N605CZ
Service difficulty reports not matched to an aircraft · 91
They name N605CZ, 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 = 'N605CZ' 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 = 'N605CZ' 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 C77A2019022600002Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE LH IB SEAT TRACK AT THE FR18 CROSSBEAM IN THE FORWARD CABIN FLOOR STRUCTURE. THE BEAM WILL BE REPAIRED BY CUTOUT ASDR C77A2019022600001Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE UPPER FLANGE OF THE FR84 CROSSBEAM IN THE CABIN FLOOR STRUCTURE OF THE CENTER FUSELAGE III. THE DAMAGE MEASURES SDR C77A2019022500001Rib · 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, REINFORCESDR C77A2020030400011Doubler · corrodedPANEL 192 BL HAS LIGHT SURFACE CORROSION AROUND SCREW HOLES WORK ORDER 2473505619SDR C77A2020030400010Doubler · corrodedPANEL 192 CR POSSIBLE CORROSION ON DOUBLER AS MARKED.WORK ORDER 2473505616SDR C77A2020030400009Floorbeam · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING FORWARD WET AREA
FLOOR STRUCTURE: LH FLOOR SILL P/N 170-03275-005, LH FLOOR SUPPORT P/N 170-13633-001,
LH FLOOR SILL P/N 170-05662-001, LH CENTER FLOOR BEAM P/N 170-07298-003.
REFERENCE ETD201SDR C77A2020030400008Door Sill · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING FORWARD WET AREA
FLOOR STRUCTURE: LH FLOOR SILL P/N 170-03275-005, LH FLOOR SUPPORT P/N 170-13633-001,
LH FLOOR SILL P/N 170-05662-001, LH CENTER FLOOR BEAM P/N 170-07298-003.
REFERENCE ETD201SDR C77A2020030400007Floor Support · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING FORWARD WET AREA
FLOOR STRUCTURE: LH FLOOR SILL P/N 170-03275-005, LH FLOOR SUPPORT P/N 170-13633-001,
LH FLOOR SILL P/N 170-05662-001, LH CENTER FLOOR BEAM P/N 170-07298-003.
REFERENCE ETD201SDR C77A2020030400006Door Sill · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS FOUND ON THE FOLLOWING FORWARD WET AREA
FLOOR STRUCTURE: LH FLOOR SILL P/N 170-03275-005, LH FLOOR SUPPORT P/N 170-13633-001,
LH FLOOR SILL P/N 170-05662-001, LH CENTER FLOOR BEAM P/N 170-07298-003.
REFERENCE ETD201SDR C77A2020030400005Floor Splice · 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 170-12118-001 FLOOR DOUBLER, P/N 170-05663-001 RH FLOOR SILL, P/N 170-12114-001 RH FLOOR SDR C77A2020030400004Door Sill · 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 170-12118-001 FLOOR DOUBLER, P/N 170-05663-001 RH FLOOR SILL, P/N 170-12114-001 RH FLOOR SDR C77A2020030400003Doubler · 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 170-12118-001 FLOOR DOUBLER, P/N 170-05663-001 RH FLOOR SILL, P/N 170-12114-001 RH FLOOR SDR C77A2020030400002Upper Sheet · 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 170-86101-001 LH UPPER SHEET AND P/N 170-86139-005 LH PANEL SUPPORT. REPLACEMENT OF PARTS WILSDR C77A2020030400001Panel 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 170-86101-001 LH UPPER SHEET AND P/N 170-86139-005 