N602CZ

Service difficulty reports not matched to an aircraft · 117

They name N602CZ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N602CZ' AND registry_match IS NULL
  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 C77A20150305011Splice · corrodedAFT CABIN RT FLOOR SPLICE, PN 170-86125-001, HAS CORROSION AT FRAME 89, X= 24458, Y= 260.4. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213171J4 IAW ETD 2015-170-016788 & EO E175-5300-100 REV IR WO 1834035.Mar 2, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150305010Splice · corrodedAFT CABIN RT FLOOR SPLICE, PN 170-65644-001, HAS CORROSION BETWEEN FRAME 87 & 88, X= 24048, Y= 1041.4. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213171J4 IAW ETD 2015-170-016788 & EO E175-5300-100 REV IR WO 1834035.Mar 2, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150305009Panel Support · corrodedAFT CABIN CROSS FRAME 89 PANEL SUPPORT, PN 170-86181-003, HAS CORROSION AT FRAME 89, X= 24458, Y=914.4. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213171J4 IAW ETD 2015-170-016788 & EO E175-5300-100 REV IR WO 1834035.Mar 2, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150305008Panel Support · corrodedAFT CABIN CROSS FRAME 86 LT PANEL SUPPORT, PN 170-66797-001, HAS CORROSION AT FRAME 87, X= 23865, Y= -736.6. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213171J4 IAW ETD 2015-170-016788 & EO E175-5300-100 REV IR WO 1834035.Mar 2, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150305007Gusset · corrodedAFT CABIN RT OTBD AFT GUSSET, PN 170-60259-001, HAS CORROSION AT FRAME 90, X= 24868, Y=660.4. R & R RT OTBD FLOOR GUSSET AT FRAME 90 IAW SRM 51-41-01 & 51-43-01 ON WO 6213171J9 IAW EO E175-5300-100 REV IR WO 1834035.Mar 2, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150305006Door Sill · corrodedFORWARD CABIN RT AFT FLOOR SILL, PN 170-05661-003, HAS CORROSION BETWEEN FRAME 17 & 18, X=5064 - 5323, Y=1066.8 TO 1270. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 14680921H4 IAW ETD 2015-170-016753A & EO E175-5300-101 REV IR WO 1834324.Mar 2, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150305005Door Sill · corrodedFORWARD CABIN RT FWD FLOOR SILL, PN 170-05663-003, HAS CORROSION BETWEEN FRAME 13 & 14, X=4011 - 4270, Y=939.8 TO Y=1244.6. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 14680921H1 IAW ETD 2015-170-016753A & EO E175-5300-101 REV IR WO 1834324.Mar 2, 2015 · N602CZ · Emb ERJ190200LR · Fuselage Miscellaneous StructureSDR C77A20150305004Doubler · corrodedFORWARD CABIN RT AFT FLOOR DOUBLER SPLICE, PN 170-12114-001, HAS CORROSION AT FRAME 18 - 19, X= 5323 - 5645, Y=609.6. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 14680921H3 IAW ETD 2015-170-016753A & EO E175-5300-101 REV IR WO 1834324.Mar 2, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150305003Doubler · corrodedFORWARD CABIN LT AFT FLOOR DOUBLER, PN 170-07311-001, HAS CORROSION AT FRAME 19, X=5645, Y= -381 & -635. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 1468092 1G2 IAW ETD 2015-170-016753A & EO E175-5300-101 REV IR WO 1834324.Mar 2, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150305002Doubler · corrodedFORWARD CABIN LT FWD FLOOR DOUBLER, PN 170-12118-001, HAS CORROSION AT FRAME 16 X= 4711, Y= -381 & -990.6. