# Service difficulty reports: N607CZ

A list on [N607CZ](https://openairdocs.org/aircraft/N607CZ.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 · 147 reports

- [SDR SWIA2026011300006](https://openairdocs.org/sdr/SWIA2026011300006.md): Warning Message · false activation · Jan 6, 2026 · N607CZ · Emb ERJ170200LR · Airfoil Anti/De-ice System
  > IN ICING CONDITION RECIEVED ANTI ICE WING FAIL CAUTION. RAN QRH AND MESSAGE PERSISTED. (FLIGHT 3792) ARRIVED AT ACFT WITH NO CURRENT FAULT. INTERROGATED CMC & FOUND NO ASSOCIATED FAULT CODE WITH ANTI-ICE WING FAIL MESSAGE. TROUBLESHOT ANTI-ICE FAIL CAUTION
- [SDR SWI2026F00045](https://openairdocs.org/sdr/SWI2026F00045.md): Anti-Ice System · warning message · Jan 6, 2026 · N607CZ · Emb ERJ170200LR · Ice/Rain Protection System
  > IN ICING CONDITION RECIEVED ANTI ICE WING FAIL CAUTION. RAN QRH AND MESSAGE PERSISTED. (FLIGHT 3792) OPEN
- [SDR SWIA20250707611](https://openairdocs.org/sdr/SWIA20250707611.md): Beam · corroded · Jun 11, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > FORWARD CARGO DOOR CUTOUT LOWER BEAM HAS CORROSION DAMAGE UNDER FORWARD MOST LATCH FITTING AND AT UPPER EDGE ABOVE THE 2 CENTER LATCH FITTINGS. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT LOWER BEAM, REF SRM 51-40-08. REPLACED WITH N
- [SDR SWI2025F00858](https://openairdocs.org/sdr/SWI2025F00858.md): Doubler · corroded · Jun 8, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > RH COCKPIT FLOOR DOUBLER HAS CORROSION AROUND RIVETS INBOARD AND OUTBOARD OF THE CO-PILOT CONTROL YOKES BETWEEN FRAMES 8-9 AND AFT OF THE CO-PILOT INBOARD SEAT TRACK BETWEEN FR11-12. (C-CHECK RO 07/03/2025)PERFORMED RH COCKPIT FLOOR DOUBLER REPAIR. REF EMB SR
- [SDR SWI2025F00857](https://openairdocs.org/sdr/SWI2025F00857.md): Control Column · corroded · Jun 8, 2025 · N607CZ · Emb ERJ170200LR · Control Column Section
  > LH COCKPIT FLOOR DOUBLER HAS CORROSION AROUND RIVETS INBOARD AND OUTBOARD OF THE PILOT CONTROL YOKE, BETWEEN FRAMES 8 AND 9. (C-CHECK RO 07/03/2025)PERFORMED COCKPIT DOUBLER REPAIR REF SRM 53-10-10/REPAIR 07P. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWI2025F00856](https://openairdocs.org/sdr/SWI2025F00856.md): Floor Support · corroded · Jun 8, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT CARGO FR 77 BETWEEN STGR 29L AND 29R L/H FLOOR SUPPORT CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FR 77 BETWEEN STGR 29L AND 29R L/H FLOOR SUPPORT. REF. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFORMED.