LH PANEL SUPPORT. REPLACEMENT OF PARTS WILSDR C77A2018062100001Actuator · failedCREW RECEIVED A NR 2 ENGINE CONTROL FAULT MESSAGE DURING DESCENT. DECLARED AN EMERGENCY. ENGINE PULL BACK TO IDLE FOR LANDING. LANDED SAFELY AND TAXIIED OFF RUNWAY. NR 2 ENGINE CONTROL FAULT EICAS MESSAGE DURING LANDING AT IDLE THRUST. REMOVED THE SLAVE SDR C77A20170502002Engine · faultedDURING LANDING, THE CREW SLOWED TO 210KTS, CAUSING THRUST TO REDUCE TO IDLE, ONCE AT IDLE A NR 2 ENGINE CONTROL FAULT MESSAGE APPEARED. THE CREW RAN THE QRH AND THE ENGINE WAS UNRESPONSIVE AND WAS STABLIZED IN AN IDLE. DECLARED AN EMERGENCY. A SINGLE ENGINE LASDR C77A20170414008Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CTL I RT LATERAL SEAT TRACK P/N 170-92568-005 AND THE FWD FUSELAGE RT LATERAL SEAT TRACK P/N 170-20956-001. DAMAGE DETAILS AND DIMENSIONS ARE SHOWN IN FIGSDR C77A20170414007Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CTL I RT LATERAL SEAT TRACK P/N 170-92568-005 AND THE FWD FUSELAGE RT LATERAL SEAT TRACK P/N 170-20956-001. DAMAGE DETAILS AND DIMENSIONS ARE SHOWN IN FIGSDR C77A20170414006Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CTL I LT LATERAL SEAT TRACK P/N 170-92570-005 AND THE FORWARD FUSELAGE LT LATERAL SEAT TRACKS P/N 170-20955-001 AND P/N 170-26859-001. DAMAGE DETAILS AND SDR C77A20170414005Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CTL I LT LATERAL SEAT TRACK P/N 170-92570-005 AND THE FORWARD FUSELAGE LT LATERAL SEAT TRACKS P/N 170-20955-001 AND P/N 170-26859-001. DAMAGE DETAILS AND SDR C77A20170414004Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CTL I LT LATERAL SEAT TRACK P/N 170-92570-005 AND THE FORWARD FUSELAGE LT LATERAL SEAT TRACKS P/N 170-20955-001 AND P/N 170-26859-001. DAMAGE DETAILS AND SDR C77A20170414002Rib · crackedCRACKED ON THE UPPER FLANGE OF RIB 12A IN THE RT HORIZONTAL STABILIZER. REPAIRED IAW ETD2017-170-031205A FIGURE 1SDR C77A20170414001Skin · damagedLH HORIZONTAL STABILIZER UPPER SKIN PANEL, REAR AND MID SPAR BETWEEN RIBS 8-14, AND STRINGERS 4 AND 8 DAMAGED. REPAIRED IAW ETD2017-170-031190, FIGURES 1 THROUGH 5.SDR C77A2017041102Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH PERMANENT REPAIRS OF CORROSION AND GOUGE DAMAGE TO THE CENTER FUSELAGE I FLOOR STRUCTURE LT INBOARD SEAT TRACK P/N 170-67358-007 AND RT INBOARD SEAT TRACK P/N 170-67861-005. ACCOMPLISHMENT OF THIS TSDR C77A20170411001Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH PERMANENT REPAIRS OF CORROSION AND GOUGE DAMAGE TO THE CENTER FUSELAGE I FLOOR STRUCTURE LT INBOARD SEAT TRACK P/N 170-67358-007 AND RT INBOARD SEAT TRACK P/N 170-67861-005. ACCOMPLISHMENT OF THIS TSDR C77A20170406004Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CENTER FUSELAGE III LT LATERAL SEAT TRACK P/N 170-65917-005 AND RT LATERAL SEAT TRACK P/N 170-65917-006. DAMAGE DETAILS AND DIMENSIONS ARE SHOWN IN FIGURESDR C77A20170406003Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CENTER