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 1468092 1G4 IAW ETD 2015-170-016753A & EO E175-5300-101 REV IR WO 1834324.Mar 2, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150305001Threshold · corrodedFORWARD PAX DOOR LOWER THRESHOLD BEAM, PN 170-03719-005, HAS CORROSION & GOUGE BETWEEN FRAME 16 - 19, X= 4711 - 5645, Y= -1270. BLENDED GOUGE & REMOVED CORROSION AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6212701G3 IAW ETD 2015-170-016193 & EA E175-53-479 REV IR Mar 2, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A201502280010Floor Support · gougedFWD CABIN FUSELAGE FLOOR SUPPORT HAS CORROSION AT X= FRAME 18, Y=787.4. R& R SUPPORT 170-14734-001 IAW SRM 51-43-01, WO 1468092 1G5 & EO E175-5300-101 REV IR WO 1834324.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A201502280012Door Sill · gougedFORWARD CABIN FUSELAGE FLOOR SILL HAS GOUGE AT X= FRAME 19, Y=STRINGER 16L. R & R FLOOR SILL 170-05662-001-001 IAW SRM 51-41-02, WO 1468092 1G1 & EO E175-5300-101 REV IR WO 1834324.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A201502280011Angle · corrodedFORWARD CABIN FUSELAGE FLOOR PANEL ANGLE HAS CORROSION AT X= FRAME 14, Y=711.2. R & R FLOOR PANEL ANGLE 170-04075-001 IAW SRM 51-43-01, WO 1468092 1G9 & EO E175-5300-101 REV IR WO 1834324.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A201502280010AAngle · corrodedFORWARD CABIN FUSELAGE FLOOR SUPPORT HAS CORROSION AT X= FRAME 18, Y=787.4. R & R SUPPORT 170-14734-001 IAW SRM 51-43-01, WO 1468092 1G5 & EO E175-5300-101 REV IR WO 1834324.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150228009Floor Support · corrodedAFT CABIN FUSELAGE CTL III FLOOR PANEL SUPPORT ANGLE HAS CORROSION AT FRAME 88, Y= 736.6. R & R SUPPORT ANGLE 170-66796-001 IAW SRM 51-10-03, WO 6213171L5 & EO E175-5300-100 REV IR WO 1834035.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150228008Upper Sheet · corrodedAFT CABIN FUSELAGE CTL III UPPER SHEET HAS CORROSION BETWEEN FRAME 85 & 86, Y= 260.4. R & R UPPER SHEET 170-86101-001-001 IAW SRM 51-41-02, WO 6213171H6 & EO E175-5300-100 REV IR WO 1834035.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150228007Floor Support · corrodedAFT CABIN FUSELAGE CTL III FLOOR PANEL SUPPORT ANGLE HAS CORROSION AT FRAME 86, Y= 739. R & R SUPPORT ANGLE 170-66796-001 IAW SRM 51-41-02 WO 6213171I3 & EO E175-5300-100 REV IR WO 1834035.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150228006Upper Sheet · corrodedAFT CABIN FUSELAGE CTL III UPPER SHEET HAS CORROSION BETWEEN FRAME 85 & 86, Y= 260.4. R & R UPPER SHEET 170-86101-001-001 IAW SRM 51-41-02, WO 6213171H5 & EO E175-5300-100 REV IR WO 1834035.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150228005Gusset · corrodedAFT CABIN FUSELAGE CTL III GUSSET HAS CORROSION AT FRAME 90, Y= 260.4. R & R GUSSET PLATE 170-60257-001 IAW SRM 51-41-02, WO 6213171J2 & EO E175-5300-100 REV IR WO 1834035.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150228004Panel · corrodedAFT CABIN FUSELAGE CTL III LT SHEAR PANEL HAS CORROSION BETWEEN FRAME 87 & 88 FROM Y= 304 - Y=1041.4. R & R SHEAR PANEL 170-65927-007 IAW SRM 51-42-02 WO 6213171H9 & EO E175-5300-100 REV IR WO 1834035.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2015022800003Shear Plate · corrodedAFT CABIN FUSELAGE CTL III LT SHEAR PANEL HAS CORROSION BETWEEN FRAME 87 & 88 FROM Y= 304 - Y=1041.4. R & R SHEAR PANEL 170-65927-007 IAW SRM 51-42-02 WO 6213171H9 & EO E175-5300-100 REV IR WO 1834035.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150228003Gusset · corrodedAFT CABIN FUSELAGE CTL III GUSSET HAS CORROSION AT FRAME 90, Y=260.4. R & R GUSSET PLATE 170-60257-001 IAW SRM 51-41-02 WO 6213171J1 & EO E175-5300-100 REV IR WO 1834035.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR C77A20150228002Support · corrodedAFT CABIN FUSELAGE CTL III PANEL SUPPORT HAS CORROSION AT FRAME 90, Y=762. R & R PANEL SUPPORT 170-86139-005 IAW SRM 51-43-01 WO 6213171I8 & EO E175-5300-100 REV IR WO 1834035.