- [SDR SWIA20250707608](https://openairdocs.org/sdr/SWIA20250707608.md): Skin · corroded · Jun 8, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > REAR FUSELAGE FR 90 TO FR 91 STGR 29L TO STGR 29R SKIN CORRODED IN FRONT OF REAR SPLICE
- [SDR SWI2025F00864](https://openairdocs.org/sdr/SWI2025F00864.md): Floor Support · corroded · Jun 7, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT CARGO FR 81 STGR 29R AND STGR 29L L/H FLOOR SUPPORT CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FR 81 STGR 29R AND STGR 29L L/H FLOOR SUPPORT. REF. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFORMED.REPLACED WITH FACTORY REPLACEMENT PA
- [SDR SWI2025F00863](https://openairdocs.org/sdr/SWI2025F00863.md): Skin · cracked · Jun 7, 2025 · N607CZ · Emb ERJ170200LR · Wing, Plate/Skin
  > SUSPECTED CRACK LH WING LOWER SKIN AT WHEEL WELL CUTOUT RIB 3 (C-CHECK RO 07/03/2025)REMOVED CRACK ON LH WING LOWER SKIN BY CUTTING AWAY DAMAGED AREA. FABRICATED, DRILLED AND INSTALL FILLER/DOUBLER/TRIPLER REPAIR ON LOWER SKIN. REF: ETD2025-170-922726 REV: A
- [SDR SWI2025F00862](https://openairdocs.org/sdr/SWI2025F00862.md): Shear Tie · corroded · Jun 7, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > FWD CARGO HAS 1EA CORRODED SHEAR CLIP AT FR 22, STGR 27R-26R. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED SHEAR CLIP AT FR 22, STGR 27R-26R. REF. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFORMED. SHEAR CLIP REPLACED WITH OEM PART, NO CHANGE IN WE
- [SDR SWI2025F00861](https://openairdocs.org/sdr/SWI2025F00861.md): Support · corroded · Jun 7, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > REAR FUSELAGE BETWEEN FR 86 AND FR 87 STGR 27R AND 29R HEATED DRAIN MAST FWD SUPPORT CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FR 86 AND FR 87 STGR 27R AND 29R HEATED DRAIN MAST FWD SUPPORT. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERF
- [SDR SWI2025F00860](https://openairdocs.org/sdr/SWI2025F00860.md): Shear Tie · corroded · Jun 7, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > REAR FUSELAGE FR 87 STRG 28R TO STGR 29R SHEAR CLIP CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACE REAR FUSELAGE FR 87 STRG 28R TO STGR 29R SHEAR CLIP. REF SRM 51-40-08. (SEE CONTINUE CARD FOR ALL ACCOMPLISHED). REPLACED WITH OEM PART. NO CHANGE IN WIEG
- [SDR SWI2025F00859](https://openairdocs.org/sdr/SWI2025F00859.md): Floor Support · corroded · Jun 7, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT CARGO FR 82 STGR 29R AND STGR 29L R/H FLOOR SUPPORT CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FR 82 STGR 29R AND STGR 29L R/H FLOOR SUPPORT. REF. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFORMED.REPAIRED WITH FACTORY REPLACEMENT PA
- [SDR SWIA20250707607](https://openairdocs.org/sdr/SWIA20250707607.md): Floor Support · corroded · Jun 7, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT CARGO FR 82 STGR 29R AND STGR 29L L/H FLOOR SUPPORT CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FR 82 STGR 29R AND STGR 29L L/H FLOOR SUPPORT. REF. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFORMED. REPAIRED WITH FACTORY REPLACEMENT P
- [SDR SWI2025F00869](https://openairdocs.org/sdr/SWI2025F00869.md): Flap Track · worn · Jun 5, 2025 · N607CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > RH WING FLAP TRACK 2A I/B HAS THICKNESS REDUCTION WEAR OF 1.2MM MAX ALONG AFT SIDE AND IS OUT OF LIMITS. ASSET# TC2-10390, DUE 7-3-25. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED RH WING FLAP TRACK 2A I/B. REF AMM:57-54-25 T. WRENCH:TC2-7219 C/D:3-12-26
