N737CS
Service difficulty reports · 38
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 = 'N737CS' 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 = 'N737CS' 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 FY4Y202110002None · corrodedCORROSION FOUND AT LH WING REAR SPAR LOWER CHORD UPPER HORIZONTAL FLANGE WBL 162SDR FY4Y202105015Spar · crackedCRACK FOUND ON NO.5 FASTENER HOLE AT AFT SUPPORT FITTING AND REAR SPAR UPPER CHORD OF RH WING RSS 222SDR FY4Y202105014Spar · crackedCRACK FOUND ON NO.5 FASTENER HOLE AT REAR SPAR UPPER CHORD OF LH WING AS MARKED. (STA RSS 222)SDR FY4Y202110001Beam · crackedLONGITUDINAL FLOOR LONGITUDINAL FLOOR BEAM FOUND TWO CRACKS BETWEEN BS705 AND 715 RBL 24.82, CRACKS SIZE 3.0 INCH AND 1.5 INCH IN AREA.SDR FY4Y202110004Battery · noneELT BATTERY TIME DUE ON 2021/JULY. NRC:CA1251-01-015SDR FY4Y202110003Battery · weakEMER EXIT LIGHT BATTERY WEAK ON MAIN ENTRY DOOR UP SIDE. NRC:CA1251-01-014SDR FY4Y202105019Spar · corrodedCORROSION AT FWD UPPER L/H HORIZONTAL STABILIZER FRONT SPAR AT STAB. STA. 68~79SDR FY4Y202105018Spar · corrodedCORROSION AT FWD UPPER R/H HORIZONTAL STABILIZER FRONT SPAR AT STAB. STA. 68~75SDR FY4Y202105013Skin · corrodedCORROSION AT L/H WING SURGE TANK DRAIN VALVE (W STA 536)SDR FY4Y202105017Spar · corrodedBULGE AT UPPER SKIN OF LH HORIZONTAL STABILIZER AT STAB. STA. 71~79 AND FROM REAR SPAR +1"SDR FY4Y202105016Beam · corrodedCORROSION AT LH SIDE THRUST BEAM UPPER SURFACE AT STA. 1105 ~ 1130. (5EA)SDR FY4Y202105012Spar · corrodedCORROSION AT L/H WING L/E FRONT SPAR LOWER CHORD HORIZONTAL LEG BETWEEN FSS 431 AND FSS 452SDR JRAA202009110005Epr System · false indicationUPON APPLYING T/O THRUST NR 2 EPR GAUGE DID NOT RESPOND. T/O CLEARANCE CANCELLED, EXITED RUNWAY FOR TROUBLESHOOTING, NO RELIEF. CHECKED MEL, NO RELIEF, RETURNED TO RAMP.SDR JRAA20190501Warning System · activatedPILOT OBSERVED #2 ENGINE LOW OIL PRESSURE LIGHT IN FLIGHT AND PERFORMED IN FLIGHT SHUT DOWN PROCEDURESSDR JRAA201807170001Connector · brokenNUMBER 2 ENGINE FIRE LIGHT CAME ON IN FLIGHT. MX DISCOVERED BROKEN NUMBER 2 ENGINE FIRE DETECTOR LOOP CONNECTOR. ITEM PREVIOUSLY MEL'D PER MEL 737071618-1. PERFORMED SYSTEM OPS CHECKS PER AMM 26-11-00. OPS CHECK GOOD.SDR JRAA2016052504Sliding Window · crackedCOCKPIT L2 WINDOW CRACKED. APPEARS HEATING ELEMENT SHORTED, CRACKED OUTER PANE DETERMINED NON STRUCTURAL, FLIGHT CONTINUED, LANDED WINDOW INSPECTED AND ACFT RETURNED TO HOME BASE UNDER SPECIAL FERRY PERMIT. RESTRICTIONS, UNPRESSURIZED, BELOW 10,000FT. UNIT WASDR JRAA20160525003Selector Valve · stickingUNCOMMANDED LT MLG EXTENSION IN FLIGHT AT 315 KNOTS. REDUCED AIRSPEED AND REDUCED ALTITUDE. CORRECTED SEVERE YAW. SELECTED GEAR DOWN, 