N925AT
Service difficulty reports · 182
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 = 'N925AT' 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 = 'N925AT' 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 DALA2021022501093Power Supply · inoperativeON THE SERVICE CHECK, MAINTENANCE FOUND THE OVER WING WALL EXIT LIGHT TO BE INOPERATIVE AT ROW 20. MAINTENANCE REPLACED THE POWER SUPPLY LOCATED AT B5-119. THE EMERGENCY LIGHTS NOW OPERATE NORMALLY REF B717 AMM 33-51. (LP 7596098)SDR DALA2021021200817Slide · no testTHE L1 DOOR SLIDE FAILED THE DEPLOYMENT TEST FORECAST #95-0525-0111 DUE TO THE LANYARD NOT ATTACHED TO GIRT BAR. PN- D29982-225 SN-2678 MFR DATE- 11/09. MAINTENANCE REPLACED THE SLIDE PER W/C 2561-9001. (LP #1728645)SDR DALA2020021801203Door Frame · corrodedAFT CARGO DOOR JAMB INTERNAL FACTORY ALUMINUM DOUBLER IS CORRODED FOR APPROXIMATELY 6 INCHES FWD AND AFT OF CENTERLINE. NRC 001-0304:5231-2002/002 00218: COMPILED WITH ER/A 585336-14 ORIGINAL. (LP #1494200)SDR DALA2020021801202Door Frame · corrodedAFT CARGO DOOR JAMB HAS CORROSION. NRC 001-0304:5231-2002/001 00013: REPAIRED REF B717 SRM 53-20-15-2R PROC 7. (LP #1493931)SDR DALA2019041102393Battery Pack · inoperativeTHE EMERGENCY LIGHTS IN ROW 5, 6, & 7 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IAW B717 AMM 33-55. ALL CHECKS ARE GOOD. (LP #5531007)SDR DALA2018032701941Frame · corrodedCORROSION ON FRAME BS 1022, BETWEEN LONGERONS 20R - 22R. REPAIRED IAW SRM 53-20-07-2R, REPAIR 3.SDR DALA2018032701940Frame · crackedCRACKED FRAME BS 1162, BETWEEN LONGERONS 1L AND 2L. REPAIRED IAW ETI-17-18-061, REV 1, AND ER/A 567141-14, REV ORIGINAL.SDR DALA2018032601901Angle · crackedCRACKED ANGLE BS 1162 LONGERON 2L. REPLACED IAW SRM 51-41-02 AND SRM 51-41-05.SDR DALA2018032501888Shear Tie · corrodedCORROSION ON THE FRAME SHEAR TIE BS 1022 BETWEEN LONGERONS 29L - 29R. THE FRAME SHEAR TIE WAS REPLACED IAW DWG 9958214, REV BW, SRM 51-41-02, AND 51-41-05.SDR DALA2018032401885Intercostal · corrodedCORROSION THE ON THE INTERCOSTAL, LONGERON 30 BETWEEN BS 1022 - 1037. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-05.SDR DALA2018032301850Floor Panel · corrodedCORROSION ON FLOOR PANEL 221NF. THE FLOOR PANEL WAS REPLACED IAW AMM 53-21-01.SDR DALA2018032301849Hinge Fitting · wornFREE PLAY AT THE LT WING OTBD FLAP HINGE FITTING. OTBD FLAP HINGE WAS REPAIRED IAW ETI-17-18-056, REV 3, AND ER/A 566913-14, REV ORIGINAL.SDR DALA2018032301884Frame Angle · corrodedCORROSION ON FRAME ANGLE BS 954 BETWEEN LONGERON 27L TO 29R IN THE AFT CARGO BAY. THE FRAME ANGLE WAS REPLACED IAW SRM 53-00-06-2R, REPAIR 2, AND DWG 9958214, REV BW.SDR DALA2018032201834Angle · corrodedCORROSION TYPE EXFOLIATION AT RT CUSP ANGLE STA 200. CORROSION LEVEL 2, RT CUSP ANGLE STA 200 WAS REPAIRED PER ETI-17-18-045 REV 1 AND ER/A 566866-14 REV ORIGINAL.SDR DALA2018032201833Fitting · crackedCRACK ON CLIP FRAME BTW LONG 25R TO 26R STA Y=870. FRAME CLIP WAS REPAIRED PER SRM 53-00-06-2R REPAIR 2. HFEC INSPECTION WAS ACCOMPLISHED ON CLIP FRAME BTW LONG 25R TO 26R STA Y=870 AFTER TRIM OUT. NO CRACKS WERE FOUND PER NDT SPM PART 6, 06-10-01.001.SDR DALA2018032101820Gusset · crackedCRACKED GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROTECTION LONG 7R AT PAX CABIN. GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROJECTION LONG 7R WAS REPAIRED PER ETI-17-18-043 REV 1 AND ER/A 566865-14 REV ORIGINAL.SDR DALA2018031901764Floor Panel · delaminatedDELAMINATION ON FLOOR PANELS #221AF, 221DF, 221FF, 221BF, 221CF, 221JF, 221HF, 222ANF, AND 