N610CZ
Service difficulty reports · 123
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 = 'N610CZ' 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 = 'N610CZ' 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 SWI2024F01278Stringer · corrodedCORROSION - RH STRINGER 19R CORRODED AS MARKED FR 88-90 (C-CHECK RO 10/30/2024) (FILED CLOSED)PERFORMED STRINGER SPLICE REPAIR BETWEEN FRAMES 88-90 REF ETD2024-170-027361. SEE CONTINUATION CARD FOR ALL WORK PERFORMED.SDR SWIA2024F01083Stringer · corrodedCORROSION - LH STRINGER 19L CORRODED AS MARKED FR 88-90 (C-CHECK RO 10/30/2024) (FILED OPEN)REMOVED DAMAGE SECTION OF LH STRINGER 19L FR 88-90. LOCATED DRILLED AND INSTALLED NEW LH STRINGER 19L REPAIR REF: ETD2024-170-027358. SEE CONTINUATION CARD FOR ALL SDR SWIA2024103010Stringer · corrodedCORROSION - RH STRINGER 19R CORRODED AS MARKED FR 88-90 (C-CHECK RO 10/30/2024) (FILED OPEN)PERFORMED STRINGER SPLICE REPAIR BETWEEN FRAMES 88-90 REF ETD2024-170-027361. SEE CONTINUATION CARD FOR ALL WORK PERFORMED.SDR SWIA20241115008Skin · crackedRH WING MAIN BOX LOWER SKIN (LOWER SURFACE) ALONG SPAR 01 HAS SUSPECTED CRACK AT RIVET IN BETWEEN SLAT #3 AND #4. (C-CHECK RO 10/30/2024) (FILED CLOSED)REPAIRED CRACK IN RH WING MAIN BOX LOWER SKIN AT RIB 20 BY FILLER AND DOUBLER REPAIR REF ETD2024-170-027059SDR SWIA2024103008Skin · crackedRH WING MAIN BOX LOWER SKIN (LOWER SURFACE) ALONG SPAR 01 HAS SUSPECTED CRACK AT RIVET IN BETWEEN SLAT #3 AND #4. (C-CHECK RO 10/30/2024) (FILED OPEN)REPAIRED CRACK IN RH WING MAIN BOX LOWER SKIN AT RIB 20 BY FILLER AND DOUBLER REPAIR REF ETD2024-170-027059. SDR SWI2024F01259Seat Track · gougedMAIN CABIN LH LATERAL SEAT TRACK FR 19-21 HAS GOUGE DAMAGE AS MARKED. (C-CHECK RO 10/30/2024) (FILED CLOSED)REMOVED AND REPLACED LH LATERAL SEAT TRACK FR 19-21 WITH NEW REF. SRM 51-40-08. SEAT TRACK REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED.SDR SWI2024F01258Seat Track · gougedMAIN CABIN LH LATERAL SEAT TRACK FR 22-23 HAS GOUGE DAMAGE AS MARKED. (C-CHECK RO 10/30/2024) (FILED CLOSED)REMOVED AND REPLACED LH LATERAL SEAT TRACK FR 22-23 WITH NEW REF. SRM 51-40-08, AMM 20-10-01. CAL. TOOL I.D.# HG2-61285, DUE DATE 7-22-25. SEAT TRACK RESDR SWI2024F01257Seat Track · gougedMAIN CABIN LH 1ST CLASS FLOOR SEAT TRACK FR 20-22 HAS GOUGE DAMAGE AS MARKED. (C-CHECK RO 10/30/2024) (FILED CLOSED)REMOVED AND REPLACED LH 1ST CLASS FLOOR SEAT TRACK FR 20-22 WITH NEW REF. SRM 51-40-08.SEAT TRACK REPLACED WITH OEM PART NO CHANGE TO WEIGHT ANDSDR SWI2024F01256Crossbeam · corrodedMAIN CABIN FORWARD WET AREA HAS CORROSION ON CROSS BEAM FR 14 BELOW FORWARD GALLEY AREA. (C-CHECK RO 10/30/2024) (FILED CLOSED) PERFORMED PERMANENT DOUBLER REPAIR ON FR 14 CROSS BEAM REF. SRM 53-00-10 /REPAIR 03P. CHANGE IN WEIGHT 563.26 GRAMS. CAL. TOOL I.D.