- [SDR SWIA20250707605](https://openairdocs.org/sdr/SWIA20250707605.md): Flap Track · gouged · Jun 5, 2025 · N607CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > LH WING FLAP TRACK 1A HAS MULTIPLE GOUGING IN RADIUS OF TRACK AND IS OUT OF LIMITS. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED LH WING FLAP TRACK 1A. REF AMM:57-54-25 T. WRENCH:TC2-7219 C/D:3-12-26
- [SDR SWI2025F00868](https://openairdocs.org/sdr/SWI2025F00868.md): Beam · corroded · Jun 4, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > FWD CARGO DOOR CUTOUT, LOWER HORIZONTAL BEAM HAS 2EA SPOTS OF CORROSION FROM FR 24-27 AS MARKED. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT LOWER BEAM FORWARD AND AFT FINGER DOUBLERS, REF SRM 51-40-08. REPLACED WITH NEW OEM PART. NO
- [SDR SWI2025F00867](https://openairdocs.org/sdr/SWI2025F00867.md): Seat Track · corroded · Jun 4, 2025 · N607CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH SEAT TRACK CORRODED 5.0€? AFT OF FRAME 13 AND RBL +11.75€?. (C-CHECK RO 07/03/2025)CUT OUT DADMAGED SECTION OF R/H I/B SEAT TRACK UPPER CAP BETWEEN FR13-14, INSTALLED DOUBLER, REINFORCEMENT ANGLE, AND FLOOR REINFORCEMENT BRACKET ON R/H I/B SEAT TRACK BET
- [SDR SWI2025F00866](https://openairdocs.org/sdr/SWI2025F00866.md): Floorbeam · corroded · Jun 4, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > RH AFT WET AREA BEAM HAS CORROSION AROUND NUTPLATE HOLE CLOSET TO FRAME 87 (C-CHECK RO 07/03/2025)REMOVED AND REPLACED RH AFT WET AREA BEAM BETWEEN FR87-89 REF. EMB SRM 51-40-08. REPLACED WITH OEM PARTS, DOES NOT AFFECT WEGHT AND BALANCE.
- [SDR SWI2025F00865](https://openairdocs.org/sdr/SWI2025F00865.md): Shear Tie · corroded · Jun 4, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > FWD CARGO HAS 1EA CORRODED SHEAR CLIP AT FR 21, STGR 27R-26R. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FWD CARGO HAS 1 SHEAR CLIP AT FR 21, STGR 27R-26R. REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED. SEE CONTINUED
- [SDR SWIA20250707604](https://openairdocs.org/sdr/SWIA20250707604.md): Shear Tie · corroded · Jun 4, 2025 · N607CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > FWD CARGO HAS 1EA CORRODED SHEAR CLIP AT FR 22, STGR 28R-27R. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FWD CARGO HAS SHEAR CLIP AT FR 22, STGR 28R-27R. REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED. SEE CONTINUATIO
- [SDR SWIA202507070602](https://openairdocs.org/sdr/SWIA202507070602.md): Skin · cracked · Jun 2, 2025 · N607CZ · Emb ERJ170200LR · Wing, Plate/Skin
  > R/H WING LOWER SKIN BETWEEN RIB 5 AND RIB 6 AT SPAT 2 HAS A SUSPECTED CRACK (C-CHECK RO 07/03/2025)REPAIRED R/H WING LOWER SKIN BETWEEN RIB 5-6 AT SPAR 2 BY APPLYING REPAIR EXTERNAL DOUBLER.SEE CONTINUATION CARD FOR WORK PERFORMED. REF ETD2025-170-922499
- [SDR SWIA202266438](https://openairdocs.org/sdr/SWIA202266438.md): None · scored · Aug 2, 2022 · N607CZ · Emb EMB110* · Horizontal Stabilizer Miscellaneous Structure
  > L/H HORIZONTAL STABILIZER HINGE LUG BORE IS SCORED. (C-CHECK RO 9/02/2022) REPAIRED LEFT HAND HORIZONTAL HINGE LUG BORE. REF SRM 55-10-02/REPAIR 01P. SEE CP 25221830 FOR FABRICATION AND INSALLATION OF BUSHINGS.
