# Service difficulty reports: N613CZ

A list on [N613CZ](https://openairdocs.org/aircraft/N613CZ.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 · 139 reports

- [SDR SWI2024F00895](https://openairdocs.org/sdr/SWI2024F00895.md): Flap Track · worn · Sep 6, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > LH FLAP TRACK 3A O/B HAS WIDTH REDUCTION OF 0.043"- FLAPS DOWN. OUT OF LIMITS. ASSET # TC2- 7153 DUE: 11-15-24 (C-CHECK RO 9/26/2024) REMOVED AND REPLACED L/H #3 OUTBOARD AFT FLAP TRACK. REF AMM 57-57-35. TORQUE WRENCH ID#7543 CAL DUE 5-13-25.
- [SDR SWI2024F00894](https://openairdocs.org/sdr/SWI2024F00894.md): Flap Track · damaged · Sep 6, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > LH FLAP TRACK 1A HAS DAMAGE TO RADIUS IN SEVERAL PLACES. ASSET # TC2- 7153 DUE: 11-15-24. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED LH FLAP TRACK 1A. REF AMM 57-54-25. TORQUE WRENCH ID#602 CAL DUE 1-31-25.
- [SDR SWI2024F00893](https://openairdocs.org/sdr/SWI2024F00893.md): Lug · scored · Sep 6, 2024 · N613CZ · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > HORIZONTAL AFT RH HINGE BEARING LUG HAS SCORING AND PITTING ON THE LUG BUSHING AND O/B FACE OF LUG (C-CHECK RO 9/26/2024) REMOVED DAMAGE TO RH HINGE BEARING LUG/INBD FACE ON HORIZONTAL STAB BY REAMING AND SPOT FACING, REF E 175 SRM 55-10-02, 55-10-08 A
- [SDR SWIA2024092706](https://openairdocs.org/sdr/SWIA2024092706.md): Lug · scored · Sep 6, 2024 · N613CZ · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > HORIZONTAL AFT LH HINGE BEARING LUG HAS SCORING AND PITTING ON THE LUG BUSHING AND I/B FACE OF LUG
- [SDR SWI2024F00892](https://openairdocs.org/sdr/SWI2024F00892.md): Shear Tie · corroded · Sep 4, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP AT FR.84 BETWEEN STR27R-28R HAS EVIDENCE OF CORROSION. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED SHEAR CLIP AT FR. 84 BETWEEN SRT. 27R - 28R REF: SRM 51-40-08. SHEAR CLIP REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
- [SDR SWI2024F00891](https://openairdocs.org/sdr/SWI2024F00891.md): Shear Tie · corroded · Sep 4, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP AT FR.85 BETWEEN STR27R-28R HAS EVIDENCE OF CORROSION. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED SHEAR CLIP AT FR. 85 BETWEEN STR. 27R - 28R REF: SRM 51-40-08. SHEAR CLIP REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED.
- [SDR SWI2024F00890](https://openairdocs.org/sdr/SWI2024F00890.md): Shear Tie · corroded · Sep 4, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP AT FR.86 BETWEEN STR27R-28R HAS EVIDENCE OF CORROSION. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED SHEAR CLIP AT FR. 86 BETWEEN STR. 27R - 28R REF: SRM 51-40-08. SHEAR CLIP REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
- [SDR SWIA2024092700004](https://openairdocs.org/sdr/SWIA2024092700004.md): Shear Tie · corroded · Sep 4, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP AT FR.88 BETWEEN STR27R-28R HAS EVIDENCE OF CORROSION. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED SHEAR CLIP AT FR. 88 BETWEEN STR 27R - 28R REF: SRM 51-40-08. SHEAR CLIP REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
- [SDR SWIA2024092703](https://openairdocs.org/sdr/SWIA2024092703.md): Flap Track · damaged · Sep 3, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > RH FLAP TRACK 1A HAS DAMAGE IN LOWER INTERNAL RADIUS (NO DAMAGE ALLOWED AREA). (C-CHECK RO 9/26/2024) REMOVED AND REPLACED RH FLAP TRACK 1A. REF. E175 AMM 57-54-25. ASSET# TC1-602, CAL. DATE:1-31-25. SEE CONTINUE CARD FOR GAP CHECK.