#SDR SWI2024F01255Crossbeam · corrodedMAIN CABIN FORWARD WET AREA HAS CORROSION ON CROSS BEAM FR 17 UNDER WARDROBE AREA. (C-CHECK RO 10/30/2024) (FILED CLOSED) REMOVED DAMAGE SECTION OF MAIN CABIN FORWARD WET AREA CROSS BEAM FR 17 UNDER WARDROBE AREA BY CUTTING AWAY DAMAGE. FABRICATED AND INSTALLESDR SWI2024F01254Seat Track · corrodedMAIN CABIN FORWARD WET AREA HAS SCRATCH AND CORROSION DAMAGE ON RH FLOOR TRACK FR 12-19 AS MARKED. (C-CHECK RO 10/30/2024) (FILED CLOSED)REMOVED AND REPLACED THE R/H FLOOR SEAT TRACK, FRAME 12-19 REF ERJ175 SRM 51-40-08. SEE CONTINUATION CARD FOR ALL WORK PERSDR SWIA2024111500004Seat Track · corrodedMAIN CABIN FORWARD WET AREA HAS CORROSION SPOTS ON TOP SIDE OF LH FLOOR TRACK FR 16-20. (C-CHECK RO 10/30/2024) (FILED CLOSED)REMOVED AND REPLACED THE L/H FLOOR SEAT TRACK, FRAME 12-20 REF ERJ175 SRM 51-40-08. SEE CONTINUATION CARD FOR ALL WORK PERFORMED. PARSDR SWIA2024F01082Seat Track · gougedMAIN CABIN LH LATERAL SEAT TRACK FR 19-21 HAS GOUGE DAMAGE AS MARKED. (C-CHECK RO 10/30/2024) (FILED OPEN)REMOVED AND REPLACED LH LATERAL SEAT TRACK FR 19-21 WITH NEW REF. SRM 51-40-08. SEAT TRACK REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED. SSDR SWIA2024F01081Seat Track · gougedMAIN CABIN LH LATERAL SEAT TRACK FR 22-23 HAS GOUGE DAMAGE AS MARKED. (C-CHECK RO 10/30/2024) (FILED OPEN)REMOVED AND REPLACED LH LATERAL SEAT TRACK FR 22-23 WITH NEW REF. SRM 51-40-08, AMM 20-10-01. CAL. TOOL I.D.# HG2-61285, DUE DATE 7-22-25. SEAT TRACK REPLSDR SWIA2024F01080Seat Track · gougedMAIN CABIN LH 1ST CLASS FLOOR SEAT TRACK FR 20-22 HAS GOUGE DAMAGE AS MARKED. (C-CHECK RO 10/30/2024) (FILED OPEN)REMOVED AND REPLACED LH 1ST CLASS FLOOR SEAT TRACK FR 20-22 WITH NEW REF. SRM 51-40-08.SEAT TRACK REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BSDR SWIA2024F01079Floorbeam · corrodedMAIN CABIN FORWARD WET AREA HAS CORROSION ON CROSS BEAM FR 14 BELOW FORWARD GALLEY AREA. (C-CHECK RO 10/30/2024) (FILED OPEN) PERFORMED PERMANENT DOUBLER REPAIR ON FR 14 CROSS BEAM REF. SRM 53-00-10 /REPAIR 03P. CHANGE IN WEIGHT 563.26 GRAMS. CAL. TOOL I.D.# SSDR SWIA2024F01078Floorbeam · corrodedMAIN CABIN FORWARD WET AREA HAS CORROSION ON CROSS BEAM FR 17 UNDER WARDROBE AREA. (C-CHECK RO 10/30/2024) (FILED OPEN) REMOVED DAMAGE SECTION OF MAIN CABIN FORWARD WET AREA CROSS BEAM FR 17 UNDER WARDROBE AREA BY CUTTING AWAY DAMAGE. FABRICATED AND INSTALLED SDR SWIA2024F01077Seat Track · corrodedMAIN CABIN FORWARD WET AREA HAS SCRATCH AND CORROSION DAMAGE ON RH FLOOR TRACK FR 12-19 AS MARKED. (C-CHECK RO 10/30/2024) (FILED OPEN)REMOVED AND REPLACED THE R/H FLOOR SEAT TRACK, FRAME 12-19 REF ERJ175 