- [SDR SWIA202266437](https://openairdocs.org/sdr/SWIA202266437.md): None · scored · Aug 2, 2022 · N607CZ · Emb EMB110* · Horizontal Stabilizer, Attach Fittings
  > L/H AFT HORIZONTAL STABILIZER HINGE FITTING IS SCORED ON THE INBOARD SIDE AS MARKED. (C-CHECK RO 9/02/2022) REPAIRED L/F AFT HORIZONTAL STABILIZER HINGE FITTING ON THE INBOARD SIDE. RED ETD2022-170-025386. SEE CONTINUATION CARD FOR WORK PERFORMED. NO
- [SDR SWIA202266436](https://openairdocs.org/sdr/SWIA202266436.md): None · gouged · Jul 28, 2022 · N607CZ · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > LH OB LATERAL SEAT TRACK HAS GOUGES/CORRODED AS MARKED BETWEEN FRAMES 34-60 (C-CHECK RO 9/02/2022) / REMOVED AND REPLACED LH OB SEAT TRACK AT FR 34-60. REF E MB SRM 51-40-08. OEM PART REPLACEMENT, NO CHANGE IN WEIGHT.
- [SDR SWIA202266435](https://openairdocs.org/sdr/SWIA202266435.md): None · corroded · Jul 28, 2022 · N607CZ · Emb EMB110* · Fuselage Structure (General)
  > CORROSION ON AND AROUND DOME NUTS FOR FWD WI-FI ANTENNA BETWEEN FRAMES 21 AND 22 AND STRINGERS 27R AND 28R INSIDE FORWARD CARGO (C-CHECK RO 9/02/2022) REMOVED AND REPLACED DOUBLER AND 2 EA STIFFENERS BETWEEN FRAMES 21 AND 22 AND STRINGERS 27R AND 28R IN
- [SDR SWIA202266434](https://openairdocs.org/sdr/SWIA202266434.md): None · damaged · Jul 27, 2022 · N607CZ · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > RH IB SEAT TRACK SECTION FROM FR 23-34 IS DAMAGED. SEE THE CONTINUATION IN CAMP FOR LOCATIONS. (C-CHECK RO 9/02/2022) REMOVED AND REPLACED RH IB SEAT TRACK SECTION FROM FR 23-34 REF EMB SRM 51-40-08. REPLACD WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE
- [SDR SWIA202266433](https://openairdocs.org/sdr/SWIA202266433.md): None · damaged · Jul 27, 2022 · N607CZ · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > RH OB SEAT TRACK SECTION FROM FR 23-34 IS DAMAGED. SEE THE CONTINUATION IN CAMP FOR LOCATIONS. (C-CHECK RO 9/02/2022) REMOVED AND REPLACED RH OB SEAT TRACK AT FR 23-34. REF EMB SRM 51-40-08
- [SDR SWIA202266432](https://openairdocs.org/sdr/SWIA202266432.md): None · damaged · Jul 27, 2022 · N607CZ · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > RH OB SEAT TRACK SECTION FROM FR 21-23 IS DAMAGED. SEE THE CONTINUATION IN CAMP FOR LOCATIONS. (C-CHECK RO 9/02/2022) REMOVED AND REPLACED RH OB SEAT TRACK SECTION FROM FR 21-23 REF EMB SRM 51-40-08
- [SDR SWIA202266431](https://openairdocs.org/sdr/SWIA202266431.md): None · damaged · Jul 27, 2022 · N607CZ · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > LH OB SEAT TRACK SECTION FROM FR 19-21 IS DAMAGED. SEE THE CONTINUATION IN CAMP FOR LOCATIONS. (C-CHECK RO 9/02/2022) REMOVED AND REPLACED LH OB SEAT TRACK SECTION FROM FR 19-21 REF SRM 51-40-08. RESSTORED SURFACE PROTECTION REF SRM 51-23-06. WORK DONE
- [SDR SWIA202266430](https://openairdocs.org/sdr/SWIA202266430.md): None · gouged · Jul 27, 2022 · N607CZ · Emb EMB110* · Electrical/Electronic Compartment Doors
  > FWD AVIONICS HATCH SKIN IS GOUGED WITH A DENT (C-CHECK RO 9/02/2022) REPAIRED FWD AVIONICS HATCH REF ETD 2022-170-025288. REINSPECTION REQUIREMENTS- EXTERNAL AND INTERNAL, DET, THRESHOLD OF 7500 FC, INTERVAL OF 7500 FC. THIS IS AN ADDITIONAL AND SPECIF
- [SDR SWIA202266429](https://openairdocs.org/sdr/SWIA202266429.md): None · dented · Jul 25, 2022 · N607CZ · Emb EMB110* · Fuselage Structure (General)
  > DENT MEASURING 1.625" W AND.025" D LOCATED 3.5" ABOVE STGR 18L AND.5" AFT OF FR 10. EVALUATE AND REPAIR OR ELIMINATE EVIDENCE USING STANDARD PRACTICES. SEE ADM# N607CZ-6931 (C-CHECK RO 9/02/2022) PERFROMED A PERMANENT REPAIR BY REMOVING AND REPLACING
- [SDR C77A2020011300001](https://openairdocs.org/sdr/C77A2020011300001.md): Warning Message · illuminated · Jan 10, 2020 · N607CZ · Emb ERJ190100LR · Trailing Edge Flap Control System
  > FLAP FAIL MSG ON CLIMBOUT RETRACTION. FLAPS AT 0.