222RF AT PAX CAB (CPAX). NRC 00560: FLOOR PANELS #221AF, 221DF, 221FF, 221BF, 221CF, 221JF, 221HF, 222ANF, AND 222RF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SDR DALA2018031901767Longeron · corrodedCORROSION OUT OF LIMITS ON LONGERON 30, BS 934 TO 1002. CORROSION OUT OF LIMITS. THE LONGERON WAS REPLACED IAW SRM 53-20-05-01-3, FIG 1.SDR DALA2018031901766Longeron · corrodedCORROSION ON LONGERON 30 BETWEEN BS 1022 - 1037. THE LONGERON SECTION WAS REPLACED IAW SRM 51-41-05-0G, AND SRM 51-41-02-0G.SDR DALA2018031901765Longeron · corrodedCORROSION ON LONGERON 27L BETWEEN BS 990 TO 1022. THE LONGERON SECTION WAS REPLACED SRM 53-20-05-01-3, FIG 1, AND 51-40-08.SDR DALA2018031801760Floor Panel · brokenBROKEN CHANNEL ON GEN FLOOR PANELS #221GF, 222AJF, AND 222EF. NRC 00536: GEN FLOOR PANELS #221GF, 222AJF, AND 222EF WERE REPAIRED PER B717 SRM 53-20-50-2R REPAIR 5 FIG. 202. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON GEN FLOOR PANELS #222AJF AND 222EF AFTER STOPSDR DALA2018031801763Floorbeam · crackedCRACKED FLOORBEAM BS 645. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 5971111, REV F.SDR DALA2018031801762Skin Splice · corrodedCORROSION ON SKIN SPLICE BS 898, BETWEEN LONGERONS 26L TO 30L. THE SKIN SPLICE WAS REPLACED IAW SRM 53-20-01-0I-3, FIG 1. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEETS 1 AND 2. FOUND OUT LIMITS IAW SRM 53-00-00-1A, ALLOWABLE DAMAGE PAR 4, FISDR DALA2018031901813Pan · crackedCRACK FOUND ON THE FWD EDGE OUTER PAN BELOW THE NR 2 STOP FITTING AT THE FWD CARGO DOOR. REPAIRED IAW ETI-17-18-055, REV 1, AND ER/A 566780-14, REV ORIG.SDR DALA2018031701759Longeron Splice · corrodedCORROSION ON THE LONGERON 30 SPLICE BETWEEN BS 927 TO 946. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-41-05.SDR DALA2018031701758Longeron Splice · corrodedCORROSION ON LONGERON SPLICE 27L BETWEEN BS 973 TO 994 IN THE AFT CARGO BAY. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-41-05.SDR DALA2018031701756Strap · corrodedCORROSION ON STRAP AT LONGERON 25L BETWEEN BS 1002 TO 1022. THE STRAP WAS REPLACED IAW SRM 51-41-05, AND DWG 5936021, REV EG.SDR DALA2018031701750Frame Angle · crackedCRACKED FRAME ANGLE, FWD FACE BS 1022, BETWEEN LONGERONS 7L - 8L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, AND 51-41-05 AND DWG 9912243, REV JS. HFEC INSPECTION WAS ACCOMPLISHED AND A CRACK WAS CONFIRMED IAW NDT SPM 06-10-01.001.SDR DALA2018031501713Membrane · corrodedCORROSION ON MEMBRANE STA Y=200 X=-54 5300-2010. CORROSION LEVEL 2, MEMBRANE WAS REPAIRED PER SRM 51-70-10-2R. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON MEMBRANE STA Y=200 X=-54, NO CRACKS WERE FOUND AFTER CUT OUT PER NDTSPM 06-10-01.001.SDR DALA2018031501709Floor Support · corrodedCORROSION ON FLOOR SUPPORTS STA Y=200, X=-7, AND X=-44 REF 5300-2010 CPAX. CORROSION LEVEL 2, FLOOR SUPPORTS STA Y=200, X=-7, AND X=-44 WERE REPLACED PER SRM 51-41-02.SDR DALA2018031501708Floor Support · corrodedCORROSION ON FLOOR SUPPORTS STA Y=200 X=-10 TO X=-44, X=-44 TO X=-54, AND X=7 TO X=-7 REF AMDS 5300-2010 CPAX. CORROSION LEVEL 2, FLOOR SUPPORTS STA Y=200 X=-10 TO X=-44, X=-44 TO X=-54, AND X=7 TO X=-7 WERE REPLACED PER SRM 51-41-02.SDR DALA2018031401687Seat Track · corrodedCORROSION ON THE SEAT TRACK LBL 54, BETWEEN BS 240 TO 247. THE SEAT TRACK WAS REPAIRED IAW SRM 53-20-52-2R-5.SDR DALA2018031401684Cusp Web · corrodedCORROSION ON THE CUSP WEB, BS 902 TO 904, LBL 54 TO RBL 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215.SDR DALA2018031301683Cusp Web · crackedCRACK