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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR C77A2019101100001Sign · inoperativeR1 DOOR EMERGENCY LIGHT INOP - LOWER "EXIT" LIGHT. REPLACED R1 DOOR LIGHT ID SIGN PER AMM 33-50-17 OPS CHECK GOOD.SDR C77A2019010700001Rib · brokenTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH PART II OF SB 170-57-0047, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION ON THE RT WING. THIS MODIFICATION CONSISTS OF REPLACING RIB 10 AT FTE WITH A NEW REINFORCED RIB 10 P/N 170-32161-628 AND PERFORMING A COLD EXPASDR C77A2019010200003Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CENTER FUSELAGE III LT INBOARD SEAT TRACK P/N 170-86081-003 AND RT INBOARD SEAT TRACK P/N 170-86082-003. DAMAGE DETAILS AND DIMENSIONS ARE SHOWN IN FISDR C77A2019010200002Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CENTER FUSELAGE III LT INBOARD SEAT TRACK P/N 170-86081-003 AND RT INBOARD SEAT TRACK P/N 170-86082-003. DAMAGE DETAILS AND DIMENSIONS ARE SHOWN IN FISDR C77A2019010200001Floorbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE TO THE UPPER FLANGE OF THE CENTER FUSELAGE II LT FLOORBEAM (P/N 170-65669-003) AT FR86. THE DAMAGE MEASURES APPROXIMATELY 0.03 INCH IN DIAMETER TO A DEPTH OF 0SDR C77A2020031800008Beam · corrodedDURING BASIC CHECK IN BNA, INSPECTION DISCOVERED CORROSION IN TWO BOLT HOLES ON THE FORWARD PASSENGER DOOR LOWER BEAM, P/N 170-03719-005. (REF ETD2018-170-135198, FIGURE 1). EAMS REQUESTED AND RECEIVED ETD2018-170-135198 FOR A PERMANENT REPAIR BY REAMING THE DSDR C77A2020031800022Doubler · corrodedMID BELLY PANEL 192CR DOUBLER CORRODED WORK ORDER 2450172623SDR C77A2020031800013Heat Shield · crackedAIRCRAFT 602CZ WAS AOG IN SJC DUE TO THE DISCOVERY OF CRACKS ON THE LH ENGINE PYLON AFT FAIRING #5 HEAT SHIELD (REF ETD2018-170-093210A, FIGURES 1-3). COMPASS AIRLINES REQUESTED AND RECEIVED RELIEF IN THE FORM OF ETD2018-170-093210 WHICH PROVIDES A 750FC FLY-BSDR C77A2020031800016Panel Support · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING AFT WET AREA FLOOR STRUCTURE: LH PANEL SUPPORT P/N 170-86139-005, LH FR87 SPLICE P/N 170-65644-001, FR90 RH OB GUSSET P/N 170-60259-001. REFERENCE ETD2018-170-133043 FIGURE 1, ETD2018-170-133216 SDR C77A2020031800015Splice · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING AFT WET AREA FLOOR STRUCTURE: LH PANEL SUPPORT P/N 170-86139-005, LH FR87 SPLICE P/N 170-65644-001, FR90 RH OB GUSSET P/N 170-60259-001. REFERENCE ETD2018-170-133043 FIGURE 1, ETD2018-170-133216 SDR C77A2020031800012Firewall · damagedDURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED FIRE LOOP CLAMP RIVET HOLES ELONGATED IN THE APU COMPARTMENT IN THE REAR FUSELAGE (REF ETD2018-170-133016, FIGURE 1). EAMS REQUESTED AND RECEIVED A PERMANENT REPAIR IN THE FORM OF ETD2018-170-133016 WHICH PROVISDR C77A2020031800021Gusset · 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 170-65644-001 RH SHEAR SPLICE, P/N 170-60257-001 FR90 RH IB GUSSET, AND P/N 170-60261-001 FR9SDR C77A2020031800020Splice · 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 170-65644-001 RH SHEAR SPLICE, P/N 170-60257-001 FR90 RH IB