- [SDR C77A2019112600001](https://openairdocs.org/sdr/C77A2019112600001.md): Battery · inoperative · Nov 26, 2019 · N607CZ · Emb ERJ170200LR · Emergency Equipment
  > FO FLASHLIGHT INOP, AND IS MISSING INSP PLACARD. REPLACED FO FLASHLIGHT PLACARD IAW GMM 12-1-6. REPLACED FO FLASHLIGHT BATTERY IAW 33-51-01 A/C OK FOR SERVICE
- [SDR C77A2020031300036](https://openairdocs.org/sdr/C77A2020031300036.md): Door Sill · corroded · May 8, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > E175-5300-237-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 170-05663-003 RH FLOOR SILL, P/N 170-04071-001 FR15 FLOOR SUPPORT, P/N 170-
- [SDR C77A2020031200035](https://openairdocs.org/sdr/C77A2020031200035.md): Shear Tie · corroded · May 8, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON SEVERAL SHEAR CLIPS IN THE LOWER AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF THE CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING A
- [SDR C77A2020031200034](https://openairdocs.org/sdr/C77A2020031200034.md): Shear Tie · corroded · May 8, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON SEVERAL SHEAR CLIPS IN THE LOWER AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF THE CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING A
- [SDR C77A2020031200033](https://openairdocs.org/sdr/C77A2020031200033.md): Shear Tie · corroded · May 8, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON SEVERAL SHEAR CLIPS IN THE LOWER AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF THE CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING A
- [SDR C77A2020031200032](https://openairdocs.org/sdr/C77A2020031200032.md): Shear Tie · corroded · May 8, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON SEVERAL SHEAR CLIPS IN THE LOWER AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF THE CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING A
- [SDR C77A2020031200031](https://openairdocs.org/sdr/C77A2020031200031.md): Shear Tie · corroded · May 8, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON SEVERAL SHEAR CLIPS IN THE LOWER AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF THE CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING A
- [SDR C77A2019050800002](https://openairdocs.org/sdr/C77A2019050800002.md): Beam · corroded · May 8, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE CORROSION WAS FOUND ON BEAM (P/N 170-66280-001) AT S-28R BETWEEN FRAME 80 (X = 21192) AND FRAME 81 (X = 21617). THE CORROSION WAS BLENDED OUT RESULTING IN TWO BLEND OUTS. THE FIRST BLEND OUT IS 2.9" L X 1.0" W, X.05" D AND THE SECON
- [SDR C77A2019050800001](https://openairdocs.org/sdr/C77A2019050800001.md): Frame · corroded · May 8, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE CORROSION WAS FOUND ON FRAME 80 (P/N 170-65422-003) AT S-28R. THE CORROSION WAS BLENDED OUT WITH A MAXIMUM DEPTH OF.066" FROM A NOMINAL THICKNESS OF.118" WHICH IS OUT OF LIMITS. THE CORRODED FRAME WAS REMOVED AND REPLACED WITH A NE
- [SDR C77A2019050600004](https://openairdocs.org/sdr/C77A2019050600004.md): Crossbeam · corroded · May 6, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE FR17 CROSSBEAM UPPER FLANGE DISCOVERED DURING BASIC CHECK. THE DAMAGE WAS REMOVED BY BLEND OUT WITH THE FOLLOWING APPROXIMATE DIMENSIONS: 0.750 INCH X