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2015022800002Gusset · corrodedAFT CABIN FUSELAGE CTL III GUSSET HAS CORROSION AT FRAME 90, Y=660.4. R & R GUSSET PLATE 170-60259-001 IAW SRM 51-41-02 WO 6213171I9 & EO E175-5300-100 REV IR WO 1834035.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A2015022800001Mount · gougedFORWARD SERVICE DOOR, FWD EES MOUNT FITTING GOUGED. BLENDED & ACCOMPLISHED HFEC. TREATED, PRIMED & TOPCOAT FWD EES MOUNT FITTING IAW SRM 51-23-04 & 53-23-05, 51-23-06 WO 1492058 8C1 & IAW EA E175-52-086 REV 1.Feb 28, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Main, Attach FittingsSDR C77A20150227003Gusset · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE R1 DOOR INTERNAL GUSSET PLATE. THE APPROX DAMAGE DIMENSIONS ARE AS FOLLOWS: .8 INCH X .3 INCH TO A MAXIMUM DEPTH OF .027 INCH DEEP. REQUESTED & RECEIVEFeb 27, 2015 · N602CZ · Emb ERJ170200LR · Service DoorsSDR C77A20150227002Shear Tie · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE TO THE FOLLOWING AFT CARGO FRAME ATTACHING STRUCTURE. SHEAR TIE PN 170-66868-001 & SHEAR TIE PN 170-66674-001 - PERMANENT REPAIR BY REPLACEMENT. SUPPORT PFeb 27, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR C77A20150227001Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CROSSBEAM FRAME 17 UPPER FLANGE. THIS NEW CORROSION DAMAGE IS INCORPORATED PREVIOUS REPAIR DOCUMENTED ON EO E175-53MR-140 IAW ETD 2013-170-011399B. Feb 27, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150226001Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CROSSBEAM FRAME 14 UPPER FLANGE. THIS NEW CORROSION DAMAGE INCORPORATED PREVIOUS REPAIRS DOCUMENTED ON EO E175-53MR-135 IAW ETD 2013-170-006436D. THFeb 26, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR C77A20150223004Floorbeam · corrodedAFT CABIN RT FLOORBEAM, PN 170-65669-004, HAS CORROSION AT FRAME 7, X= 23865 Y= 260.4. R & R RT FLOORBEAM IAW SRM 51-41-01 & 51-43-01 ON WO 6213171H8 IAW 53MR-094 REV 4 WO 1832102.Feb 23, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR C77A20150223003Floorbeam · corrodedAFT CABIN LT FLOORBEAM HAS CORROSION AT FRAME 87, X=23865, Y= -260.4. R & R LT FLOORBEAM IAW SRM 51-41-01 & 51-43-01 ON WO 6213171H7 IAW EO E170-53MR-093 REV 3 WO 1832163.Feb 23, 2015 · N602CZ · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR C77A20150223002Seat Track · corrodedFORWARD CABIN RT SEAT TRACK, PN 170-03263-001 & EXISTING REPAIR DOUBLER HAS CORROSION BETWEEN FRAME 14 - 17, X=4270-5064, Y=260.4. R & R RT SEAT TRACK IAW SRM 51-41-01 & 51-43-01 ON WO 14680921G7 IAW EO E170-53MR-062 REV 5 WO 1831538.Feb 23, 2015 · N602CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR C77A20150223001Seat Track · corrodedFORWARD CABIN LT SEAT TRACK, PN 170-03264-001, HAS SEVERAL AREAS OF CORROSION BETWEEN FRAME 16 - 20, X=4711-6070, Y= -260.4. R & R LT SEAT TRACK IAW SRM 51-41-01 & 51-43-01 ON WO 14963892E8 IAW EO E170-53MR-061 REV 5 WO 1831518.Feb 23, 2015 · N602CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR C77A20140630001Battery · dischargedR1 FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. DEFERRED & THEN R & R THE R1 FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM.Jun 27, 2014 · N602CZ · Emb ERJ170200LR · Emergency EquipmentSDR C77A20130430030Wire · damagedDURING BASIC CHECK 3, RODENT DAMAGE WAS EVIDENT IN THE FWD CABIN CEILING AREA. OPENED ENTIRE INTERIOR CEILINGS AND SIDEWALLS FOR A RODENT DAMAGE INSPECTION. THE INSPECTION RESULTED IN 30 DAMAGED WIRES, THREE WHICH WERE FLY BY WIRE, 20 DAMAGED INSULATION BLANKApr 26, 2013 · N602CZ · Emb ERJ170200LR · Flight Control System WiringSDR C77A20130430029Flap Track · wornRT WING FLAP