SRM 51-40-08. SEE CONTINUATION CARD FOR ALL WORK PERFOSDR SWIA2024103004Seat Track · corrodedMAIN CABIN FORWARD WET AREA HAS CORROSION SPOTS ON TOP SIDE OF LH FLOOR TRACK FR 16-20. (C-CHECK RO 10/30/2024) (FILED OPEN)REMOVED AND REPLACED THE L/H FLOOR SEAT TRACK, FRAME 12-20 REF ERJ175 SRM 51-40-08. SEE CONTINUATION CARD FOR ALL WORK PERFORMED. PART SDR SWIA202411150002Shear Tie · corrodedSHEAR CLIP AT FR 88 BETWEEN STRINGERS 27R-28R CORRODED. (C-CHECK RO 10/30/2024) (FILED CLOSED)REMOVED AND REPLACED SHEAR CLIP AT FR 88 BETWEEN STRINGERS 27R-28R REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.SHEAR CLIP REPLACED WITH OEM PART NOSDR SWIA2024103002Shear Tie · corrodedSHEAR CLIP AT FR 88 BETWEEN STRINGERS 27R-28R CORRODED. (C-CHECK RO 10/30/2024) (FILED OPEN)REMOVED AND REPLACED SHEAR CLIP AT FR 88 BETWEEN STRINGERS 27R-28R REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.SHEAR CLIP REPLACED WITH OEM PART NO CSDR SWIA202411150001Bearing · no testHORIZONTAL STABILIZER FAILED ROLL BACKLASH FUNCTIONAL TEST. (C-CHECK RO 10/30/2024) (FILED CLOSED)REMOVED AND REPLACED HORIZONTAL STABILIZER BEARINGS, SEE CONTINUE CARDS FOR WORK PERFORMED. COMPLIED WITH ETD 2024-170-028112 REACCOMPLISHED HORIZONTAL ROLL BACKLSDR SWIA2024103001Bearing · failedHORIZONTAL STABILIZER FAILED ROLL BACKLASH FUNCTIONAL TEST. (C-CHECK RO 10/30/2024) (FILED OPEN) REMOVED AND REPLACED HORIZONTAL STABILIZER BEARINGS, SEE CONTINUE CARDS FOR WORK PERFORMED. COMPLIED WITH ETD 2024-170-028112 REACCOMPLISHED HORIZONTAL ROLL BACKLASDR SWI2024F01260Spar · crackedSUSPECTED CRACK ON LH HORIZONTAL SPAR 1 INBD FWD LOWER FLANGE (C-CHECK RO 10/30/2024) (FILED CLOSED)REPAIRED CRACK ON LH HORIZONTAL SPAR 1 REF ETD2024-170-026288 AND TI-170-24-245. SEE CONTINUE CARD FOR WORK PERFORMED.SDR SWIA202410301076Spar · crackedSUSPECTED CRACK ON LH HORIZONTAL SPAR 1 INBD FWD LOWER FLANGE (C-CHECK RO 10/30/2024) (FILED OPEN)REPAIRED CRACK ON LH HORIZONTAL SPAR 1 REF ETD2024-170-026288 AND TI-170-24-245. SEE CONTINUE CARD FOR WORK PERFORMED.SDR SWIA20230205Not Reported · failedBEFORE DEPARTURE WE NOTICED SOME NICKS ON THE N1 BLADES FOR ENGINE 2. WE HAD MAINTENANCE COME OUT AND CORRECT IT. WHILE IN ROUTE TO BOSTON WE GOT HIGH VIBES ON ENGINE 2. RAN THE QRH PROCEDURE FOR HIGH ENGINE VIBRATION. ENGINE 2 MAX HP VIBE 4.0 (AMBER). THEN ATSDR SWIA2021082060611Intercostal · corrodedCORROSION AROUND LOWER FASTENERS ON LH INTERCOSTAL BETWEEN FRAMES 85 AND 86. (C-CHECK RO 8/18/2021) REMOVED AND REPLACED LH INTERCOSTAL BETWEEN FRAMES 85 AND 86 REF. EMB 175 SRM 51-40-08..SEE CONTINUATION CARD FOR WORK DONESDR SWIA2021082060610Skin · dentedFORWARD FUSELAGE SKIN DENTED FRAME 19 STRINGERS 20L/21L (C-CHECK RO 8/18/2021) / PERFORMED CUTOUT AND DOUBLER REPAIR ON FWD FUSELAGE SKIN AT FR 19 BETWEEN STGR 20L-21L. REF EMB ETD2021-170-020197. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. NO APPRECISDR C77A2020022270010Doubler · corrodedDURING THE B6 BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED IN THE FORWARD FUSELAGE AT THE RH COCKPIT FLOOR DOUBLER (P/N 170-03238-005) DURING INSPECTION IN THE AREA. THE DAMAGE EXCEEDED THE LIMITS PROVIDED IN THE SRM BECAUSE OF ITS DEPTH. EAMS REQUESTESDR C77A2019071900001Seat Track · damagedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON-CONDITION REPAIR OF CORROSION OR OTHER DAMAGE TO THE CENTER FUSELAGE III LT LATERAL SEAT TRACK P/N 170-65917-005 (-003). THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DIRECT REPLACEMENT OF THESDR C77A2019071800003Seat Track · corrodedDURING THE HEAVY CHECK OF THE AIRCRAFT, DAMAGE WAS DISCOVERED ON THE LT IB SEAT TRACK (P/N 170-03264-001) AT THE FR19 CROSSBEAM IN THE FORWARD CABIN FLOOR STRUCTURE. THE BEAM WILL BE REPAIRED BY CUTOUT AND DOUBLER INSTALLATION PER SRM PART II 53-10-10 REPAIR 0SDR C77A2019071800002Doubler · corrodedDURING THE B6 BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED IN THE FORWARD FUSELAGE AT THE RT COCKPIT FLOOR DOUBLER (P/N 170-03238-005) DURING INSPECTION IN THE AREA. THE DAMAGE EXCEEDED THE LIMITS PROVIDED IN THE SRM BECAUSE OF ITS DEPTH. EAMS REQUESTESDR C77A2020022270017Floorbeam · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE CENTER FUSELAGE III FLOOR STRUCTURE FRAME 86RH (P/N 170-86101-001) AND FLOOR SPLICE AT FRAME 90 (P/N 170-86119-005). REFERENCE ETD2019-170-092046 FIGURE 1 FOR DETAILS ON THE FRAME 86RH AND ETD2019-1SDR C77A2020022270016Floor Support · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE FORWARD FUSELAGE FRAME 16 FLOOR DOUBLER (P/N 170-12118-001) AND RH SILL BETWEEN FRAME 12 - 14 (P/N 170-05663-003). REFERENCE ETD2019-170-092106 FIGURE 1 FOR DETAILS ON THE FRAME 16 FLOOR DOUBLER ANDSDR C77A2020022270015Floor Support · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE FORWARD FUSELAGE FRAME 16 FLOOR DOUBLER (P/N 170-12118-001) AND RH SILL BETWEEN FRAME 12 - 14 (P/N 170-05663-003). REFERENCE ETD2019-170-092106 FIGURE 1 FOR DETAILS ON THE FRAME 16 FLOOR DOUBLER ANDSDR C77A2020022370025Support · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: P/N 170-86181-005 RH PANEL SUPPORT, P/N 170-86139-005 LH SILL PANEL FR 88-90, P/N 170-66796-001 LSDR C77A2020022370024Gusset · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: P/N 170-86181-005 RH PANEL SUPPORT, P/N 170-86139-005 LH SILL PANEL FR 88-90, P/N 170-66796-001 LSDR C77A2020022370023Gusset · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: P/N 170-86181-005 