- [SDR SWI2024F00897](https://openairdocs.org/sdr/SWI2024F00897.md): Flap Track · worn · Sep 1, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > LH FLAP TRACK 2A O/B HAS WIDTH REDUCTION OF 0.043" FLAPS UP- OUT OF LIMITS. ASSET # TC2- 7153 DUE: 11-15-24. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED LH FLAP TRACK 2A O/B. REF. E175 AMM 57-54-25. ASSET# TC2-7401, CAL. DATE: 5-13-25. SEE CONTINUE CAR
- [SDR SWI2024F00896](https://openairdocs.org/sdr/SWI2024F00896.md): Flap Track · worn · Sep 1, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > LH FLAP TRACK 2A I/B HAS THICKNESS REDUCTION OF 0.037" FLAPS UP. ASSET # TC2- 7153 DUE: 11-15-24. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED LH FLAP TRACK 2A I/B. REF. E175 AMM 57-54-25. ASSET# TC2-7401, CAL. DATE: 5-13-25. REMOVED AND REINSTALLED LH
- [SDR SWIA2024092701](https://openairdocs.org/sdr/SWIA2024092701.md): Flap Track · damaged · Sep 1, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > RH FLAP TRACK 2A O/B HAS WIDTH REDUCTION OF 0.043" AND DAMAGE TO RADIUS OF TRACK. OUT OF LIMITS. ASSET # TC2- 7153 DUE: 11-15-24.
- [SDR SWIA2024092700003](https://openairdocs.org/sdr/SWIA2024092700003.md): Floorbeam · corroded · Aug 29, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > COCK PIT FLOOR CROSSBEAM FR11 HAS CORROSION ON TOP FLANGE AT CENTERLINE AREA (C-CHECK RO 9/26/2024) PERFORMED PERMANENT DOUBLER REPAIR ON COCKPIT FLOOR FR 11 CROSSBEAM REF. ETD2024-170-023439. CHANGE IN WEIGHT 195.32 GRAMS CAL. TOOL I.D.# SH2-10286, DUE
- [SDR SWI2024F00889](https://openairdocs.org/sdr/SWI2024F00889.md): Stringer · corroded · Aug 26, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > EVIDENCE OF CORROSION LOCATED ON STRINGER 28R BETWEEN FR.86-87 AS MARKED. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED STRINGER 28R BETWEEN FR. 83 - FR. 90 REF: SRM 51-40-08. WEIGHT OF REPAIR PARTS IS 103.4 GRAMS I.D# SH2-5 DUE: 07/02/25 NO NOTICABLE CHA
- [SDR SWI2024F00888](https://openairdocs.org/sdr/SWI2024F00888.md): Stiffener · corroded · Aug 26, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION LOCATED ON STIFFENER BETWEEN FR.86-87 STR.27R AND 28R AS MARKED. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED STIFFENER BETWEEN FR. 86 - 87 STR. 27R - 28R REF: SRM 51-40-08. STIFFENER REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND B
- [SDR SWIA202409300001](https://openairdocs.org/sdr/SWIA202409300001.md): Frame · corroded · Aug 26, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Frame
  > EVIDENCE OF CORROSION LOCATED ON FR.87 BETWEEN STR.27R AND 28R AS MARKED. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED FR. 87 BETWEEN STR. 26R - 26L REF: SRM 51-40-08. FRAME WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
- [SDR SWI2024F00887](https://openairdocs.org/sdr/SWI2024F00887.md): Service Panel · delaminated · Aug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > INTERNAL SIDE OF WASTE SERVICE PANEL BOX HAS DELAMINATED/DETERIORATED COMPOSITE MATERIAL (C-CHECK RO 9/26/2024) REPAIRED WASTE BOX COMPOSITE DAMAGE AND REPAIRED COPPER FOIL MESH REF EMB SRM 53-23-60/REPAIR02P. SEE CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWI2024F00886](https://openairdocs.org/sdr/SWI2024F00886.md): Beam · corroded · Aug 23, 2024 · N613CZ · Emb ERJ170200LR · Passenger/Crew Doors
