N613CZ

Service difficulty reports · 139

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 = 'N613CZ' 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 SWI2024F00895Flap Track · wornLH 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.Sep 6, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR SWI2024F00894Flap Track · damagedLH 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.Sep 6, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR SWI2024F00893Lug · scoredHORIZONTAL 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 ASep 6, 2024 · N613CZ · Emb ERJ170200LR · Horizontal Stabilizer StructureSDR SWIA2024092706Lug · scoredHORIZONTAL AFT LH HINGE BEARING LUG HAS SCORING AND PITTING ON THE LUG BUSHING AND I/B FACE OF LUGSep 6, 2024 · N613CZ · Emb ERJ170200LR · Horizontal Stabilizer StructureSDR SWI2024F00892Shear Tie · corrodedSHEAR 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 NOTEDSep 4, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWI2024F00891Shear Tie · corrodedSHEAR 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.Sep 4, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWI2024F00890Shear Tie · corrodedSHEAR 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 NOTEDSep 4, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA2024092700004Shear Tie · corrodedSHEAR 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 NOTEDSep 4, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA2024092703Flap Track · damagedRH 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.Sep 3, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR SWI2024F00897Flap Track · wornLH 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 CARSep 1, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR SWI2024F00896Flap Track · wornLH 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 Sep 1, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR SWIA2024092701Flap Track · damagedRH 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.Sep 1, 2024 · N613CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR SWIA2024092700003Floorbeam · corrodedCOCK 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, DUEAug 29, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWI2024F00889Stringer · corrodedEVIDENCE 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 CHAAug 26, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Longeron/StringerSDR SWI2024F00888Stiffener · corrodedEVIDENCE 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 BAug 26, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA202409300001Frame · corrodedEVIDENCE 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 NOTEDAug 26, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, FrameSDR SWI2024F00887Service Panel · delaminatedINTERNAL 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 PERFORMEDAug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, StructureSDR SWI2024F00886Beam · corrodedL/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 CONAug 23, 2024 · N613CZ · Emb ERJ170200LR · Passenger/Crew DoorsSDR SWI2024F00885Door Frame · corrodedAFT 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 AAug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, StructureSDR SWI2024F00884Door Frame · corrodedLH 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 LAug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, StructureSDR SWI2024F00883Floor Support · corrodedAFT 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/REPAIR04PAug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWI2024F00882Seat Track · corrodedR/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 WAug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00881Floorbeam · corrodedAFT 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 BYAug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWIA20240823Shear Tie · corrodedSHEAR 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 NOTEDAug 23, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA202409270002Skin · dentedADM #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 Aug 21, 2024 · N613CZ · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA202266450Skin · dentedTRANSFER 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 CLOSEDSep 11, 2022 · N613CZ · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA202160619Intercostal · corrodedL/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, 51-23Jul 31, 2021 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2021082660624Seat Track · corrodedCORROSION 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 BALANCEJul 21, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021082660623Seat Track · corroded: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 ETDJul 20, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021082660622Seat Track · corrodedRH 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 REPLACEMENTJul 20, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021082660621Seat Track · chafedLH 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.Jul 20, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021082660620Seat Track · chafedCHAFFING 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 BALANCEJul 20, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021082660617Seat Track · chafedCHAFFING 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.Jul 20, 2021 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021082660618Skin · crackedLH 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 SURFJul 19, 2021 · N613CZ · Emb ERJ170200LR · Wing, Plate/SkinSDR C77A2019112500001Warning Message · activatedBRK LH FAULT AND BRK RH FAULT MSGS ON APPROACH AFTER GEAR EXTENSION, FOLLOWED QRH 13.12. MSGS REMAINED ACTIVE AT GATE.Nov 23, 2019 · N613CZ · Emb ERJ170200LR · Landing Gear Brake SystemSDR C77A2019112100001Fault Light · illuminatedBRAKE LH FAULT AND BRAKE RH FAULTNov 20, 2019 · N613CZ · Emb ERJ170200LR · Landing Gear Brake SystemSDR C77A2020011100008Crossbeam · damagedDURING 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 Sep 17, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Main, StructureSDR C77A2019091600001Floorbeam · damagedTHIS 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 DRAWISep 16, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR C77A2020011100010Gusset · corrodedCORROSION AR FR 11 COCKPIT FLORR CROSSBEAM CENTER GUSSETSep 14, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2020011100009Floor Support · crackedAFT WET AREA FLOOR PANEL SUPPORT HAS CRACK AT FR 86Sep 14, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2019091200006Seat 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 THESep 14, 2019 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR C77A2019091200005Seat 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 THESep 14, 2019 · N613CZ · Emb ERJ170100LR · Fuselage, Seat/Cargo Attach FittingsSDR C77A2019091200004Seat Track · corrodedTHIS 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 THESep 14, 2019 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR C77A2019091200003Seat Track · corrodedTHIS 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 THESep 14, 2019 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR C77A2019091200002Seat Track · corrodedCORROSION 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 Sep 14, 2019 · N613CZ · Emb ERJ170100LR · Fuselage, Seat/Cargo Attach FittingsSDR C77A2019091200001Seat Track · corrodedCORROSION 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 Sep 14, 2019 · N613CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR C77A2019091300004Beam · corrodedDURING 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 CSep 13, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Main, StructureSDR C77A2019091300007Doubler · corrodedDURING 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 DEEPESTSep 13, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR C77A2019091300006Doubler · corrodedDURING 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 RESep 13, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2019091300005Doubler · corrodedDURING 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 RESep 13, 2019 · N613CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
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