RH PANEL SUPPORT, P/N 170-86139-005 LH SILL PANEL FR 88-90, P/N 170-66796-001 LSDR C77A2020022270022Gusset · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: P/N 170-86181-005 RH PANEL SUPPORT, P/N 170-86139-005 LH SILL PANEL FR 88-90, P/N 170-66796-001 LSDR C77A2020022270020Panel · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: P/N 170-86181-005 RH PANEL SUPPORT, P/N 170-86139-005 LH SILL PANEL FR 88-90, P/N 170-66796-001 LSDR C77A2020022270019Floor Support · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: P/N 170-86181-005 RH PANEL SUPPORT, P/N 170-86139-005 LH SILL PANEL FR 88-90, P/N 170-66796-001 LSDR C77A2020022270018Floor Splice · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE CENTER FUSELAGE III FLOOR STRUCTURE FRAME 86RH (P/N 170-86101-001) AND FLOOR SPLICE AT FRAME 90 (P/N 170-86119-005). REFERENCE ETD2019-170-092046 FIGURE 1 FOR DETAILS ON THE FRAME 86RH AND ETD2019-1SDR C77A2020022270012Floor Support · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING FORWARD CABIN FLOOR STRUCTURE: P/N 170-07311-001 (-003) FLOOR DOUBLER, P/N 170-05661-003 (-005) RH SILL, P/N 170-04071-001 FSDR C77A2020022270021Shear Panel · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: P/N 170-86181-005 RH PANEL SUPPORT, P/N 170-86139-005 LH SILL PANEL FR 88-90, P/N 170-66796-001 LSDR C77A2019071500001Seat Track · damagedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON CONDITION REPLACEMENT OF A DAMAGED OR PREVIOUSLY REPAIRED RT FLOOR TRACK P/N 170-03263-001 BETWEEN FRAMES 12 AND 20 WITH A NEW P/N 170-03263-001 FLOOR TRACK. THE FLOOR TRACK WILL BE REPLACED SDR C77A2019071100001Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON CONDITION REPAIR OF CORROSION OR OTHER DAMAGE TO THE CENTER FUSELAGE I LT LATERAL SEAT TRACK P/N 170-92570-005 (-003). THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DIRECT REPLACEMENT OF THE ASDR C77A2020022270014Doubler · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING FORWARD CABIN FLOOR STRUCTURE: P/N 170-07311-001 (-003) FLOOR DOUBLER, P/N 170-05661-003 (-005) RH SILL, P/N 170-04071-001 FSDR C77A2020022270011Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE LH IB SEAT TRACK (P/N 170-03264-001) AT THE FR19 CROSSBEAM IN THE FORWARD CABIN FLOOR STRUCTURE. THE BEAM WILL BE SDR C77A20170725001Stringer · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CENTER FUSELAGE III STRINGER 29R, BY PART REPLACEMENT DUE TO CORROSION DAMAGE BEING DISCOVERED BETWEEN FR75-FR80 DURING THE AIRCRAFT’S BASIC CHECK. THERE ARE SEVERAL AREAS OSDR C77A20170721001Rib · crackedRIGHT HORIZONTAL STABILIZER HAS A CRACKED RIB 12A. REPAIRED IAW DRAWINGS, SRM 51.
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