  > L/H FWD CABIN PAX DOOR INTERNAL LOWER BEAM HAS CORROSION. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED FWD CABIN PAX DOOR LOWER BEAM REF EMB SRM 51-40-08. FWD PAX DOOR LOWER BEAM WAS REPLACED WITH OEM PARTS, NO CHANGE IN WEIGHT AND BALANCE NOTED. SEE CON
- [SDR SWI2024F00885](https://openairdocs.org/sdr/SWI2024F00885.md): Door Frame · corroded · Aug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > AFT SERVICE DOOR FWD AND AFT FLOOR FITTING CUTOUTS HAVE CORROSON ON TOP EDGES AS MARKED (C-CHECK RO 9/26/2024) REMOVED AND REPLACED AFT SERVICE DOOR LOWER BEAM REF EMB SRM 51-40-08. AFT SERVICE DOOR BEAM WAS REPLACED WITH OEM PARTS NO CHANGE TO WEIGHT A
- [SDR SWI2024F00884](https://openairdocs.org/sdr/SWI2024F00884.md): Door Frame · corroded · Aug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > LH AFT PAX DOOR FWD AND AFT FLOOR FITTING CUTOUTS HAVE CORROSON ON TOP EDGES AS MARKED (C-CHECK RO 9/26/2024) REMOVED AND REPLACED LH AFT PAX DOOR LOWER BEAM WITH NEW REF. SRM 51-40-08. SEE CONTINUATION CARD FOR FURTHER WORK PERFORMED. LH AFT PAX DOOR L
- [SDR SWI2024F00883](https://openairdocs.org/sdr/SWI2024F00883.md): Floor Support · corroded · Aug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA CORROSION AROUND RIVET HEADS ON RH FLOOR BEAM UPPER SHEET BETWEEN FRAMES 84/85 AS MARKED (C-CHECK RO 9/26/2024) INSTALLED DOUBLER/FILLER REPAIR ON RH FLOOR SEAT TRACK AT FR 84/85 REF SRM 53-23-10/REPAIR04P
- [SDR SWI2024F00882](https://openairdocs.org/sdr/SWI2024F00882.md): Seat Track · corroded · Aug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > R/H FWD CABIN FLOOR. TRACK RIGHT FOUND CORROSION MULTIPLES SPOTS. (C-CHECK RO 9/26/2024) PERFORMED DOUBLER AND FILLER REPAIR ON RH FWD CABIN FLOOR TRACK BY FR 13-14 REF EMB SRM 53-10-10/ REPAIR 01P. DOUBLER AND FILLER WEIGHT 111G. NO ADVERSE CHANGE IN W
- [SDR SWI2024F00881](https://openairdocs.org/sdr/SWI2024F00881.md): Floorbeam · corroded · Aug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > AFT WET AREA LH FLOOR BEAM HAS CORROSION/SCRATCH BETWEEN FRAME 87 AND 89 AS MARKED (C-CHECK RO 9/26/2024) REMOVED AND REPLACED AFT WET AREA LH FLOOR BEAM FR 87-89 REF SRM 51-40-08. BEAM WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED BY
- [SDR SWIA20240823](https://openairdocs.org/sdr/SWIA20240823.md): Shear Tie · corroded · Aug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP AT FR.87 BETWEEN STR27R-28R HAS EVIDENCE OF CORROSION. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED SHEAR CLIP FR. 87 BETWEEN STR 27R - 28R REF: SRM 51-40-08 SHEAR CLIP WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
- [SDR SWIA202409270002](https://openairdocs.org/sdr/SWIA202409270002.md): Skin · dented · Aug 21, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > ADM #N613CZ-7545 - REAR FUSELAGE BETWEEN FR 98 - 99 AND BETWEEN STRINGER 23L - 25L. DENT MEASURING L=.530" X W =.530" X H.004 W/H = 132. PLEASE EVALUATE DENT AND RECONTOUR TO ORIGINAL FORM. (C-CHECK RO 9/26/2024) AFTER FURTHER EVALUATION ON REAR
- [SDR SWIA202266450](https://openairdocs.org/sdr/SWIA202266450.md): Skin · dented · Sep 11, 2022 · N613CZ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 990088: RAMP CREW INFORMED MAINTENANCE,THEY FOUND A DENT ON FUSELAGE NOSE SECTION LEFT SIDE ABOUT 1 INCH, SHOWN TO MAINTENANCE TEAM. DENT HAS BEEN DETERMINED TO BE A MAJOR REPAIR PER GMM 3-26. FORM M-337 WILL BE REQUIRED. (FILED CLOSED
