# Service difficulty reports: N614CZ

A list on [N614CZ](https://openairdocs.org/aircraft/N614CZ.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 · 112 reports

- [SDR SWI2025F00152](https://openairdocs.org/sdr/SWI2025F00152.md): Circuit Breaker · arced · Jan 23, 2025 · N614CZ · Emb ERJ170200LR · Electrical Power System Wiring
  > L/H CIRCUIT BREAKER PANEL ARCED ON FRAME 10 BETWEEN STRINGERS 12L-13L. (C-CHECK RO 2/15/2025) REMOVED DAMAGE AND INSTALLED FABRICATED DOUBLER BEHIND L/H CIRCUIT BREAKER PANEL AT FRAME 10, BETWEEN STRINGERS 12L AND 13L REF ETD2025-170-900503, REV A. NO
- [SDR SWI2025F00160](https://openairdocs.org/sdr/SWI2025F00160.md): Doubler · corroded · Jan 17, 2025 · N614CZ · Emb ERJ170200LR · Fuselage Floor Panel
  > RH COCKPIT FLOOR DOUBLER CORRODED AS MARKED FR 8-12 (C-CHECK RO 2/15/2025) REMOVED AND PERFORMED DOUBLER REPAIR ON RH COCKPIT FLOOR DOUBLER BETWEEN FR 8-12. WEIGHT FOR REPAIR PARTS AND FASTENERS MEASURE 80G.(I.D# HG3-61241 DUE: 08/21/25) REF: SRM 53-10-
- [SDR SWIA202502180117](https://openairdocs.org/sdr/SWIA202502180117.md): Doubler · corroded · Jan 17, 2025 · N614CZ · Emb ERJ170200LR · Fuselage Floor Panel
  > LH COCKPIT FLOOR DOUBLER CORRODED AS MARKED FR 8 - 12 (C-CHECK RO 2/15/2025) CUT OUT DAMAGED SECTION OF LH COCKPIT FLOOR DOUBLER BETWEEN FR8 - FR12. INSTALLED NEW LH COCKPIT FLOOR DOUBLER REPAIR. WEIGHT OF REPAIR PARTS AND FASTENERS MEASURE 56.4 G. NO C
- [SDR SWIA20250218116](https://openairdocs.org/sdr/SWIA20250218116.md): Shear Tie · corroded · Jan 16, 2025 · N614CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFTER REMOVAL OF WASTE BOX FOUND SHEAR CLIP AT FR88 STRINGER 27R-28R CORRODED (C-CHECK RO 2/15/2025) REMOVED AND REPLACED SHEAR CLIP AT FR88 STRINGER 27R-28R REF: SRM 51-40-08. SHEAR CLIP REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
- [SDR SWI2025F00159](https://openairdocs.org/sdr/SWI2025F00159.md): Skin · cracked · Jan 12, 2025 · N614CZ · Emb ERJ170200LR · Vertical Stabilizer, Plate/Skin
  > UPON REMOVAL OF VERTICAL LEADING EDGE, FOUND VERTICAL STABILIZER SUPPORT FLANGE CRACKED ON RH SIDE JUST FORWARD OF PANEL 323GR. (C-CHECK RO 2/15/2025) REPAIRED VERTICAL STABILIZER FWD SPAR AT LEADING EDGE SUPPORT FLANGE WITH DOUBLER REPAIR REF ETD2025-1
- [SDR SWI2025F00158](https://openairdocs.org/sdr/SWI2025F00158.md): Seat Track · corroded · Jan 12, 2025 · N614CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > AFT WET AREA RH SEAT TRACK AT FRAME 84 HAS CORROSION.REMOVED AND REPLACED RH INBD FLOOR BEAM SEAT TRACK FR 74-84 WITH NEW REF. ERJ175 SRM 51-40-08. REPLACED WITH OEM PART NO CHANGE IN WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR FURTHER WORK PERFORMED.
