# Service difficulty reports: N610CZ

A list on [N610CZ](https://openairdocs.org/aircraft/N610CZ.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 123 reports

- [SDR SWI2024F01278](https://openairdocs.org/sdr/SWI2024F01278.md): Stringer · corroded · Oct 10, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION - 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 SWIA2024F01083](https://openairdocs.org/sdr/SWIA2024F01083.md): Stringer · corroded · Oct 10, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION - 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 SWIA2024103010](https://openairdocs.org/sdr/SWIA2024103010.md): Stringer · corroded · Oct 10, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION - 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 SWIA20241115008](https://openairdocs.org/sdr/SWIA20241115008.md): Skin · cracked · Oct 8, 2024 · N610CZ · Emb ERJ170200LR · Wing, Plate/Skin
  > RH 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 ETD2024-170-027059
- [SDR SWIA2024103008](https://openairdocs.org/sdr/SWIA2024103008.md): Skin · cracked · Oct 8, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > RH 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 SWI2024F01259](https://openairdocs.org/sdr/SWI2024F01259.md): Seat Track · gouged · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 SWI2024F01258](https://openairdocs.org/sdr/SWI2024F01258.md): Seat Track · gouged · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 RE
- [SDR SWI2024F01257](https://openairdocs.org/sdr/SWI2024F01257.md): Seat Track · gouged · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 AND
- [SDR SWI2024F01256](https://openairdocs.org/sdr/SWI2024F01256.md): Crossbeam · corroded · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > MAIN 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 SWI2024F01255](https://openairdocs.org/sdr/SWI2024F01255.md): Crossbeam · corroded · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > MAIN 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 INSTALLE
- [SDR SWI2024F01254](https://openairdocs.org/sdr/SWI2024F01254.md): Seat Track · corroded · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 PER
- [SDR SWIA2024111500004](https://openairdocs.org/sdr/SWIA2024111500004.md): Seat Track · corroded · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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. PAR
- [SDR SWIA2024F01082](https://openairdocs.org/sdr/SWIA2024F01082.md): Seat Track · gouged · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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. S
- [SDR SWIA2024F01081](https://openairdocs.org/sdr/SWIA2024F01081.md): Seat Track · gouged · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 REPL
- [SDR SWIA2024F01080](https://openairdocs.org/sdr/SWIA2024F01080.md): Seat Track · gouged · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 B
- [SDR SWIA2024F01079](https://openairdocs.org/sdr/SWIA2024F01079.md): Floorbeam · corroded · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > MAIN 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.# S
- [SDR SWIA2024F01078](https://openairdocs.org/sdr/SWIA2024F01078.md): Floorbeam · corroded · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > MAIN 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 SWIA2024F01077](https://openairdocs.org/sdr/SWIA2024F01077.md): Seat Track · corroded · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 PERFO
- [SDR SWIA2024103004](https://openairdocs.org/sdr/SWIA2024103004.md): Seat Track · corroded · Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 SWIA202411150002](https://openairdocs.org/sdr/SWIA202411150002.md): Shear Tie · corroded · Oct 2, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR 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 NO
- [SDR SWIA2024103002](https://openairdocs.org/sdr/SWIA2024103002.md): Shear Tie · corroded · Oct 2, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR 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 C
- [SDR SWIA202411150001](https://openairdocs.org/sdr/SWIA202411150001.md): Bearing · no test · Oct 1, 2024 · N610CZ · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > HORIZONTAL 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 BACKL
- [SDR SWIA2024103001](https://openairdocs.org/sdr/SWIA2024103001.md): Bearing · failed · Oct 1, 2024 · N610CZ · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > HORIZONTAL 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 BACKLA
- [SDR SWI2024F01260](https://openairdocs.org/sdr/SWI2024F01260.md): Spar · cracked · Sep 30, 2024 · N610CZ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > SUSPECTED 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 SWIA202410301076](https://openairdocs.org/sdr/SWIA202410301076.md): Spar · cracked · Sep 30, 2024 · N610CZ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > SUSPECTED 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 SWIA20230205](https://openairdocs.org/sdr/SWIA20230205.md): Not Reported · failed · Feb 5, 2023 · N610CZ · Emb ERJ170200LR · Cylinder Head Temperature (CHT) Indicating System
  > BEFORE 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 AT
- [SDR SWIA2021082060611](https://openairdocs.org/sdr/SWIA2021082060611.md): Intercostal · corroded · Jun 27, 2021 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION 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 DONE