ON THE RT CUSP WEB, BS 674, RBL 46: THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R-2. HFEC WAS ACCOMPLISHED ON EDGES OF TRIMMED AREA, NO CRACKS FOUND IAW NDT SPM PART 6, 06-10-01.001,SDR DALA2018031301626None · noneEXCESSIVE CORROSION ON FUEL ACCSESS PLATE #620CT, 520CT, AND 520DT AT SETTLEMENT AND COUNTERSINK AREA RH/LH WING IN REFERENCE NRCS 00549, 00553, AND 00554. NRC 00603: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND 620CT WERE REPLACED DUE TO BLEND OUT REPAIR SDR DALA2018031301625Floor Panel · corrodedCORRODED FLOOR PANEL. A NEW FLOOR PANEL WAS FABRICATED, AND REPLACED IAW DWG 9957828, REV AB.SDR DALA2018031201620Floor Panel · crackedCRACKS ON FLOOR PANELS #221EF, 211ANF, AND 223GF AT PAX CAB (CPAX). NRC 00556: FLOOR PANELS #221EF, 211ANF, AND 223GF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50. FLOOR PANELS WERE INTALLED WITH JIC CARD 2040-0024. (LP #0460121)SDR DALA2018031201623Access Panel · corrodedCORROSION OUT OF LIMITS ON ACCESS PANEL 620AT. THE ACCES PANEL WAS REPLACED IAW SRM 57-10-01-2R-2, PAR 5.SDR DALA2018031201622Door Frame · crackedCRACKED NLG DOOR FRAME, RT SIDE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2. HFEC WAS ACCOMPLISHED, NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM PART 6, 06-10-01.SDR DALA2018031201621Door Frame · crackedCRACKED DOOR FRAME AT THE NLG LT SIDE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2. HFEC WAS ACCOMPLISHED, AND NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM PART 6, 06-10-01.SDR DALA2018031201619Web · crackedCRACKED WEB BS 208, LONGERON 15L. THE WEB WAS REPAIRED IAW SRM 53-10-15-2R, PR 4. HFEC INSPECTION PERFORMED AND NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM 06-10-01.001.SDR DALA2018031201618Cusp Web · crackedCRACKED CUSP WEB BS 219, LBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R. HFEC INSPECTION WAS PERFORMED AT THE TRIMMED OUT AREA. NO CRACKS WERE FOUND IAW NDT SPM PART 6 06-10-01.001.SDR DALA2018031201617Angle · crackedCRACKED ANGLE AT THE RT FWD EMERGENCY EXIT DOOR UPPER BEAM FWD EDGE. THE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9957735, REV G.SDR DALA2018031201616Angle · crackedCRACKED ANGLE AT THE FWD CARGO DOOR BETWEEN THE UPPER EDGE AND BEAM 1 AND NEXT TO AFT HINGE. THE ANGLE WAS REPLACED SRM 51-41-02, 51-41-05, AND DWG 9957664, REV N.SDR DALA2018031201615Cusp Web · corrodedCORROSION ON THE RT CUSP WEB BS 389, RBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R -2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND ON TRIMMED OUT AREA IAW NDT SPM 06-10-01.SDR DALA2018031201614Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT BETWEEN BS 120 TO 148, RBL 50 IN THE COCKPIT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-08, AND DWG 9936533, REV CM.SDR DALA2018031101612Rub Strip · corrodedCORROSION ON RUBSTRIPS OF THE FUEL ACCESS PANELS 520GB AND 520MB ON THE LT WING THE RUBSTRIPS WERE REPLACED IAW SRM 57-10-01-2R, REP 3, PAR 6.SDR DALA2018031101611Skin · puncturedPUNCTURE ON AFT EDGE INTERNAL SKIN OF LT MLG DOOR. THE DOOR SKIN WAS REPAIRED IAW SRM 52-82-02-2R-1, FIG 201, SHEET 5.SDR DALA2018031101610Frame Angle · crackedCRACKED FRAME ANGLE AFT FACE, BS 1022 BETWEEN LONGERONS 16 - 17R. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DRAWING 9912243, REV JS.SDR DALA2018031101609Frame Angle · crackedCRACKED FRAME ANGLE, FWD FACE BS 1022 BETWEEN LONGERONS 16 - 17R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, AND SRM 51-20-09.
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