- [SDR SWI2025F00157](https://openairdocs.org/sdr/SWI2025F00157.md): Seat Track · corroded · Jan 12, 2025 · N614CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FWD WET AREA RH SEAT TRACK HAS CORROSION BETWEEN FRAMES 17-18 AS MARKED. (C-CHECK RO 2/15/2025) REMOVED AND REPLACED THE R/H INBOARD SEAT TRACK IN THE FORWARD WET AREA, BETWEEN FRAMES 12 AND 20 REF ERJ175 SRM 51-40-08. SEAT TRACK WAS REPLACED WITH O.E
- [SDR SWI2025F00156](https://openairdocs.org/sdr/SWI2025F00156.md): Floorbeam · corroded · Jan 12, 2025 · N614CZ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > FWD WET AREA RH CROSS BEAM HAS CORROSION AT FRAME 14 AS MARKED. (C-CHECK RO 2/15/2025) CUT AWAY DAMAGED SECTION OF FR 14 CROSSBEAM TO REMOVE DAMAGE. PREFORMED "L" ANGLE/FILLER REPAIR ON FR14 CROSSBEAM REF: SRM 53-00-10/REPAIR 03P. WEIGHT OF REPAIR PARTS
- [SDR SWI2025F00155](https://openairdocs.org/sdr/SWI2025F00155.md): Seat Track · corroded · Jan 12, 2025 · N614CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > AFT WET AREA LH SEAT TRACK AT FRAME 84 HAS CORROSION. (C-CHECK RO 2/15/2025) PERFORMED PERMANENT SPLICE REPAIR ON LH INBD FLOOR BEAM SEAT TRACK FR 83-84 REF. ETD2022-170-022163 REV. B. CHANGE IN WEIGHT MEASURES 267.01 GRAMS CAL. TOOL I.D.# SH2-10286, DU
- [SDR SWIA20250218112](https://openairdocs.org/sdr/SWIA20250218112.md): Support · corroded · Jan 12, 2025 · N614CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > AFT WET AREA RH BEAM BETWEEN FRAMES 86-87 HAS CORROSION AROUND FASTENER HOLE. (C-CHECK RO 2/15/2025) REMOVED AND REPLACED RH FR 86-87 BEAM WITH NEW REF. ERJ175 SRM 51-40-08. REPLACED WITH OEM PART NO CHANGE IN WEIGHT AND BALANCE. SEE CONTINUATION CARD F
- [SDR SWIA2021090860817](https://openairdocs.org/sdr/SWIA2021090860817.md): Bolt · corroded · Aug 13, 2021 · N614CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > DURING REMOVAL OF R/H I/B AFT FLAP, FOUND MULTIPLE SEIZED HARDWARE (C-CHECK RO 9/4/21) REPLACED R/H I/B AFT FLAP SEIZED HARDWARE, SEE CAMP 232578.30-1 FOR MAINTENANCE PERFORMED
- [SDR SWIA2021090860816](https://openairdocs.org/sdr/SWIA2021090860816.md): Flap Track · worn · Aug 8, 2021 · N614CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > RH WING FLAP TRACK 1A HAS MATERIAL LOSE IN RADIUS OF TRACK. (C-CHECK RO 9/4/21) / REMOVED AND REPLACED RH WING FLAP TRACK 1A REF E-175 AMM 57-54-25 TQ WRENCH TC1-456 CAL DUE 5-3-22
- [SDR SWIA2021090860815](https://openairdocs.org/sdr/SWIA2021090860815.md): Flap Track · worn · Aug 8, 2021 · N614CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > LH WING FLAP TRACK 1A HAS MATERIAL LOSE IN RADIUS OF TRACK. (C-CHECK RO 9/4/21) / REMOVED AND REPLACED LH WING FLAP TRACK 1A REF E175 AMM 57-54-25 SEE CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWIA2021090860819](https://openairdocs.org/sdr/SWIA2021090860819.md): Web · deformed · Aug 5, 2021 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FR 52 WEB HAS DOUBLER THAT HAS BEEN INSTALLED THAT HAS ADDITIONAL HOLES THAN THE RIB REINFORCEMENT HAS UNABLE TO USE EXISTING HOLES (C-CHECK RO 9/4/21) REMOVED AND REPLACED LH. FR 52 WEB REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2021090860818](https://openairdocs.org/sdr/SWIA2021090860818.md): Pcu · no test · Aug 3, 2021 · N614CZ · Emb ERJ170200LR · Elevator Control System
  > LH ELEVATOR OUTBOARD PCU FAILED BACKLASH FUNCTIONAL TEST. (C-CHECK RO 9/4/21) REMOVED AND REPLACED LH ELEVATOR PCU TO HINGE BOLT REF. EMB 175 AMM 27-32-01. TW:TC2-61343 DUE: 2-3-22. PERFORMED ELEVETOR CONTROL SYSTEM BACKLASH REF. EMB 175 AMM 27-30-00. BAC
- [SDR C77A2019111100003](https://openairdocs.org/sdr/C77A2019111100003.md): Warning Message · illuminated · Nov 8, 2019 · N614CZ · Emb ERJ170200LR · Aileron Control System
  > AILERON R/H FAIL MSG ON EICAS IN CRUISE.