- [SDR SWIA2021082060610](https://openairdocs.org/sdr/SWIA2021082060610.md): Skin · dented · Jun 23, 2021 · N610CZ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FORWARD 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 APPRECI
- [SDR C77A2020022270010](https://openairdocs.org/sdr/C77A2020022270010.md): Doubler · corroded · Jul 22, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Floor Panel
  > DURING 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 REQUESTE
- [SDR C77A2019071900001](https://openairdocs.org/sdr/C77A2019071900001.md): Seat Track · damaged · Jul 20, 2019 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THIS 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 THE
- [SDR C77A2019071800003](https://openairdocs.org/sdr/C77A2019071800003.md): Seat Track · corroded · Jul 18, 2019 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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 0
- [SDR C77A2019071800002](https://openairdocs.org/sdr/C77A2019071800002.md): Doubler · corroded · Jul 18, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING 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 REQUESTE
- [SDR C77A2020022270017](https://openairdocs.org/sdr/C77A2020022270017.md): Floorbeam · corroded · Jul 17, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > DURING 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 ETD2019-1
- [SDR C77A2020022270016](https://openairdocs.org/sdr/C77A2020022270016.md): Floor Support · corroded · Jul 17, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING 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 AND
- [SDR C77A2020022270015](https://openairdocs.org/sdr/C77A2020022270015.md): Floor Support · corroded · Jul 17, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING 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 AND
- [SDR C77A2020022370025](https://openairdocs.org/sdr/C77A2020022370025.md): Support · corroded · Jul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS 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 L
- [SDR C77A2020022370024](https://openairdocs.org/sdr/C77A2020022370024.md): Gusset · corroded · Jul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS 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 L
- [SDR C77A2020022370023](https://openairdocs.org/sdr/C77A2020022370023.md): Gusset · corroded · Jul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS 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 L
- [SDR C77A2020022270022](https://openairdocs.org/sdr/C77A2020022270022.md): Gusset · corroded · Jul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS 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 L
- [SDR C77A2020022270020](https://openairdocs.org/sdr/C77A2020022270020.md): Panel · corroded · Jul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS 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 L
- [SDR C77A2020022270019](https://openairdocs.org/sdr/C77A2020022270019.md): Floor Support · corroded · Jul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS 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 L
- [SDR C77A2020022270018](https://openairdocs.org/sdr/C77A2020022270018.md): Floor Splice · corroded · Jul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING 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 ETD2019-1
- [SDR C77A2020022270012](https://openairdocs.org/sdr/C77A2020022270012.md): Floor Support · corroded · Jul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS 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 F
- [SDR C77A2020022270021](https://openairdocs.org/sdr/C77A2020022270021.md): Shear Panel · corroded · Jul 15, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS 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 L
- [SDR C77A2019071500001](https://openairdocs.org/sdr/C77A2019071500001.md): Seat Track · damaged · Jul 15, 2019 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THIS 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 C77A2019071100001](https://openairdocs.org/sdr/C77A2019071100001.md): Seat Track · corroded · Jul 11, 2019 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THIS 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 A
- [SDR C77A2020022270014](https://openairdocs.org/sdr/C77A2020022270014.md): Doubler · corroded · Jul 10, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS 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 F
- [SDR C77A2020022270011](https://openairdocs.org/sdr/C77A2020022270011.md): Seat Track · corroded · Jul 10, 2019 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THIS 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 C77A20170725001](https://openairdocs.org/sdr/C77A20170725001.md): Stringer · corroded · Jul 25, 2017 · N610CZ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > THIS 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 O
- [SDR C77A20170721001](https://openairdocs.org/sdr/C77A20170721001.md): Rib · cracked · Jul 21, 2017 · N610CZ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STABILIZER HAS A CRACKED RIB 12A. REPAIRED IAW DRAWINGS, SRM 51.

Next page: https://openairdocs.org/aircraft/N610CZ/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N610CZ/reports

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