GUSSET, AND P/N 170-60261-001 FR9SDR C77A2020031800019Door Sill · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED ON THE FOLLOWING FORWARD WET AREA FLOOR STRUCTURE: RH SILL P/N 170-05661-003, RH FLOOR DOUBLER P/N 170-05663-003, LH SILL P/N 170-03275-005. REFERENCE ETD2018-170-132553 FIGURE 1 FOR THE DAMAGE LOCATIONS ANDSDR C77A2020031800018Doubler · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED ON THE FOLLOWING FORWARD WET AREA FLOOR STRUCTURE: RH SILL P/N 170-05661-003, RH FLOOR DOUBLER P/N 170-05663-003, LH SILL P/N 170-03275-005. REFERENCE ETD2018-170-132553 FIGURE 1 FOR THE DAMAGE LOCATIONS ANDSDR C77A2020031800017Door Sill · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED ON THE FOLLOWING FORWARD WET AREA FLOOR STRUCTURE: RH SILL P/N 170-05661-003, RH FLOOR DOUBLER P/N 170-05663-003, LH SILL P/N 170-03275-005. REFERENCE ETD2018-170-132553 FIGURE 1 FOR THE DAMAGE LOCATIONS ANDSDR C77A2020031800014Gusset · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING AFT WET AREA FLOOR STRUCTURE: LH PANEL SUPPORT P/N 170-86139-005, LH FR87 SPLICE P/N 170-65644-001, FR90 RH OB GUSSET P/N 170-60259-001. REFERENCE ETD2018-170-133043 FIGURE 1, ETD2018-170-133216 SDR C77A2020031800011Shear Tie · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON TWO SHEAR CLIPS IN THE 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 AFT CARGO SSDR C77A2020031800010Shear Tie · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON TWO SHEAR CLIPS IN THE 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 AFT CARGO SSDR C77A2020031700007Tube · chafedDURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED CHAFE DAMAGE ON THE MOVABLE SHAFT TUBE, P/N 170-83123-001, WHICH IS PART OF THE FORWARD PASSENGER DOOR FORWARD ARM ASSEMBLY, P/N 170-83000-417 (REF ETD2018-170-132516, FIGURE 1). THE CHAFE DAMAGE WAS BLENDED SMSDR C77A2020031800023Seal Rest · corrodedFORWARD CARGO CUTOUT, AFT SEAL REST REST HAS CORROSION AS MARKED.WORK ORDER 2450172273SDR C77A2020031800009Beam · corrodedDURING BASIC CHECK IN BNA, INSPECTION DISCOVERED CORROSION IN A FASTENER HOLE LOCATED IN THE FORWARD SERVICE DOOR LOWER BEAM (REF ETD2018-170-132950, FIGURE 1). EAMS REQUESTED AND RECEIVED ETD2018-170-132950 FOR A PERMANENT REPAIR BY BLENDING AND REAMING THE DSDR C77A2018072400002Warning System · false activationSOC RECEIVED ACARS MESSAGE STATING "CABIN HIGH ALT. DECLARED EMERGENCY." CREW ALSO STATED IN ACARS THEY WOULD BE RETURNING TO SEA. SEA OPS NOTIFIED. AC HAS LANDED WITHOUT INCIDENT AND IS BEING GATED. CREW SPOKED WITH SOC AND CP HAS DEPLANED. CABIN O2 MASKS NOTSDR C77A20171124002Wire Harness · chafedCREW REPORTED A LOSS OF IDG 1 AFTER TAKE-OFF. FLIGHT RETURNED TO DEPARTURE, EMERGENCY DECLARED. IDG 2 OIL CAUTION MESSAGE IN FLIGHT. QRH 5.15 COMPLIED WITH. DISCOVERED A CHAFED WIRE HARNESS APPROX. 