- [SDR C77A2020020380026](https://openairdocs.org/sdr/C77A2020020380026.md): Shear Tie · corroded · Oct 24, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > DURING THE B6 BASIC CHECK IN BNA, CORROSION WAS DISCOVERED ON THE P/N 170-66531-001 FR88 SHEAR CLIP BETWEEN S-27R/S-28R DURING INSPECTION IN THE AREA. THE DISCREPANT PART WILL BE REPLACED WITH A NEW PART IN ACCORDANCE WITH EMBRAER PRODUCTION DRAWINGS AND SRM C
- [SDR C77A2019102210002](https://openairdocs.org/sdr/C77A2019102210002.md): Floorbeam · corroded · Oct 22, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > DURING SUBSEQUENT INSPECTION OF THE AREA DURING THE B6 BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED AT THE REPAIR DOUBLER, AND ADDITIONAL FURTHER CORROSION WAS FOUND TO THE BEAM. THIS NEW DAMAGE CAN BE REPAIRED BY SRM PART II 53-23-10 REPAIR 04, WHICH WAS A
- [SDR C77A2019102200003](https://openairdocs.org/sdr/C77A2019102200003.md): Rib · cracked · Oct 22, 2019 · N614CZ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > THIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH THE INSTRUCTIONS THAT ARE SPECIFIC TO THE RH HORIZONTAL STABILIZER FROM SB 170-55-0014, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING HORIZONTAL STABILIZER RIBS 10A, 11A, AND 12A WITH NEW,
- [SDR C77A2019102200002](https://openairdocs.org/sdr/C77A2019102200002.md): Rib · cracked · Oct 22, 2019 · N614CZ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > THIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH THE INSTRUCTIONS SPECIFIC TO THE LH HORIZONTAL STABILIZER FROM SB 170-55-0014, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING HORIZONTAL STABILIZER RIBS 10A, 11A, AND 12A WITH NEW, REINFORCE
- [SDR C77A2020020380032](https://openairdocs.org/sdr/C77A2020020380032.md): Floor Support · corroded · Oct 18, 2019 · N614CZ · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90
- [SDR C77A2020020380031](https://openairdocs.org/sdr/C77A2020020380031.md): Gusset · corroded · Oct 18, 2019 · N614CZ · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90
- [SDR C77A2020020380027](https://openairdocs.org/sdr/C77A2020020380027.md): Gusset · corroded · Oct 18, 2019 · N614CZ · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90
- [SDR C77A2020020380025](https://openairdocs.org/sdr/C77A2020020380025.md): Floor Support · corroded · Oct 18, 2019 · N614CZ · 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 170-05663-003 (170-05663-005) RH FLOOR SILL, P/N 170-12114-001 RH FLOOR SPLICE, P/N 170-0
- [SDR C77A2020020380024](https://openairdocs.org/sdr/C77A2020020380024.md): Floor Support · corroded · Oct 18, 2019 · N614CZ · 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 170-05663-003 (170-05663-005) RH FLOOR SILL, P/N 170-12114-001 RH FLOOR SPLICE, P/N 170-0
- [SDR C77A2020020380023](https://openairdocs.org/sdr/C77A2020020380023.md): Floor Support · corroded · Oct 18, 2019 · N614CZ · Emb ERJ170200LL · 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 170-05663-003 (170-05663-005) RH FLOOR SILL, P/N 170-12114-001 RH FLOOR SPLICE, P/N 170-0
- [SDR C77A2020020430050](https://openairdocs.org/sdr/C77A2020020430050.md): Floor Support · corroded · Oct 17, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON THE CENTER FUSELAGE III FLOOR STRUCTURE LONGITUDINAL BEAM INTERCOSTAL BETWEEN FRAMES 89-90. REFERENCE ETD2019-170-138520 FIGURES 1 FOR DETAILS, FOR THE DAMAGE LOCATIONS AND DIMENSIONS. EAMS REQUEST
- [SDR C77A2020020380033](https://openairdocs.org/sdr/C77A2020020380033.md): Floor Support · corroded · Oct 17, 2019 · N614CZ · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90