- [SDR SWIA202160619](https://openairdocs.org/sdr/SWIA202160619.md): Intercostal · corroded · Jul 31, 2021 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > L/H O/B INTERCOSTAL AT FR 84 - FR 85 HAS CORROSION AS MARKED. (C-CHECK RO 8/23/21) / REMOVED AND REPLACED LH OB INTERCOSTAL FR 84-85 REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION AT LH OB INTERCOSTAL FR 84-85 REF EMB SRM 51-23-04, 51-23-05, 51-23
- [SDR SWIA2021082660624](https://openairdocs.org/sdr/SWIA2021082660624.md): Seat Track · corroded · Jul 21, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN L/H O/B SEAT TRACK AT FR.23. (C-CHECK RO 8-23-21) REMOVED AND REPLACED LH O/B SEAT TRACK AT FRAME 23. REF SRM 51-40-08 FACTORY REPLACEMENT SEAT TRACK NO CHANGE IN WEIGHT AND BALANCE
- [SDR SWIA2021082660623](https://openairdocs.org/sdr/SWIA2021082660623.md): Seat Track · corroded · Jul 20, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > :LH FIRST CLASS SEAT TRACK HAS CORROSION IN SEVERAL SPOTS AS MARKED FR 23-30 (C-CHECK RO 8-23-21) / PERFORMED SEAT TRACK SPLICE REPAIR ON LH FIRST CLASS SEAT TRACK CORROSION IN SEVERAL SPOTS FROM FR 23-30 REPLACED FWD SECTION FROM FR 23 TO FR 30 REF ETD
- [SDR SWIA2021082660622](https://openairdocs.org/sdr/SWIA2021082660622.md): Seat Track · corroded · Jul 20, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR BEAM SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION AS MARKED FR 23-34 (C-CHECK RO 8/23/21) / REMOVED AND REPLACED RH FLOOR BEAM SEAT TRACK FR 23-34 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 PART REPLACEED WITH FACTORE REPLACEMENT
- [SDR SWIA2021082660621](https://openairdocs.org/sdr/SWIA2021082660621.md): Seat Track · chafed · Jul 20, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR BEAM SEAT TRACK HAS 5 SPOTS OF CORROSION AS MARKED FR 30 - 34. (C-CHECK RO 8-23-21) / REMOVED AND REPLACED LH FLOOR BEAM SEAT TRACK 21-34 IN REF.TO EMB 175 SRM 51-40-08 SEE CONTIUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2021082660620](https://openairdocs.org/sdr/SWIA2021082660620.md): Seat Track · chafed · Jul 20, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CHAFFING ON LH OTBD SEAT TRACK IN 5 SPOTS FR 23-33 AS MARKED. (C-CHECK RO 8-23-21) / REMOVED AND REPLACED LH OB SEAT TRACK FR 23-33 REF EMB SRM 51-40-08 FACTORY REPLACEMENT PART NO CHANGE TO THE WEIGHT AND BALANCE
- [SDR SWIA2021082660617](https://openairdocs.org/sdr/SWIA2021082660617.md): Seat Track · chafed · Jul 20, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CHAFFING ON RH OTBD SEAT TRACK IN 9 SPOTS FR 23-34 AS MARKED. (C-CHECK RO 8-23-21) / REMOVED AND REPLACED RH OTBD SEAT TRACK FR 23-34 WITH FACTORY PART NO CHANGE TO WEIGHT AND BALANCE REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2021082660618](https://openairdocs.org/sdr/SWIA2021082660618.md): Skin · cracked · Jul 19, 2021 · N613CZ · Emb ERJ170200LR · Wing, Plate/Skin
  > LH WING FIXED LEADING EDGE SKIN EDGE HAS SUSPECTED CRACK AS MARKED AT THE SLAT 2 OTBD TRACK CUTOUT. (C-CHECK RO 8-23-21) CUT OUT LH WING FIXED LEADING EDGE SKIN EDGE CRACK AS MARKED AT THE SLAT 2 OTBD TRACK CUTOUT.REF SRM 57-49-01/REPAIR 06P. RESTORED SURF
- [SDR C77A2019112500001](https://openairdocs.org/sdr/C77A2019112500001.md): Warning Message · activated · Nov 23, 2019 · N613CZ · Emb ERJ170200LR · Landing Gear Brake System
  > BRK LH FAULT AND BRK RH FAULT MSGS ON APPROACH AFTER GEAR EXTENSION, FOLLOWED QRH 13.12. MSGS REMAINED ACTIVE AT GATE.
