N614CZ

Service difficulty reports · 112

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 = 'N614CZ' 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 SWI2025F00152Circuit Breaker · arcedL/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 Jan 23, 2025 · N614CZ · Emb ERJ170200LR · Electrical Power System WiringSDR SWI2025F00160Doubler · corrodedRH 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-Jan 17, 2025 · N614CZ · Emb ERJ170200LR · Fuselage Floor PanelSDR SWIA202502180117Doubler · corrodedLH 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 CJan 17, 2025 · N614CZ · Emb ERJ170200LR · Fuselage Floor PanelSDR SWIA20250218116Shear Tie · corrodedAFTER 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 NOTEDJan 16, 2025 · N614CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWI2025F00159Skin · crackedUPON 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 ETD2025-1Jan 12, 2025 · N614CZ · Emb ERJ170200LR · Vertical Stabilizer, Plate/SkinSDR SWI2025F00158Seat Track · corrodedAFT 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.Jan 12, 2025 · N614CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWI2025F00157Seat Track · corrodedFWD 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.EJan 12, 2025 · N614CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWI2025F00156Floorbeam · corrodedFWD 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 Jan 12, 2025 · N614CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWI2025F00155Seat Track · corrodedAFT 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, DUJan 12, 2025 · N614CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA20250218112Support · corrodedAFT 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 FJan 12, 2025 · N614CZ · Emb ERJ170200LR · Fuselage Main, StructureSDR SWIA2021090860817Bolt · corrodedDURING 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 PERFORMEDAug 13, 2021 · N614CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR SWIA2021090860816Flap Track · wornRH 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 5-3-22Aug 8, 2021 · N614CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR SWIA2021090860815Flap Track · wornLH 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 PERFORMEDAug 8, 2021 · N614CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR SWIA2021090860819Web · deformedFR 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.Aug 5, 2021 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2021090860818Pcu · no testLH 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. BACAug 3, 2021 · N614CZ · Emb ERJ170200LR · Elevator Control SystemSDR C77A2019111100003Warning Message · illuminatedAILERON R/H FAIL MSG ON EICAS IN CRUISE.Nov 8, 2019 · N614CZ · Emb ERJ170200LR · Aileron Control SystemSDR C77A2020020380026Shear Tie · corrodedDURING 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 COct 24, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR C77A2019102210002Floorbeam · corrodedDURING 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 AOct 22, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR C77A2019102200003Rib · crackedTHIS 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, Oct 22, 2019 · N614CZ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/RibSDR C77A2019102200002Rib · crackedTHIS 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, REINFORCEOct 22, 2019 · N614CZ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/RibSDR C77A2020020380032Floor 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90 Oct 18, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2020020380031Gusset · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90 Oct 18, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2020020380027Gusset · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90 Oct 18, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2020020380025Floor 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 170-05663-003 (170-05663-005) RH FLOOR SILL, P/N 170-12114-001 RH FLOOR SPLICE, P/N 170-0Oct 18, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2020020380024Floor 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 170-05663-003 (170-05663-005) RH FLOOR SILL, P/N 170-12114-001 RH FLOOR SPLICE, P/N 170-0Oct 18, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2020020380023Floor 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 170-05663-003 (170-05663-005) RH FLOOR SILL, P/N 170-12114-001 RH FLOOR SPLICE, P/N 170-0Oct 18, 2019 · N614CZ · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR C77A2020020430050Floor Support · corrodedDURING 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 REQUESTOct 17, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2020020380033Floor 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90 Oct 17, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2020020380030Gusset · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90 Oct 17, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2019101700001Crossbeam · corrodedTHIS 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 FUSELAGEOct 17, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Main, StructureSDR C77A202002043046Fitting · nickedDURING 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 DAMOct 16, 2019 · N614CZ · Emb ERJ170200LR · SpoilersSDR C77A202002043047Skin · chafedDURING 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 DISPOSIOct 16, 2019 · N614CZ · Emb ERJ170200LR · Wing, Plate/SkinSDR C77A2020020430048Skin · dentedDURING 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 OOct 16, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR C77A2020020430049Bearing · corrodedDURING 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 THEOct 16, 2019 · N614CZ · Emb ERJ170200LR · Wing, Landing Gear Attach FittingsSDR C77A2020020380029Shear 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90 Oct 10, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2020020380028Gusset · 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 170-60259-001 FR90 RH OB GUSSET, P/N 170-60257-001 FR90 RH IB GUSSET, P/N 170-60257-001 FR90 Oct 10, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2019101000001Floor Support · damagedTHIS 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 PSEOct 10, 2019 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2019042600004Shutoff Valve · failedON 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 EMPApr 26, 2019 · N614CZ · Emb ERJ170200LR · Pneumatic Distribution SystemSDR C77A20170925003Beam · corrodedDURING 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.Sep 25, 2017 · N614CZ · Emb ERJ170200LR · Fuselage Main, StructureSDR C77A20170922001Fitting · corrodedCORROSION 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 ISSep 20, 2017 · N614CZ · Emb ERJ170100STD · Fuselage Miscellaneous StructureSDR C77A20170926001Floorbeam · corrodedDURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED THE FORWARD FUSELAGE FRAME 16 FLOORBEAM CORRODED BEYOND THE SRM 53-10-10 LIMITS. REPAIRED IAW. ETD 2017-170-078286Sep 18, 2017 · N614CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR C77A20151224001Flashlight · inoperativeBOTH AFT FLIGHT ATTENDANT FLASHLIGHTS LED LIGHT NOT FLASHING. R & R BOTH AFT FLIGHT ATTENDANT FLASHLIGHTS IAW AMM 33-51-01. OK FOR SERVICE.Dec 23, 2015 · N614CZ · Emb ERJ170200LR · Emergency EquipmentSDR C77A20151218002Fuse · blownR2 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.Dec 16, 2015 · N614CZ · Emb ERJ170200LR · Emergency LightingSDR C77A20151014001Battery · dischargedFORWARD GALLEY FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERY IAW AMM 33-51-00. OK FOR SERVICE.Oct 13, 2015 · N614CZ · Emb ERJ170200LR · Emergency EquipmentSDR C77A20151013020Retainer · corrodedAFT 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 Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20151013019Retainer · corrodedAFT 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 REVOct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20151013018Support · corrodedCORROSION 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.Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20151013017Gusset · corrodedEXFOLIATION 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.Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20151013016Gusset · corrodedCORROSION ON AFT CABIN FLOOR, RT OTBD GUSSET FRAME 90. R & R THE GUSSET IAW SRM 51-41-01 & 51-43-01.Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20151013015Gusset · corrodedEXFOLIATION 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.Oct 11, 2015 · N614CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
Back to N614CZ