- [SDR C77A2020020380030](https://openairdocs.org/sdr/C77A2020020380030.md): Gusset · corroded · Oct 17, 2019 · N614CZ · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90
- [SDR C77A2019101700001](https://openairdocs.org/sdr/C77A2019101700001.md): Crossbeam · corroded · Oct 17, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING THE B6 BASIC CHECK AT EAMS ON THE UPPER FLANGE OF THE P/N 170-21769-405 FR17 CROSSBEAM IN THE CABIN FLOOR STRUCTURE OF THE FORWARD FUSELAGE
- [SDR C77A202002043046](https://openairdocs.org/sdr/C77A202002043046.md): Fitting · nicked · Oct 16, 2019 · N614CZ · Emb ERJ170200LR · Spoilers
  > DURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED MINOR NICK/TOOLING DAMAGE ON THE RH WING #1 SPOILER ACTUATOR FITTING ASSEMBLY, P/N 170-34105-406. THERE ARE 14 AREAS OF DAMAGE ON THE ASSEMBLY. REF ETD2019-170-144300, FIGURE 1-4 FOR DAMAGE INFORMATION. THE DAM
- [SDR C77A202002043047](https://openairdocs.org/sdr/C77A202002043047.md): Skin · chafed · Oct 16, 2019 · N614CZ · Emb ERJ170200LR · Wing, Plate/Skin
  > DURING BASIC CHECK AT EAMS, WEAR/CHAFE DAMAGE WAS DISCOVERED ON THE LH WING OB FLE SKIN BETWEEN RIB 37 AND RIB 42. REFERENCE ETD2019-170-141270 FIGURES 1 FOR DETAILS, FOR THE DAMAGE LOCATIONS AND DIMENSIONS. EAMS REQUESTED AND RECEIVED PERMANENT REPAIR DISPOSI
- [SDR C77A2020020430048](https://openairdocs.org/sdr/C77A2020020430048.md): Skin · dented · Oct 16, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED MULTIPLE DENTS ON FORWARD FUSELAGE RH LATERAL SKIN PANEL P/N 170-03385-004 FROM FR01 TO FR05 BETWEEN STGR8R/STGR18R. REFER ETD2019-170-138883 FOR DENTS LOCATIONS AND MEASUREMENTS. THE DAMAGE IS OUT OF LIMITS O
- [SDR C77A2020020430049](https://openairdocs.org/sdr/C77A2020020430049.md): Bearing · corroded · Oct 16, 2019 · N614CZ · Emb ERJ170200LR · Wing, Landing Gear Attach Fittings
  > DURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON THE RH WING SPAR 2 MLG TRUNNION BEARING. REFERENCE ETD2019-170-140027 FIGURES 1 FOR DETAILS, FOR THE DAMAGE LOCATIONS AND DIMENSIONS. EAMS REQUESTED AND RECEIVED PERMANENT REPAIR DISPOSITION IN THE
- [SDR C77A2020020380029](https://openairdocs.org/sdr/C77A2020020380029.md): Shear Panel · corroded · Oct 10, 2019 · N614CZ · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90
- [SDR C77A2020020380028](https://openairdocs.org/sdr/C77A2020020380028.md): Gusset · corroded · Oct 10, 2019 · N614CZ · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90
- [SDR C77A2019101000001](https://openairdocs.org/sdr/C77A2019101000001.md): Floor Support · damaged · Oct 10, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON CONDITION REPLACEMENT OF A DAMAGED OR PREVIOUSLY REPAIRED. LT FLOOR BEAM RBL 273 BETWEEN FRAMES 86 AND 89. THE DAMAGED STRUCTURE WILL BE REPLACED BY USING DRAWINGS. BECAUSE THE TRACK IS A PSE
- [SDR C77A2019042600004](https://openairdocs.org/sdr/C77A2019042600004.md): Shutoff Valve · failed · Apr 26, 2019 · N614CZ · Emb ERJ170200LR · Pneumatic Distribution System
  > ON CLIMB OUT OF PDX CREW REPORTED RECEIVING BLEED OVER PRESSURE MSG. CREW DECLARED EMERGENCY AND SAFELY RETURNED TO PDX; BURNED FUEL FOR LAND WEIGHT. BLEED 2 FAIL/ BLEED 2 OVERPRESS AFTER T/O. DEFERRED IAW MEL 36-11-03-1. TRANSFERRED TO SDI PER MXC D AMOS EMP
- [SDR C77A20170925003](https://openairdocs.org/sdr/C77A20170925003.md): Beam · corroded · Sep 25, 2017 · N614CZ · Emb ERJ170200LR · Fuselage Main, Structure
  > DURING A BASIC CHECK, INSPECTION DISCOVERED THE L1 DOOR LOWER BEAM TO HAVE CORROSION DAMAGE THAT IS BEYOND THE ALLOWABLE SRM LIMITS. BLENDED THE AREA TO REMOVE THE CORROSION. THE BLENDED AREA MEASURES THE FOLLOWING APPROXIMATE DIMENSIONS OF 1.765 INCHES X 1.