30 INCHES FROM IDG 2, J2 ON W8 HARNESS CONTACTING FUEL/OILSDR C77A20170216002Rib · crackedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CRACK DAMAGE TO THE UPPER AND LOWER FLANGES OF RT RIB 11A P/N 170-62783-002 AND LT RIB 12A P/N 170-62642-001 ON THE HORIZONTAL STABILIZER. REFERENCE FIGURES 1-3 FOR DAMAGE DSDR C77A20170216001Rib · crackedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CRACK DAMAGE TO THE UPPER AND LOWER FLANGES OF RT RIB 11A P/N 170-62783-002 AND LT RIB 12A P/N 170-62642-001 ON THE HORIZONTAL STABILIZER. REFERENCE FIGURES 1-3 FOR DAMAGE DSDR C77A20170211002Floorbeam · corrodedAFT CABIN FLOOR, RT FLOORBEAM P/N 170-65669-004 HAS CORROSION IN SEVERAL AREAS FROM FRAME 86 - 89. X=23403 -24408, Y= 273. REMOVED AND REPLACED AFT CABIN RT FLOORBEAM IAW SRM 51-41-01 & 51-43-01 PER EO E175-53MR-094 REV 5.SDR C77A20170211001Floorbeam · corrodedAFT CABIN FLOOR, LT FLOORBEAM P/N 170-65669-003, HAS CORROSION IN SEVERAL AREAS FROM FRAME 86 - 89 X=23403 - 24408. Y= -273. REMOVED AND REPLACED AFT CABIN LT FLOORBEAM IAW SRM 51-41-01 & 51-43-01 PER EO E175-53MR-093 REV 3.SDR C77A20170210002Floorbeam · corrodedCORROSION DAMAGE TO THE UPPER FLANGE OF THE FRAME 14 FLOORBEAM. REPAIRED IAW ETD2015-170-016971A.SDR C77A20170209002Gusset · gougedEO E175-52MR-003 WAS ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE R1 DOOR INTERNAL GUSSET PLATE, WHICH WAS DISCOVERED AT A BASIC CHECK. THE ORIGINAL APPROXIMATE GOUGE DIMENSIONS WERE 0.8 INCH X 0.3 INCH TO A MAXIMUM SDR C77A20170209001Crossbeam · corrodedEO E175-53MR-159 WAS RELEASED TO REPAIR CORROSION DAMAGE TO THE UPPER FLANGE OF THE FR17 CROSSBEAM BY CUTOUT AND DOUBLER INSTALLATION IN ACCORDANCE WITH ETD2015-170-016964A. DURING A SUBSEQUENT INSPECTION OF THE AREA DURING BASIC CHECK AT EAMS, NEW CORROSION ASDR C77A20170207001Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE TO THE FWD CABIN FLOOR STRUCTURE RT SEAT TRACK P/N 170-03263-001 AT THE FR14 CROSS BEAM. THE APPROXIMATE DAMAGE DIMENSIONS ARE 1.8 INCHES X 1.2 INCHES X 0.028 SDR C77A20161219003Warning Light · illuminatedIN FLIGHT THE CREW RECEIVED A CARGO FWD FIRE SYSTEM FAIL EICAS MESSAGE. AN EMERGENCY WAS DECLARED AND THE FLIGHT PERFORMED AN AIR RETURN TO DEPARTURE.SDR C77A20161031003Wire Harness · faultedDURING DESCENT, THE CREW RECEIVED A FLAP/SLAT FAIL MESSAGE AT 4000 FT. DECLARED AN EMERGENCY AND MANAGED TO GET A NO SLAT/FLAP FAIL MESSAGE PRIOR TO LANDING. THE FLIGHT LANDED SAFELY. MAINTENANCE TROUBLESHOT AND FOUND LEFT OTBD NR 4 SLAT HARNESS AT FAULT. R &SDR C77A20160816002Uplock · failedNLG UNCOMMANDED DOWN WITH NO ABNORMAL EICAS INDICATION. R & R NOSE LANDING GEAR UPLOCK IAW AMM 32-32-03. OPS TEST OF LANDING GEAR EXTENSION & RETRACTION SYSTEM PERFORMED IAW AMM 32-33-01. OPS CHECKED GOOD.SDR C77A20160718002Landing Gear · malfunctionedAFTER GEAR RETRACTION, NOSE GEAR MADE CONTINUOUS BANGING NOISE WITH LANDING GEAR INDICATION TURNING AMBER AT SAME TIME. RETURNED HANDLE TO GEAR DOWN POSITION. THREE GREEN INDICATIONS. CREW REPORTING UNABLE TO RETRACT NOSE GEAR AFTER DEPARTURE. ALL GEARS SHOWSDR C77A20160713002Compressor · odorDURING FLIGHT, THERE WAS AN ODOR OF BURNING PLASTIC. THE AIRCRAFT DIVERTED AND AN EMERGENCY WAS DECLARED. FOUND PROBLEM TO BE CAUSED BY POTABLE WATER SYSTEM AIR COMPRESSOR.SDR C77A20151026003Actuator · inoperativeON DECENT NOTICED NO PITCH TRIM INDICATION, DISCOUNTED AP, UPON DISCONNECTION OF AP, RECEIVED AP FAIL & PITCH TRIM FAIL EICAS MSG. PERFORMED QRH CH S 3.3 & 7.16, FAULT REMAINED. UPON LANDING RECEIVED FLT CTRL DISPATCH & STALL PROT FAULT MSG. PERFORMED FIM TSDR C77A20150521001Battery · dischargedL1 FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT BATTERY IAW CMM 25-60-02. OPERATIONS CHECKED GOOD.SDR C77A201503050021Skin · corrodedCORROSION ON FUSELAGE SKIN INNER SURFACE AT AFT CARGO COMPARTMENT BETWEEN FRAME 80 & 81, STATION 21446 & OTBD SIDE OF STRINGER 28R. