CORRODED AT STA 560 TO 712. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2.SDR CALA9701047Membrane · corrodedINSPECTION FOUND LEFT CUSP MEMBRANE CORRODED BETWEEN STA 740 TO 745. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2.SDR CALA9701045Jamb · corrodedINSPECTION FOUND CORROSION ON LOWER AND FORWARD DOOR JAMB PAN IN FORWARD BAGGAGE BIN AT STA 370 TO 427. THE CORRODED SECTION WAS CUT OUT AND A NEW PAN SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 44.SDR CALA9701043Pan · crackedINSPECTION FOUND A 2 INCH CRACK IN MAIN CABIN DOOR PAN FRAME LOWER FORWARD CORNER IN CUTOUT FOR LOWER HINGE ARM. THE DOOR PAN WAS REPLACED IAW SRM 51-30-2.SDR CALA9701049Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN FORWARD RT INNER ATTACH ANGLE OF VERTICAL STABILIZER. THE ANGLE WAS REPLACED IAW SRM 51-30-2.SDR CALA9701046Longeron · corrodedINSPECTION FOUND SKIN AND LONGERON 30 CORRODED AT STA 489 TO 496. THE CORRODED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION OF LONGERON WAS SPLICED IN. THE FUSELAGE SKIN WAS BURNISHED OUT. WORK WAS PERFORMED IAW SRM 53-02, FIGURE 1.SDR CALA9701113Clips · out of adjustTHE TAILCONE INTERIOR HANDLE PULLED FROM CLIPS AT 37 POUNDS. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR CALA9701112Cables · out of adjustTHE TAILCONE INTERIOR RELEASE HANDLE REQUIRED 45 POUNDS OF PULL TO RELEASE TAILCONE. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-53-00.SDR CALA9701114Slide · low pressureINSPECTION FOUND THE TAILCONE EMERGENCY SLIDE PRESSURE LOW. THE TAILCONE SLIDE WAS REMOVED AND REPLACED IAW MM 25-62.SDR CALA9601893Strut · low pressureTHE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG SHOCK STRUT PRESSURE LOW. A FULL STRUT SERVICE WAS PERSDR CALA9601425Wire · brokenINSPECTION FOUND EMERGENCY FLOOR TRACK LIGHTING FROM ROWS 25 TO 32 LOOSE AND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE IN AFT SECTION. THE WIRE WAS REPLACED AND OPERATION OF THE TRACK LIGHTING WAS RESTORED.SDR CALA9601250Wire · brokenINSPECTION FOUND THE AFT CABIN FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE IN AFT SECTION OF EMERGENCY TRACK LIGHTING. THE WIRE WAS SPLICED AND OPERATION OF THE PATH LIGHTING CHECKED GOOD.SDR CALA9601065Ignition Syst · inoperativeTHE APU SHUT DOWN WHILE EN ROUTE TO EWR. A RESTART ATTEMPT WAS UNSUCCESSFUL. THE APU COMBUSTOR UNIT AND IGNITION EXCITER WERE REMOVED AND REPLACED. THE APU WAS OPERATED SEVERAL TIMES AND LEAK AND OPERATIONAL CHECKS WERE GOOD. PART TOTAL CYCLES, 5,593.SDR CALA9601047Stator Suppt · brokenTHE NR 2 ENGINE COMPRESSOR BEGAN TO STALL AFTER TAKEOFF AT 13,000 FEET. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. INSPECTION BY MAINTENANCE FOUND DAMAGE TO THE NR 2 ENGINE 13TH STAGE COMPRESSOR. THE NR 2 ENGINE WAS REMOVED AND REPLASDR CAL951141Current Limiter · blownORF - FLT 0443 - THE LEFT ENGINE GENERATOR WAS LOST ACCOMPANIED BY FEEDER FAULT LIGHT AND A CROSS-TIE LOCK OUT WHILE EN ROUTE FROM EWR TO FLL. THE AIRCRAFT WAS DIVERTED TO ORF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AC CROSS-TIE RELAY PHASE CSDR CAL950983Strut · flatFLT NR 305 - EWR - THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED UNTIL THE GEAR HANDLE WAS SELECTED DOWN FOR RETURN TO EWR. THE NOSE GEAR LIGHT INDICATED GREEN FOR LANDING AT EWR. MAINTENANCE FOU
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