TRACK 2A OTBD, IS WORN OUT OF LIMITS THICKNESS REDUCTION D= .015" REF SRM 57-52-03, TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR C77A20130430028Flap Track · wornRT WING FLAP TRACK 2 OTBD, WORN OUT OF LIMITS THICKNESS REDUCTION D= .017" REF SRM 57-52-03, TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR C77A20130430027Flap Track · wornRT WING FLAP TRACK 2 INBD, IS WORN OUT OF LIMITS THICKNESS REDUCTION D=.017" IAW SRM 57-52-03, TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR C77A20130430026Flap Track · wornLT WING FLAP TRACK 2 OTBD, IS WORN OUT OF LIMITS THICKNESS REDUCTION D= .019" REF SRM 57-52-03 TABLE 101. BLENDED WORN AREA IAW SRM PART II 51-10-03.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Trailing Edge FlapsSDR C77A20130430025Heat Shield · chafedRT AFT PYLON NR 4 HEAT SHIELD HAS L/E AND T/E DAMAGE. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW SRM PART II 54-31-00.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Nacelle/Pylon, Main FrameSDR C77A20130430024Heat Shield · chafedRT AFT PYLON NR 3 HEAT SHIELD HAS L/E AND T/E DAMAGE. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW SRM PART II 54-31-00.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Nacelle/Pylon, Main FrameSDR C77A20130430023Heat Shield · chafedRT AFT PYLON NR 2 HEAT SHIELD HAS L/E AND T/E DAMAGE. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW SRM PART II 54-31-00.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Nacelle/Pylon, Main FrameSDR C77A20130430022Heat Shield · chafedRT AFT PYLON, NR 1 HEAT SHIELD IS CHAFED IN THE LWR CENTER AREA. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW SRM PART II 54-31-00.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Nacelle/Pylon, Main FrameSDR C77A20130430021Heat Shield · chafedLT AFT PYLON NR 3 HEAT SHIELD HOLE IN THE AFT JOGGLE AND CHAFED ON THE AFT EDGE. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW SRM PART II 54-31-00.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Nacelle/Pylon, Main FrameSDR C77A20130430020Heat Shield · chafedLT AFT PYLON, NR 1 HEAT SHIELD CHAFED IN THE LWR CENTER AREA. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW PRINCIPLES OF SRM PART II 54-50-23, REPAIR 16P ON WO 670776-407 IAW ETD 2013-170-006437 AND COMPASS EA E175-54-132, REV IR WO 722744.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Nacelle/Pylon, Main FrameSDR C77A20130430019Structure · wornRT MLG MIDDLE DOOR ATTACHMENT HOLE IS ELONGATED AT THE FASTENER HOLE. REAMED HOLE OVERSIZED IAW SRM PART II 51-40-02 AND FABRICATED AND INSTALLED REPAIR BUSHING IAW SPEC NE32-003, ETD 2013-170-006485 AND COMPASS EO E175-53MR-002, REV IR.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Landing Gear DoorsSDR C77A20130430018Bushing · migratedNLG RETRACTION ACTUATOR INBD BUSHING, MIGRATED ON SHOCK STRUT. REPLACED NLG RETRACT ACTUATOR FITTING INBD BUSHING IAW ED-LLI-10-0008 AND EO E17X-3200-007 REV IR.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Nose/Tail Landing GearSDR C77A20130430017Doubler · corrodedAFTER REMOVAL OF BRACKET, CORROSION WAS FOUND ON INTERNAL DOUBLER SKIN. Y= 21192-21617, STR= 27R-28R. BLENDED CORROSION IAW SRM 51-10-03 & 51-12-01.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR C77A20130430016Door Frame · chafedFWD CARGO DOOR FRAME HAS CHAFE DAMAGE ON DOOR FRAME AT 3 DOOR LINER ISOLOATOR LOCATIONS. BLENDED DAMAGED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 670776-818 IAW 2013-170-006488-A AND COMPASS EO E175-53MR-002 REV IR WO 724643.Apr 26, 2013 · N602CZ · Emb ERJ170200LR · Cargo/Baggage Doors
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