N927AT
Service difficulty reports · 218
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 = 'N927AT' 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 = 'N927AT' 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 DALA2018040202109Support · crackedCRACKED VERTICAL SUPPORT BS 737 BELOW THE SEAT TRACK LBL 44. THE SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018040102108Tee Fitting · crackedCRACKED TEE FITTING, BS 389 LOWER EDGE, AT THE FWD CARGO DOOR. THE TEE FITTING WAS REPLACED IAW SRM 51-41-01-0G, 51-41-05-0G, AND DWG 3926046, REV B.SDR DALA2018040102107Beam · crackedCRACKED RT DOOR FRAME BEAM, AT THE NLG WHEEL WELL. THE BEAM WAS REPAIRED IAW SRM 53-10-14-2R, FIG 201.SDR DALA2018040102106Beam · crackedCRACKED LT DOOR FRAME BEAM AT THE NLG WHEEL WELL. THE BEAM WAS REPAIRED IAW SRM 53-10-14-2R, FIG 201.SDR DALA2018040102105Cusp Web · crackedCRACKED CUSP WEB, BS 673, BETWEEN RBL 54 TO 60. REPAIRED IAW SRM 53-00-55-2R-4.SDR DALA2018040102104Hinge · corrodedRIGHT ELEVATOR HINGE NR 5 AND 6, CORRODED. THE HINGE WAS REPAIRED IAW OHM 27-30-2, AND FOUND WITHIN LIMITS. FABRICATED BUSHINGS.SDR DALA2018040102103Intercostal · crackedINTERCOSTAL CRACKED BS 408, BETWEEN BEAM NR 5 TO UPPER EDGE AT THE FWD CARGO DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9957664, REV N.SDR DALA2018040102102Frame · crackedFRAME ANGLE CRACKED, BS 1021, LONGERON 16R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018040102101Angle · crackedCRACKED ANGLE BETWEEN BEAM NR 5 AND UPPER FWD EDGE, BS 408 AT THE FWD CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9957664, REV N.SDR DALA2018040102100Frame · crackedFRAME ANGLE CRACKED, BS 1021, LONGERON 14R, THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018040102099Pan · crackedCRACKED INNER PAN (SEEN FROM OUTSIDE) BS 954 BTW BEAM 1-2 AT AFT CARGO COMPARTMENT DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R FIG. 204.SDR DALA2018040102098Cusp Web · corrodedREPAIR DOUBLER CORRODED ON THE CUSP WEB, BETWEEN BS 540 - 560 LBL 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4.SDR DALA2018033102097Cusp Web · crackedSEVERAL CRACKS BS 655 - 672, 674, 698, AND 715 ON THE LT CUSP WEB. THE CUSP WEB WAS REPLACED IAW SRM 53-00-55-2R, FIG 203.SDR DALA2018033002096Cusp Web · crackedTHE RT CUSP WEB WAS CRACKED BS 594, BETWEEN RBL 54 - 56. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 217.SDR DALA2018033002171Floor Panel · crackedCRACKED FLOOR PANEL 221PF. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50-2R-3.SDR DALA2018033002095Floor Panel · delaminatedFLOOR PANEL 211ANF DELAMINATED IN THE COCKPIT. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50-2R-3 AND CARD 2040-0024.SDR DALA2018033002094Floor Panel · crackedCRACKED FLOOR PANEL 211ALF IN THE COCKPIT. THE FLOOR PANEL WAS FABRICATED IAW SRM 53-20-50-2R-3 AND INSTALLED IAW CARD 2040-0024 JOB 001-0061.SDR DALA2018033002093Cusp Web · corrodedLEFT CUSP WEB CORRODED BETWEEN BS 896 - 898, BETWEEN LBL 56 TO 60. HFEC INSPECTION WAS ACCOMPLISHED BETWEEN BS 896 - 898, LBL 56 TO 60, NO CRACKS WERE FOUND AFTER DAMAGE REMOVAL, IAW NDT SPM 06-10-01.001. DAMAGE AREA WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 2SDR DALA2018033002092Strap · corrodedCORRODED STRAP NEXT TO THE DOOR FRAME WEB BETWEEN BS 168 - 169, RBL 56. THE STRAP WAS REPLACED IAW SRM 53-10-15-0I-2, FIG.1, SRM 51-41-01-0G, SRM 51-41-02-0G, AND SRM 51-41-05-0G.SDR DALA2018033002091Cusp Web · corrodedRIGHT CUSP WEB CORRODED BS 381, BETWEEN RBL 56 TO 60. HFEC INSPECTION WAS ACCOMPLISHED ON CUT OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 53-00-55-2R FIG. 207.SDR DALA2018033002090Cusp Web · corrodedRIGHT CUSP WEB CORRODED BS 299 BETWEEN RBL 56 TO 60. HFEC INSPECTION WAS ACCOMPLISHED AFTER CUT OUT, AND NO CRACKS WERE FOUND IAW NDT SPM PART 6, 06-10-01.001. REPAIRED IAW SRM 53-00-55-2R, FIG 215.SDR DALA2018032902008Intercostal · crackedCRACKED INTERCOSTAL BS 184 BTW BEAM 4-5 AT THE L1 DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018032801978Cusp Web · crackedCRACKED RT CUSP WEB, BS 218 - 228, RBL 56 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4.SDR DALA2018032801977Cusp Web · crackedCRACKED RT CUSP WEB BETWEEN BS 718 - 724, RBL 54 TO 60. DAMAGE AREA WAS REPAIRED IAW SRM 53-00-55-2R, FIG 204. HFEC INSPECTION WAS ACCOMPLISHED ALONG THE TRIM LINES, NO CRACKS INDICATIONS WERE FOUND IAW NDT SPM 06-10-01.001.SDR DALA2018032701945Angle · crackedCRACK ON INTERNAL ANGLES, FWD & AFT UPPER CORNERS AND FWD LOWER CORNER. AT THE RT AFT EMERGENCY EXIT DOOR. THE ANGLES WERE REPLACED IAW DWG 9957735, REV G, SRM 51-41-05-0G, 51-41-02-0G, AND 51-41-01-0G.SDR DALA2018032701944Angle · crackedCRACK ON INTERNAL ANGLE, AFT UPPER CORNER AT THE LT AFT EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW DWG 9957735, REV G, SRM 51-41-05-0G, 51-41-02-0G, AND 51-41-01-0G.SDR DALA2018032701943Threshold · corrodedCORROSION ON METALIC STRIP AND WEB OF FWD SERVICE DOOR TRESHOLD.FILLER AND PANEL WERE REPLACED IAW DWG 9957828, REV Y.SDR DALA2018032701942Plate · corrodedCORROSION ON PLATES OF FWD SERVICE DOOR ENTRY. THE PLATES WERE REPLACED IAW SRM 51-40-08-0G.SDR DALA2018032601903Floor Panel · crackedCRACKED FLOOR PANEL 223FF IN THE PAX CABIN. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50-2R-3.SDR DALA2018032601902Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL 222AMF IN THE PAX CABIN. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50, 2R-3.SDR DALA2018032601900Pan · crackedCRACKED OUTER PAN BS 427 BETWEEN BEAMS 2 - 1, REPAIRED IAW SRM 52-30-02-2R-4, FIG 201.SDR DALA2018032601899Pan · crackedCRACKED OUTER PAN BS 370 BETWEEN BEAMS 2 - 1. REPAIRED IAW SRM 52-30-02-2R-4, FIG 201.SDR DALA2018032601898Angle · corrodedCORRODED FLOORBEAM BS 180, RBL 10 TO 43. THE FLOOR BEAM WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018032601897Pan · crackedCRACK ON RING PAN UPPER CORNER RT FWD FRAME BS 579. REPAIRED IAW SRM 