- [SDR C77A2019050600002](https://openairdocs.org/sdr/C77A2019050600002.md): Fitting · corroded · May 6, 2019 · N607CZ · Emb ERJ170100LR · Fuselage Miscellaneous Structure
  > CORROSION HAS BEEN FOUND ON THE AFT CARGO DOORWAY– FWD FITTING P/N 170-85492-403, CENTER FITTING P/N 170-85251-401, AND/OR AFT FITTING P/N 170-85493-403 ON SEVERAL AIRCRAFT DURING BASIC CHECK. SINCE CLASSIFIES THESE FITTINGS AS PSES, HAS CLASSIFIED REPLACEMENT
- [SDR C77A2019050600001](https://openairdocs.org/sdr/C77A2019050600001.md): Crossbeam · corroded · May 6, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > EO E175-53MR-185 REV IR WAS RELEASED TO REPAIR CORROSION DAMAGE TO THE UPPER FLANGE OF THE FR17 CROSSBEAM BY CUTOUT AND DOUBLER INSTALLATION IN ACCORDANCE WITH ETD2015-170-050159. DURING A SUBSEQUENT INSPECTION OF THE AREA DURING THE B6 BASIC CHECK, NEW CORROS
- [SDR C77A2020031400037](https://openairdocs.org/sdr/C77A2020031400037.md): Seat Track · corroded · May 5, 2019 · N607CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > DURING BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED AT A PREVIOUS REPAIR DOUBLER ON FORWARD FUSELAGE LH IB SEAT TRACK BEAM (P/N 170-03264-001) AT FR17 IN THE FORWARD WET AREA FLOOR STRUCTURE. REFERENCE ETD2019-170-055163 FIGURE 1 FOR THE DAMAGE LOCATION AND D
- [SDR C77A2019050400001](https://openairdocs.org/sdr/C77A2019050400001.md): Seat Track · corroded · May 4, 2019 · N607CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION HAS BEEN FOUND ON THE CABIN RT SEAT TRACK P/N 170-02056-008 DURING BASIC CHECK. SINCE 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 AIRCRAFT. THI
- [SDR C77A2019042900001](https://openairdocs.org/sdr/C77A2019042900001.md): Seat Track · corroded · May 4, 2019 · N607CZ · 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 FORWARD FUSELAGE LT LATERAL SEAT TRACK P/N 170-20955-001. THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DIRECT REPLACEMENT OF THE AFFECTED
- [SDR C77A2019050300002](https://openairdocs.org/sdr/C77A2019050300002.md): Crossbeam · corroded · May 3, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > EO E175-53MR-184 REV 1 WAS RELEASED TO REPAIR CORROSION DAMAGE TO THE UPPER FLANGE OF THE FR14 CROSSBEAM BY CUTOUT AND DOUBLER INSTALLATION IN ACCORDANCE WITH ETD2015-170-048470B. DURING A SUBSEQUENT INSPECTION OF THE AREA DURING THE B6 BASIC CHECK, NEW CORROS
- [SDR C77A2019050300001](https://openairdocs.org/sdr/C77A2019050300001.md): Crossbeam · corroded · May 3, 2019 · N607CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING INSPECTION DURING THE B6 BASIC CHECK, CORROSION DAMAGE WAS FOUND AT THE UPPER FLANGE OF THE FR11 CROSSBEAM. REFERENCE ETD2019-170-055897B FIGURE 1 FOR DETAILS. REQUESTED AND RECEIVED ETD2019-170-055897B TO REPAIR THE DAMAGE. THIS EO IS BEING ISSUED TO P

Next page: https://openairdocs.org/aircraft/N607CZ/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 = 'N607CZ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N607CZ/reports

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