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213041M3 IAW 15-170-017453 & EA E175-53-485 REV IR WO 1834666SDR C77A201503050019Retainer · corrodedCORROSION ON WATER SERVICE ACCESS PAN FWD RETAINER, PN 170-86656-001 & AFT RETAINER, PN 170-86657-001, BETWEEN STATION 21263 & 21675, STRINGER 27L - 29L. PERMANENTLY REMOVED THE WATER PAN RETAINERS ON WO 6213151L3 IAW EO E17X-5300-004 REV IR ON WO 694208.SDR C77A201503050020Retainer · corrodedCORROSION ON WASTE SERVICE ACCESS PAN FWD RETAINER, PN 170-86654-003, AFT RETAINER, PN 170-86655-003, BETWEEN STATION 22270 & 22680, STRINGER 24R - 26R. PERMANENTLY REMOVED THE WATER PAN RETAINERS ON WO 6213151L3 IAW EO E17X-5300-004 REV IR ON WO 694208.SDR C77A20150305019Retainer · corrodedCORROSION ON WATER SERVICE ACCESS PAN FWD RETAINER, PN 170-86656-001, AFT RETAINER, PN 170-86657-001, BETWEEN STATION 21263 & 21675, STRINGER 27L - 29L. PERMANENTLY REMOVED THE WATER PAN RETAINERS ON WO 6213151L3 IAW EO E17X-5300-004 REV IR ON WO 694208.SDR C77A20150305018Skin · corrodedAFT CARGO COMPARTMENT BILGE SKIN HAS CORROSION AROUND RIVETS BETWEEN FRAME 77 - 78 & BETWEEN STRINGER 29L - 29R, X=20007 - 20387. REMOVED CORROSION BY BLENDING IAW SRM 51-10-03 & 51-12-01. MATERIAL LOSS IS WITHIN LIMITS IAW SRM 53-23-01 ON WO 14358891S8.SDR C77A20150305017Seal Depressor · corrodedAFT CARGO DOOR LOWER CTR SEAL DEPRESSOR, PN 170-85251-401, HAS CORROSION X=20242.0 - 20950.7, STRINGER 27R. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01. MATERIAL LOSS IS WITHIN LIMITS IAW SRM 53-21-11 ON WO 14751831F4.SDR C77A20150305016Upper Sheet · corrodedAFT CABIN RT UPPER SHEET, PN 170-86101-001 HAS CORROSION BETWEEN FRAME 85 & 86, X= 23041 - 23453, Y=260.4. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213171J4 IAW ETD 015-170-016788 & EO E175-5300-100 REV IR WO 1834035.SDR C77A20150305015Upper Sheet · corrodedAFT CABIN LT UPPER SHEET, PN 170-86101-001, HAS CORROSION BETWEEN FRAME 85 & 86, X= 23041 - 23453, Y= -260.4. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213171H6 IAW ETD 2015-170-016788 & EO E175-5300-100 REV IR WO 134035.SDR C77A20150305014Panel · corrodedAFT CABIN RT SHEAR PANEL, PN 170-91919-001, HAS CORROSION BETWEEN FRAME 87 & 88, X= 23865, FROM Y= 304.8 - 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.SDR C77A20150305013Panel · corrodedAFT CABIN FLOOR CTR SHEAR PANEL, PN 170-65928-001, HAS CORROSION BETWEEN FRAME 87 & 88, X= 23865, FROM Y= -222.3 - Y= 222.3. 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.SDR C77A20150305012Panel Support · corrodedAFT CABIN CROSS FRAME 87, RT OTBD FLOOR PANEL SUPPORT, PN 170-66797-001, HAS CORROSION AT FRAME 87, X= 23865, Y=711.2. 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.
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