- [SDR C77A20170922001](https://openairdocs.org/sdr/C77A20170922001.md): Fitting · corroded · Sep 20, 2017 · N614CZ · Emb ERJ170100STD · 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. REPLACEMENT OF THESE FITTINGS AS A MAJOR REPAIR. THIS EO IS BEING IS
- [SDR C77A20170926001](https://openairdocs.org/sdr/C77A20170926001.md): Floorbeam · corroded · Sep 18, 2017 · N614CZ · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > DURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED THE FORWARD FUSELAGE FRAME 16 FLOORBEAM CORRODED BEYOND THE SRM 53-10-10 LIMITS. REPAIRED IAW. ETD 2017-170-078286
- [SDR C77A20151224001](https://openairdocs.org/sdr/C77A20151224001.md): Flashlight · inoperative · Dec 23, 2015 · N614CZ · Emb ERJ170200LR · Emergency Equipment
  > BOTH AFT FLIGHT ATTENDANT FLASHLIGHTS LED LIGHT NOT FLASHING. R & R BOTH AFT FLIGHT ATTENDANT FLASHLIGHTS IAW AMM 33-51-01. OK FOR SERVICE.
- [SDR C77A20151218002](https://openairdocs.org/sdr/C77A20151218002.md): Fuse · blown · Dec 16, 2015 · N614CZ · Emb ERJ170200LR · Emergency Lighting
  > R2 DOOR EMER OVERHEAD EXIT SIGN NOT ILLUMINATING DURING OPERATIONS CHECKS. R & R ELPU FUSE IAW SMPE 17X-33-002 RI. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR C77A20151014001](https://openairdocs.org/sdr/C77A20151014001.md): Battery · discharged · Oct 13, 2015 · N614CZ · Emb ERJ170200LR · Emergency Equipment
  > FORWARD GALLEY FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERY IAW AMM 33-51-00. OK FOR SERVICE.
- [SDR C77A20151013020](https://openairdocs.org/sdr/C77A20151013020.md): Retainer · corroded · Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT FUSELAGE WATER SERVICE ACCESS DOOR CUT OUT INTERNAL RETAINERS, PN 170-86654-003 & 170-86657-001, ARE CORRODED BETWEEN STATION 23041.0 - 23453.0, STRINGER 27L - 29L, X=23041 - 23453, Y= STRINGER 27L - 29L. PERMANENTLY REMOVED THE WATER PAN RETAINERS ON WO
- [SDR C77A20151013019](https://openairdocs.org/sdr/C77A20151013019.md): Retainer · corroded · Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT FUSELAGE WASTE SERVICE PAN RETAINERS, PN 170-86654-003 & 170-86655-003, HAVE CORROSION BETWEEN STATION 24048 - 24458, Y=+260.4, X=24048 - 24458, Y= STRINGER 24R - 26R. PERMANENTLY REMOVED THE WASTE PAN RETAINERS ON WO 19451501G3 IAW EO E17X-5300-004.3 REV
- [SDR C77A20151013018](https://openairdocs.org/sdr/C77A20151013018.md): Support · corroded · Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CABIN FLOOR, LT GALLEY SUPPORT PN 170-86132-003 AT FRAME 90, X=24868, Y=+100. R & R AFT CABIN FRAME 90, LT FLOOR SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 19451482F1 IAW EO E175-5300-125 REV IR WO 1965342.
- [SDR C77A20151013017](https://openairdocs.org/sdr/C77A20151013017.md): Gusset · corroded · Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > EXFOLIATION CORROSION ON AFT CABIN FLOOR, RT INBD GUSSET PN 170-60257-001 AT FRAME 90, Y=-260.4, X=24868, Y= -260. R & R AFT CABIN FRAME 90, RT INBD GUSSET IAW SRM 51-41-01 & 51-43-01 ON WO 19451482F7 IAW EO E175-5300-125 REV IR WO 1965342.
- [SDR C77A20151013016](https://openairdocs.org/sdr/C77A20151013016.md): Gusset · corroded · Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CABIN FLOOR, RT OTBD GUSSET FRAME 90. R & R THE GUSSET IAW SRM 51-41-01 & 51-43-01.
- [SDR C77A20151013015](https://openairdocs.org/sdr/C77A20151013015.md): Gusset · corroded · Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > EXFOLIATION CORROSION ON AFT CABIN FLOOR, LT INBD GUSSET PN 170-60257-001, AT FRAME 90, Y=.260.4, X=24868, Y= -260. R & R AFT CABIN FRAME 90, LT INBD GUSSET IAW SRM 51-41-01 & 51-43-01 ON WO 19451482F3 IAW EO E175-5300-125 REV IR WO 1965342.

Next page: https://openairdocs.org/aircraft/N614CZ/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 = 'N614CZ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N614CZ/reports

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