3 DOWN & LOCKED. CONTINUE TO DESTINATION. FLY-BY CONFIRMED GEARS DOWN AND PERFORMED A SAFE LANDING. JACKED ACFT, AND TROUSDR JRAA20160420002Sliding Window · crackedCOCKPIT L2 SLIDING WINDOW CRACKED. APPEARS HEATING ELEMENT SHORTED, CRACKED OUTER PANE DETERMINED NONSTRUCTURAL, FLIGHT CONTINUED & LANDED. WINDOW INSPECTED, ACFT RETURNED TO HOME BASE ON SPECIAL FERRY FLIGHT PERMIT, ISSUED 4 19 2016. REPLACEMENT WINDOW INSSDR 33AY2016FA0000063Keelbeam · corrodedINSPECTION FOUND LT KEEL BEAM LOWER CHORD, LBBL 6.30, CORRODED BETWEEN BS 540-BS 580. THE CORRODED HORIZONTAL FLANGE SECTION WAS BLENDED AND TRIMMED OUT. INSTALLED REPAIR FILLERS, REPAIR STRAP AND REPAIR ANGLE IAW REPAIR PLAN 121083-R041, REV 02.SDR 33AY2016FA0000053Keelbeam · cutINSPECTION FOUND LT KEEL BEAM LOWER CHORD, LBL 6.30, CORRODED AND CRACKED BETWEEN BS 668 - 672. THE KEEL BEAM LOWER CHORD WAS CUT AT BS 625 AND THE KEEL BEAM AFT SEGMENT WAS REMOVED AND THEN REPLACED WITH NEW PART BETWEEN BS 625-BS 727+16 IAW REPAIR PLAN NR 1SDR 33AY2016FA0000071Fitting · corrodedINSPECTION FOUND STRINGER FITTING AT S-27L, BS 1016 BULKHEAD CORRODED. THE DAMAGED STRINGER FITTING WAS R & R BY INSTALLING A NEW FITTING IAW SRM 51-3-02, REV 108.SDR 33AY2016FA0000070Fitting · corrodedINSPECTION FOUND STRINGER FITTING AT S26R, STA 1016 BULKHEAD CORRODED. THE DAMAGED STRINGER FITTING WAS R & R BY INSTALLING A NEW FITTING IAW SRM 51-3-02, REV 108.SDR 33AY2016FA0000069Fitting · corrodedINSPECTION FOUND STRINGER FITTING AT S-26L, BS 1016 BULKHEAD CORRODED. THE DAMAGED STRINGER FITTING WAS R & R BY INSTALLING A NEW FITTING IAW SRM 51-3-02, REV 108.SDR 33AY2016FA0000068Fitting · corrodedINSPECTION FOUND STRINGER FITTING AT S-25R, STA 1016 BULKHEAD CORRODED. THE DAMAGED STRINGER FITTING WAS R & R BY INSTALLING A NEW FITTING IAW SRM 51-3-02, REV 108.SDR 33AY2016FA0000066Fuel Cell · corrodedINSPECTION FOUND CENTER TANK LOWER SKIN CORRODED BETWEEN S-9C TO S-10C, LBBL 6.30 TO RBBL 6.30. THE CORRODED SKIN AREAS WERE BLENDED. THE AREA WAS FOUND OUT OF SRM ALLOWABLE LIMIT AND REPAIRED IAW REPAIR PLAN 121083-R043, REV 06. EXTERNAL REPAIR DOUBLER WASSDR 33AY2016FA0000065Fitting · corrodedINSPECTION FOUND STRINGER FITTING AT STRINGER 27R, BS 1016 BULKHEAD CORRODED. THE DAMAGED STR FITTING WAS R & R BY INSTALLING A NEW FITTING IAW SRM 51-3-02, REV 108.SDR 33AY2016FA0000064Fuel Tank · corrodedINSPECTION FOUND CENTER TANK LOWER SKIN CORRODED BETWEEN S-4C TO S-5C, LBBL 6.30 TO RBBL 6.30. THE CORRODED SKIN AREAS WERE BLENDED. THE AREA WAS FOUND OUT OF SRM ALLOWABLE LIMIT AND REPAIRED IAW REPAIR PLAN 121083-R043, REV 06.SDR 33AY2016FA0000057Frame · corrodedINSPECTION FOUND FRAME UPPER FLANGE AT BS 500B BETWEEN STR 25R TO STR 26R