FUSELAGE III LT LATERAL SEAT TRACK P/N 170-65917-005 AND RT LATERAL SEAT TRACK P/N 170-65917-006. DAMAGE DETAILS AND DIMENSIONS ARE SHOWN IN FIGURESDR C77A20170406002Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CENTER FUSELAGE I FIRST CLASS SEAT TRACKS P/N 171-01734-003 AND P/N 171-02362-001. DAMAGE DETAILS AND DIMENSIONS ARE SHOWN IN FIGURES 1-4. THE PERMANENT RSDR C77A20170406001Seat Track · gougedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF GOUGE DAMAGE TO THE CENTER FUSELAGE I FIRST CLASS SEAT TRACKS P/N 171-01734-003 AND P/N 171-02362-001. DAMAGE DETAILS AND DIMENSIONS ARE SHOWN IN FIGURES 1-4. THE PERMANENT RSDR C77A20161122001Battery · inoperativeR1 FA JUMPSEAT FLASHLIGHT INOPERATIVE. R & R THE BATTERY IAW AMM 31-51-01. OPS CHECKED GOOD. OK FOR SERVICE.SDR C77A20161108001Motor · shortedDURING FLIGHT (ABOUT 15 MINUTES FROM SEA) THE CREW RECEIVED A STAB LOCK FAULT EICAS MESSAGE. THEY HAVE DECLARED AN EMERGENCY AND WILL BE LANDING IN PDX. PDX HAS BEEN NOTIFIED AND WAS ASSIGNED A GATE. AN FCND WAS RECEIVED UPON LANDING AND THE AIRCRAFT TAXIEDSDR C77A20161024001Battery Pack · inoperativeFLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 33-51-01. OPS CHECKED GOOD.SDR C77A20160108002Outflow Valve · malfunctionedPRESN AUTO FAIL. CABIN PRESS DROP. COMPLIED WITH QRH, MSG CLEARED. PRESS RETURNED TO NORM, IN DESCENT. DEFERED IAW MEL 21-31-01-1A. TRANSFERRED TO SDI & PLACARD INSTALLED. OK FOR SERVICE. MEL 21-31-01-1A CAT C. R & R OUTFLOW VLV IAW AMM 21-31-02. OPERSDR C77A20150515006Wire · brokenCAPTAINS FLASHLIGHT LED IS NOT ILLUMINATING. DEFERRED CAPTAINS FLASHLIGHT IAW MEL 25-62-07-1. TRANSFERRED TO SDI AS DMI DM1907904 & PLACARD INSTALLED, OK FOR SERVICE, MEL 25-62-07-1 CAT C. SPLICED BROKEN WIRES TO CAPTAINS FLASHLIGHT ASSEMBLY IAW SWPM 20-41-SDR C77A20150505019Floor Support · corrodedFORWARD MAIN CABIN LT FLOOR ANGLE PN 170-14731-001 HAS CORROSION AT FRAME 14 , X= 4270 Y= -736.6. R & R LT FLOOR PANEL ANGLE SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 14966272H4 IAW EO E170-5300-106 REV IR WO 1900761.SDR C77A20150505018Door Sill · corrodedFORWARD MAIN CABIN FLOOR LT FWD SILL PN 170-03275-005 HAS CORROSION AT FRAME 16, X= 4711 Y=-1219.2. R & R RT FWD FLOOR SILL IAW SRM 51-41-01 & 51-43-01 ON WO 14966272G5 IAW EO E170-5300-106 REV IR WO 1900761.SDR C77A20150505017Doubler · corrodedFORWARD MAIN CABIN FLOOR LT FWD DOUBLER PN 170-12118-001 HAS CORROSION AT FRAME 16, X= 4711 BETWEEN Y=-330.2 - -914.4. R & R RT FLOOR DOUBLER IAW SRM 51-41-01 & 51-43-01 ON WO 14966272G6 IAW EO E170-5300-106 REV IR WO 1900761.SDR C77A20150505016Floor Support · corrodedFORWARD MAIN CABIN RT FLOOR PANEL SUPPORT PN 170-13939-001 HAS CORROSION AT FRAME 14, X= 4270, Y= 736.6. R & R RT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 14966272H5 IAW EO E170-5300-106 REV IR WO 1900761.SDR C77A20150505015Floor Support · corrodedAFT CABIN RT FLOOR SUPPORT PN 170-66797-001 HAS CORROSION AT FRAME 87, RBL 