56-20-02-2R1, FIG 202.SDR DALA2018032601896Pan · crackedCRACK ON RING PAN LOWER CORNER AFT FRAME BS 794. AREA WAS REPAIRED IAW SRM 56-20-02-2R1, FIG 202.SDR DALA2018032601895Floor Support · corrodedCORRODED FLOOR SUPPORT IN LBL 7 BETWEEN BS 148 - 200. FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-01-0G.SDR DALA2018032601894Pan · crackedCRACKED RING PAN ON UPPER CORNER FWD OF FRAME BS 832. AREA WAS REPAIRED IAW SRM 56-20-02-2R1 FIG 202.SDR DALA2018032601893Pan · crackedCRACKED RING PAN CORNER AFT FRAME, BS 655. THE AREA WAS REPAIRED IAW SRM 56-20-02-2R1, FIG 202. HFEC INSPECTION ACCOMPLISHED, NO CRACKS FOUND IAW NDT SPM 06-10-01.001.SDR DALA2018032601892Pan · crackedCRACKED RING PAN UPPER CORNER AFT OF FRAME, BS 696. THE AREA WAS REPAIRED IAW SRM 56-20-02-2R1, FIG 203. HFEC INSPECTION WAS ACCOMPLISHED, CRACKS FOUND IAW NDT SPM 06-10-01.001.SDR DALA2018032601891Pan · crackedCRACKED RING PAN ON UPPER CORNER FWD OF FRAME BS 889. THE AREA WAS REPAIRED IAW SRM 56-20-02-2R1, FIG 202. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND IAW SPM 06-10-01.001.SDR DALA2018032501890Skin · crackedEXTERNAL REPAIR DOUBLER WAS FOUND CRACKED BS 994 BETWEEN LONGERONS 24R - 26R. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-20-15-2R-12, FIGURE 201.SDR DALA2018032501889Skin · scratchedSCRATCHES ON TOPSIDE SKIN BETWEEN BS 446 AND 465, LONGERONS 3L TO 3R. THE SCRATCHES WERE BLEND OUT IAW SRM 53-02-01-2R, PAR 5.A. HFEC WAS ACCOMPLISHED, NO CRACKS FOUND AFTER BLEND OUT IAW SRM 53-02-01-2R PAR. 5.A.(1)(A)2, & NDT SPM 06-10-01.001 WAS ACCOMPLSDR DALA2018032501887Cusp Web · crackedCRACKED RT CUSP WEB BS 699, BETWEEN RBL 54 TO 60. DAMAGE AREA WAS REPAIRED IAW SRM 53-00-55-2R, FIG. 204.SDR DALA2018032501886Beam · crackedNR 1 BEAM CRACKED, L1 DOOR. REPAIRED IAW SRM 52-10-02-2R-7, FIGURES 201 & 202.SDR DALA2018032802007Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT, RBL 44 - 54, BS 160 - 200. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND SRM 51-41-05-0G.SDR DALA2018032802006Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT, BS 200 BETWEEN LBL 14 TO RBL 5. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G.SDR DALA2018032802005Floor Support · corrodedCORRODED FLOOR SUPPORT BS 200 BETWEEN RBL 10 TO 52. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G.SDR DALA2018032802004Plate · crackedCRACKED PLATE BS 1053, LBL 58. THE PLATE WAS REPLACED IAW SRM 51-41-05-0G, AND DWG 9910154, REV AM.SDR DALA2017122608920Slide · out of toleranceON SERVICE CHECK FOUND R1 SLIDE IN NO GO RANGE. REPLACED SERVICE DOOR SLIDE IAW T/C 2561-9005. INSTALLED A NEW R1 DOOR SLIDE. OPS CHECKED NORMAL.SDR DALA2017082206328Frame · dentedFRAME FORMER AT STA 237 L-17L HAS DENT DAMAGE. REPAIRED FRAME FORMER AT STA 237 BETWEEN LONGERON 17LT TO 16LT IAW SRM 53-00-06 REPAIR 2, 53-20-06 REPAIR 2, AND DRAWING 9911523 REV E. THIS IS A PERMANENT REPAIR WITH NO SPECIAL FOLLOW UP INSPECTIONS.
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