CORRODED OUT OF SRM ALLOWABLE LIMIT. THE DAMAGED SECTION WAS TRIMMED OUT AND REPAIR FILLER AND FRAME DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-03, REV 108.SDR 33AY2016FA0000056Skin · corrodedINSPECTION FOUND CORROSION ON UPPER SKIN FAYING SURFACE AT LAP JOINT STR 26R BETWEEN BS 500 TO BS 500A. THE CORRODED UPPER SKIN SECTION WAS TRIMMED OUT AND EXTERNAL REPAIR DOUBLER WAS INSTALLED. REPAIR WAS DONE IAW SRM 53-30-3, REV 108.SDR 33AY2016FA0000055Frame · corrodedINSPECTION FOUND FRAME UPPER FLANGE AT BS 492 BETWEEN STR 25R CORRODED OUT OF SRM ALLOWABLE LIMIT. THE DAMAGED SECTION WAS TRIMMED OUT AND REPAIR FILLER AND FRAME DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-03, REV 108.SDR 33AY2016FA0000054Skin · corrodedINSPECTION FOUND CORROSION ON UPPER SKIN FAYING SURFACE AT LAP JOINT STR 26R BETWEEN BS 370 TO BS 400. THE CORRODED UPPER SKIN SECTION WAS TRIMMED OUT AND EXTERNAL REPAIR DOUBLER WAS INSTALLED. REPAIR WAS DONE IAW SRM 53-30-3, REV 108.SDR 33AY2016FA0000062Skin · dentedAIRCRAFT FOUND WITH DENT AND GOUGE DAMAGE TO THE SKIN ABOVE THE FWD CARGO DOOR CUTOUT, AT APPROXIMATELY BS 450, STR 18R. THIS DAMAGE IS WITHIN 10" OF THE DOOR AND IS THEREFORE OUT OF LIMITS FOR REPAIR 1, FIG 48. THIS DAMAGE WAS REPAIRED IAW REPAIR DOCUMENT 1SDR 33AY2016FA0000073Keelbeam · corrodedINSPECTION FOUND RT KEEL BEAM LOWER CHORD HORIZONTAL FLANGE CORRODED BETWEEN BS 540-BS 580, RBL 6.30. THE CORRODED FLANGE SECTION WAS BLENDED AND TRIMMED OUT. INSTALLED REPAIR FILLERS, REPAIR FILLERS, REPAIR STRAP AND REPAIR ANGLE IAW REPAIR PLAN 121083-R044SDR 33AY2016FA0000059Frame · corrodedINSPECTION FOUND FRAME AT BS 787, BETWEEN STR 25L TO STR 26L CORRODED OUT OF SRM ALLOWABLE LIMIT. THE DAMAGED SECTION WAS TRIMMED OUT AND FRAME REPAIR DOUBLER WAS INSTALLED IAW EA B737-53-004.SDR 33AY2016FA0000058Frame · corrodedINSPECTION FOUND FRAME UPPER FLANGE AT BS 887 ABOVE STRINGER STR 26L CORRODED OUT OF SRM ALLOWABLE LIMIT. THE DAMAGED SECTION WAS TRIMMED OUT AND FRAME REPAIR DOUBLE WAS INSTALLED IAW EA B737-53-004.SDR 33AY2016FA0000067Splice · corrodedINSPECTION FOUND KEEL BEAM SPLICE CORRODED AT LBBL 6.30, BS 727-BS727A. THE DAMAGED SPLICE WAS R & R IAW SRM 51-30-02.SDR 33AY2016FA0000072Skin · corrodedINSPECTION FOUND LT WING LOWER T/E SKIN CORRODED BETWEEN WBL 254 TO WBL 279.25 . THE CORRODED SKIN AREA WAS BLENDED AND REPAIRED IAW REPAIR PLAN 121083-R039, REV 02.SDR 33AY2016FA0000060Door Frame · corrodedINSPECTION FOUND AFT CARGO DOORWAY AFT FRAME AT BS 847 CORRODED. REPAIRED IAW AD 93-14-10 AND SB 737-53-1096, REV 5 BY REMOVING THE DAMAGED FRAME SEGMENT AND INSTALLING A NEW FRAME REPAIR KIT WITH PN 65C35243-11.
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