- [SDR C77A2019112100001](https://openairdocs.org/sdr/C77A2019112100001.md): Fault Light · illuminated · Nov 20, 2019 · N613CZ · Emb ERJ170200LR · Landing Gear Brake System
  > BRAKE LH FAULT AND BRAKE RH FAULT
- [SDR C77A2020011100008](https://openairdocs.org/sdr/C77A2020011100008.md): Crossbeam · damaged · Sep 17, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE FORWARD FUSELAGE FR11 COCKPIT CROSSBEAM. REFERENCE ETD2019-170-122405-A, FIGURE 1 FOR DETAILS. EAMS REQUESTED AND RECEIVED PERMANENT REPAIRS FOR THE DAMAGE IN THE FORM OF ETD2019-170-122405-A WHICH
- [SDR C77A2019091600001](https://openairdocs.org/sdr/C77A2019091600001.md): Floorbeam · damaged · Sep 16, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON CONDITION REPLACEMENT OF A DAMAGED OR PREVIOUSLY REPAIRED LT FLOOR BEAM P/N 170-65669-003 (Y = -273) BETWEEN FRAMES 86 AND 89. THE DAMAGED STRUCTURE WILL BE REPLACED BY USING PRODUCTION DRAWI
- [SDR C77A2020011100010](https://openairdocs.org/sdr/C77A2020011100010.md): Gusset · corroded · Sep 14, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION AR FR 11 COCKPIT FLORR CROSSBEAM CENTER GUSSET
- [SDR C77A2020011100009](https://openairdocs.org/sdr/C77A2020011100009.md): Floor Support · cracked · Sep 14, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR PANEL SUPPORT HAS CRACK AT FR 86
- [SDR C77A2019091200006](https://openairdocs.org/sdr/C77A2019091200006.md): Seat Track · damaged · Sep 14, 2019 · N613CZ · 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 C77A2019091200005](https://openairdocs.org/sdr/C77A2019091200005.md): Seat Track · damaged · Sep 14, 2019 · N613CZ · Emb ERJ170100LR · 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 C77A2019091200004](https://openairdocs.org/sdr/C77A2019091200004.md): Seat Track · corroded · Sep 14, 2019 · N613CZ · 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 RT LATERAL SEAT TRACK P/N 170-65917-006 (-004). THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DIRECT REPLACEMENT OF THE
- [SDR C77A2019091200003](https://openairdocs.org/sdr/C77A2019091200003.md): Seat Track · corroded · Sep 14, 2019 · N613CZ · 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 RT INBOARD SEAT TRACK P/N 170-86082-005 (-003). THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DIRECT REPLACEMENT OF THE
- [SDR C77A2019091200002](https://openairdocs.org/sdr/C77A2019091200002.md): Seat Track · corroded · Sep 14, 2019 · N613CZ · Emb ERJ170100LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION HAS BEEN FOUND ON THE CABIN RT SEAT TRACK P/N 170-02056-008 DURING BASIC CHECK. SINCE MANUFACTURER CLASSIFIES THIS SEAT TRACK AS PSE, HAS CLASSIFIED REPLACEMENT OF THIS TRACK AS A MAJOR REPAIR. IN LIEU OF CONTINUING TO WRITE INDIVIDUAL EO’S FOR EACH
- [SDR C77A2019091200001](https://openairdocs.org/sdr/C77A2019091200001.md): Seat Track · corroded · Sep 14, 2019 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION HAS BEEN FOUND ON THE LT CABIN SEAT TRACK P/N 170-02056-007 DURING BASIC CHECK. SINCE MANUFACTURER CLASSIFIES THIS SEAT TRACK AS PSE, HAS CLASSIFIED REPLACEMENT OF THIS TRACK AS A MAJOR REPAIR. IN LIEU OF CONTINUING TO WRITE INDIVIDUAL EO’S FOR EACH
- [SDR C77A2019091300004](https://openairdocs.org/sdr/C77A2019091300004.md): Beam · corroded · Sep 13, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > DURING THE CURRENT B6 BASIC CHECK, CORROSION DAMAGE WAS DISCOVERED ON THE AFT PASSENGER (L2) DOOR LOWER THRESHOLD BEAM (P/N 170-65703-005) AT FASTENER HOLES AROUND THE AFT GIRT BAR FITTING DURING ACCOMPLISHMENT OF EO E175-5300-221.2 FOR A MODIFICATION OF THE C
- [SDR C77A2019091300007](https://openairdocs.org/sdr/C77A2019091300007.md): Doubler · corroded · Sep 13, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING BASIC CHECK, CORROSION DAMAGE WAS DISCOVERED DURING INSPECTION ON THE CENTER FUSELAGE III WASTE BOX SKIN DOUBLER, P/N 170-66931-001, ALONG THE INNER EDGES OF THE DOUBLER (REFERENCE PHOTO 1 FOR DETAILS). THE CORROSION DAMAGE WAS BLENDED WITH THE DEEPEST
- [SDR C77A2019091300006](https://openairdocs.org/sdr/C77A2019091300006.md): Doubler · corroded · Sep 13, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING THE B6 BASIC CHECK, 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 REQUESTED AND RE
- [SDR C77A2019091300005](https://openairdocs.org/sdr/C77A2019091300005.md): Doubler · corroded · Sep 13, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING THE B6 BASIC CHECK, 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 REQUESTED AND RE

Next page: https://openairdocs.org/aircraft/N613CZ/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 = 'N613CZ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N613CZ/reports

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