28, X= 23865 Y= 863. R & R RT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 14966222K1 IAW EO E170-5300-106 REV IR WO 1900248.SDR C77A20150505014Floor Support · corrodedAFT CABIN RT PANEL SUPPORT PN 170-92908-001 HAS CORROSION AT FRAME 84, RBL 35 - 46, X= 22847 Y= 943-116. R & R RT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 14966222K5 IAW EO E170-5300-106 REV IR WO 1900248.SDR C77A20150505013Door Sill · corrodedAFT CABIN LT AFT PANEL SUPPORT, SILL, PN 170-86139-005 HAS CORROSION BETWEEN FRAME 88 & 90, LBL 41". X= 24048 - 24868, Y= -947. R & R LT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 14966222J6 IAW EO E170-5300-106 REV IR WO 1900248.SDR C77A20150505012Support Angle · corrodedAFT CABIN RT FLOOR SUPPORT ANGLE PN 170-60287-002 HAS CORROSION 4 INCHES AFT OF FRAME 90, RBL11, X= 24560, Y= 260. R & R RT FLOOR SUPPORT ANGLE IAW SRM 51-41-01 & 51-43-01 ON WO 14966222L1 IAW EO E170-5300-106 REV IR WO 1900248.SDR C77A20150505011Gusset · corrodedAFT CABIN RT OTBD GUSSET PLATE PN 170-60259-001 HAS CORROSION AT FRAME 90, RBL22, X= 24868, Y= 559. R & R RT OTBD GUSSET IAW SRM 51-41-01 & 51-43-01 ON WO 14966222K3 IAW EO E170-5300-106 REV IR WO 1900248.SDR C77A20150505010Gusset · corrodedAFT CABIN LT OTBD GUSSET PLATE PN 170-60261-001 HAS CORROSION AT FRAME 90, LBL 21" X=24868, Y= -489. R & R LT OTBD GUSSET IAW SRM 51-41-01 & 51-43-01 ON WO 14966222I6 IAW EO 5300-106 REV IR WO 1900248.SDR C77A20150505008Gusset · corrodedAFT CABIN LT INBD GUSSET PLATE PN 170-60257-001 HAS CORROSION AT FRAME 90, LBL 11", X= 24868, Y= -260. R & R LT INBD GUSSET IAW SRM 51-41-01 & 51-43-01 ON WO 14966222I8 IAW EO E170-5300-106 REV IR WO 1900248.SDR C77A20150505009Gusset · corrodedRIGHT INBD GUSSET PLATE HAS CORROSION AT FRAME 90, RBL 11. X= 24868, Y= 260. R & R RT INBD GUSSET IAW SRM 51-41-01 & 51-43-01.SDR C77A20150505007Panel · corrodedAFT CABIN LT SHEAR PANEL PN 170-65927-007 HAS CORROSION AT FRAME 87 BETWEEN LBL 12" - LBL 41" . X=23865.0, Y= -304.8- -1041.4. R & R LT SHEAR PANEL IAW SRM 51-41-01 & 51-43-01 ON WO 14966222I8 IAW EO E170-5300-106 REV IR WO 1900248.SDR C77A20150505006Panel · corrodedAFT CABIN CTR SHEAR PANEL PN 170-65928-001 HAS CORROSION AT FRAME 87, BETWEEN LBL 10" - RBL 10", X=23865.0, Y= -222.3 - 222.3. R & R CTR SHEAR PANEL IAW SRM 51-41-01 & 51-43-01 ON WO 14966222J2 IAW EO E170-5300-106 REV IR WO 1900248.SDR C77A20150505005Panel · corrodedAFT CABIN RT SHEAR PANEL PN 170-91919-001 HAS CORROSION BETWEEN FRAMES 87 - 88, RBL 12 TO 41, X= 23865.0 - 24048.0, Y= 304.8 - 1041.4. R & R RT SHEAR PANEL IAW SRM 51-41-01 & 51-43-01 ON WO 14966222J8 IAW EO E170-5300-106 REV IR WO 1900248.SDR C77A20150505004Upper Sheet · corrodedAFT CABIN LT UPPER SHEET PN 170-86101-001 HAS CORROSION BETWEEN FRAMES 85 - 86, LBL 11". X= 23041 - 23453, Y= -260. R & R LT UPPER SHEET IAW SRM 51-41-01 & 51-43-01 ON WO 14966222I9 IAW EO E170-5300-106 REV IR WO 1900248.
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