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.

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.Oct 10, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Longeron/StringerSDR 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 Oct 10, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Longeron/StringerSDR 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.Oct 10, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Longeron/StringerSDR 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 ETD2024-170-027059Oct 8, 2024 · N610CZ · Emb ERJ170200LR · Wing, Plate/SkinSDR 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. Oct 8, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR 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.Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 REOct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 ANDOct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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.#Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, StructureSDR 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 INSTALLEOct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, StructureSDR 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 PEROct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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. PAROct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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. SOct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 REPLOct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 BOct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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.# SOct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR 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 Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR 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 PERFOOct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 Oct 4, 2024 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 NOOct 2, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR 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 COct 2, 2024 · N610CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR 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 BACKLOct 1, 2024 · N610CZ · Emb ERJ170200LR · Horizontal Stabilizer StructureSDR 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 BACKLAOct 1, 2024 · N610CZ · Emb ERJ170200LR · Horizontal Stabilizer StructureSDR 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.Sep 30, 2024 · N610CZ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/RibSDR 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.Sep 30, 2024 · N610CZ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/RibSDR 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 ATFeb 5, 2023 · N610CZ · Emb ERJ170200LR · Cylinder Head Temperature (CHT) Indicating SystemSDR 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 DONEJun 27, 2021 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 APPRECIJun 23, 2021 · N610CZ · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR 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 REQUESTEJul 22, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Floor PanelSDR 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 THEJul 20, 2019 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 0Jul 18, 2019 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 REQUESTEJul 18, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 ETD2019-1Jul 17, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR 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 ANDJul 17, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 ANDJul 17, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 LJul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 LJul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 LJul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 LJul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 LJul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 LJul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 ETD2019-1Jul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 FJul 16, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 LJul 15, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 Jul 15, 2019 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 AJul 11, 2019 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 FJul 10, 2019 · N610CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR 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 Jul 10, 2019 · N610CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR 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 OJul 25, 2017 · N610CZ · Emb ERJ170200LR · Fuselage Main, Longeron/StringerSDR C77A20170721001Rib · crackedRIGHT HORIZONTAL STABILIZER HAS A CRACKED RIB 12A. REPAIRED IAW DRAWINGS, SRM 51.Jul 21, 2017 · N610CZ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
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