N24212
Service difficulty reports · 127
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 = 'N24212' 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 = 'N24212' 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 CALA2012100800658Frame · crackedRIGHT FRAME BS 440 HAS A CRACK INDICATION AT INBD FASTENER, REPAIRED FRAME IAW EA 5310-04716.SDR CALA2012100800657Frame · crackedLEFT FRAME BS 400 HAS A CRACK INDICATION, INBD FASTENER SIDE. REPAIRED FRAME IAW EA 5310-04716.SDR CALA2012100800656Frame · crackedLEFT FRAME, BS 440 HAS A CRACK, HFEC OTBD FASTENER SIDE. REPAIRED LT FRAME AT BS 440 IAW EA 5310-04716, REV C, FIG 3.SDR CALA2012100800654Frame · crackedLEFT FRAME, BS 867 SHOWS A CRACK INBD FASTENER. CUT OUT DAMAGED AREA IAW EA 5310-04716, FABRICATED REPAIR ANGLES IAW EA5310-04716 TREAT & PRIMED & INSTALLED IAW EA 5310-0 4716, REV C & SRM 51-40-02.SDR CALA2012100800653Frame · crackedFRAME BS 727F SHOWS A CRACK MFEC INBD FASTENER. REPAIR LT FRAME BS 727F, REF EA 5310-04716, REV C.SDR CALA2012100800652Frame · crackedRT FRAME BS 867 SHOWS A CRACK MFEC INBD FASTENER, REPAIRED CRACKED FRAME AT BS 867 RT SIDE IAW EA 5310-04716, REV C, OP 1.SDR CALA2011122300824Clamp · looseFL 380 PRESSURIZATION WARN HORN SOUNDED. RAN CHECKLIST UNABLE TO HOLD PRESS IN MANUAL. EMERGENCY DESCENT - PRESSURIZATION CONTROLLER IN MANUAL WORKED AT 5000 LWR PSI. FOUND APU DUCT REAR BELLOW IN KEEL BEAM CLAMP OFF, RESCUED. PERFORMED CABIN PRESSURE LEAKSDR CALA2011122300825Clamp · defectiveLOST PRESSURIZATION AT FL 360. NO INDICATION. SLOW CABIN CLIMB RATE - APPX 500 FPM. ABLE TO CONTROL CABIN DURING EMERG DESCENT IN "MAN". BITE CHECKED BOTH PRESSURE CONTROLLERS - CHECKED OK. FOUND PNEUMATIC DUCT PRESSURE SEAL IN AFT KEEL BEAM WITH BAD CLAMSDR CALA2010101300480Battery Pack · dischargedEMERGENCY EXIT LIGHTS AT THE R-1 DOOR AND FWD FIRST CLASS CABIN DO NOT ILLUMINATE DURING TEST REPLACED POWER SUPPLY BATTERY PACK. EMERGENCY EXIT LIGHTS OPERATE NORMAL. REF AMM 33-51-06-960-805.SDR CALA0800936Battery Pack · dischargedEMERGENCY LIGHT ON LEFT-HAND AFT BULLNOSE, LIGHTS ON SEATS 9-14 AND 26-29 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS M1694 AND M1672, SYSTEM OPERATIONAL CHECKS OK PER AMM 33-51-06-960-805.SDR CALA0800493Skin · corrodedAFT CARGO DOOR STATION 815 AT LOWER INNER SKIN HAS CORROSION. REPAIRED NOTED DAMAGED AREA IAW EC/RA 5232-01101.SDR CALA0800492Skin · corrodedAFT CARGO DOOR STATION 837 AT LOWER INNER SKIN HAS CORROSION. REPAIRED NOTED DAMAGED AREA IAW EC/RA 5232-01101.SDR CALA0800415Door Frame · corrodedL1 DOOR CHORD HAS CORROSION AT SEVERAL SCREW HOLES. REMOVED AND REPLACED L-1 DOOR CHORD PER SRM 51-40-02, B737-53-3-0735.SDR CALA0600482Support · corrodedINSPECTION FOUND CORROSION UNDER PANEL ON CROSS SUPPORT FORWARD OF C/P DOOR AT STA 270, BL 0. THE AREA WAS REPAIRED IAW ECRA 5311-01279 AND ECRA 5310-04585.SDR CALA0600241Battery · inoperativeTHE L-1 DOOR EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. THE EMERGENCY LIGHT BATTERY WAS REMOVED AND REPLACED IAW MM 33-51-06.SDR CALA0500165Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 43 TO RBL 29. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01222.SDR CALA0500164Seat Track · corrodedINSPECTION FOUND LT O/B SEAT TRACK CORRODED BETWEEN BS 360 AND 380 CLOSET MOUNT TRACK, LBL 45.5. THE SEAT TRACK WAS REMOVED AND REPLACED IAW ECRA 5321-01226.SDR CALA0500163Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 45 TO RBL 49. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01227.SDR CALA0500157Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 10. A REPAIR WAS INSTALLED IAW ECRA 5321-01223.SDR CALA0500156Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 12. A CAP WAS INSTALLED ON FLOORBEAM IAW ECRA 5321-01224.SDR CALA0500175Intercostal · crackedINSPECTION FOUND A 3/4" CRACK IN INTERCOSTAL AT STA 312-328, LBL 38. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-10-51, 51-20-01, AND 51-40-02,SDR CALA0500174Intercostal · crackedINSPECTION FOUND A 1/2 INCH CRACK IN INTERCOSTAL AT STA 270-294, LBL 50. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-51, 51-20-01, AND 51-40-02.SDR CALA0500173Intercostal · crackedINSPECTION FOUND A 3/4 INCH CRACK IN INTERCOSTAL AT STA 312-328, RBL 50. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-51, 51-20-01, AND 51-40-02.SDR CALA0400110Strap · lightning strikeINSPECTION FOUND RIGHT O/B HORIZONTAL STABILIZER TRAILING EDGE STRAP WITH EVIDENCE OF A LIGHTNING STRIKE. THE AFT O/B UPPER TRAILING EDGE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02. THE FIBERGLASS UNDERNEATH WAS REPAIRED IAW SRM 51-70-08 AND 51-21-101-7SDR CALA0300323Skin · dentedA FUELING TRUCK STRUCK THE AIRCRAFT ON THE FUSELAGE SKIN BETWEEN STA 1040 AND 1088 AND BETWEEN STRINGERS 18R AND 20R. THE DAMAGE INCLUDED PUNCTURED AND DENTED SKIN, SEVERED STRINGERS, A TWISTED STRINGER, DENTED SHEAR TIES, AND A DENTED FRAME. THE DAMAGED ARESDR CALA0200029Link · crackedINSPECTION FOUND THE NLG AFT LOCK LINK CRACKED DURING PSV INSPECTION. THE LOCK LINK WAS REMOVED AND REPLACED IAW MM 32-33-51, 401-801. AN ADJUSTMENT/TEST OF NLG LOCK SENSOR WAS PERFORMED IAW MM 32-61-41, PAGE 501. AN FCD IS BEING ISSUED TO PERFORM A DETAILESDR CALA0000229Skin · crackedINSPECTION BY MAINTENANCE, AFTER AIRCRAFT LANDED AND DRAGGED TAIL SKID ON RUNWAY, FOUND A 9 INCH CRACK IN FUSELAGE SKIN AT STA 887-920, S27L - S27R. THE SKIN WAS REPAIRED IAW ECRA 5330-02934 AND SRM 53-00-01.
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