N610CZ
Service difficulty reports · 123
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 = 'N610CZ' 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.
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 = 'N610CZ' AND registry_match = 'registration' 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 C77A20170717001Rib · crackedRIB 11A ON THE RT HORIZONTAL STABILIZER CRACKED. REPAIRED IAW DRAWING 170-62400-453,SDR C77A20170504001Slide · unserviceableFOUND SAFETY STRING ON L2 EVACUATION SLIDE BROKEN. R&R L2 EMERGENCY SLIDE IAW AMM-25-65-01. OK FOR SVC.SDR C77A20170109001Diaphragm · damagedDURING REPAIR FOR A L2 DOOR ESCAPE SLIDE INDICATION, THE L2 DOOR ASSIST BOTTLE WAS DEPLETED. R & R THE DIAPHRAM AND SHEAR PIN IAW AMM 52-12-53 SVC'D DOOR ASSIT BOTTLE TO 2000 PSI IAW AMM 52-12-51 AND OPENED RT2210398 TO RECHECK ASSIST BOTTLE PSI IN 24 TO 48 HSDR C77A20161031001Flashlight · inoperativeFWD LEFT FA FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 33-51-01. OK FOR SERVICE.SDR C77A20160712002Power Supply · inoperativeAFT EMERGENCY EXIT LOCATOR INOPERATIVE ON TEST. R & R AFT EMERGENCY EXIT BATTERY IAW AMM 33-50-01. NO FIX. SLAVED LIGHT TO FWD BATTERY. LAMP OPS GOOD. R & R NR 3 EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01, OPS CHECKED GOOD IAW AMM 33-50-00 OPS CHECKED GOSDR C77A20160628004Diaphragm · defectiveTHE L2 DOOR WAS FOUND DIFFICULT TO ARM AND DISARM, THE EVACUATION ESCAPE SLIDE BUSTLE PIN WAS FOUND DETACHED AND PNEUMATIC ASSIST BOTTLE PRESSURE WAS DEPLETED. THE L2 DOOR DIAPHRAGM ASSY WAS REPLACED IAW AMM AND WAS CHARGED. THE EVACUATION SLIDE MECHANISM WASDR C77A20151116002Shutoff Valve · intermittentBLEED 1 FAIL MSG AT FL314. QRH 2.5 COMPLETE, CONDITION PERSISTS. DEFERRED IAW MEL 36-00-00-1, TRANSFERRED TO SDI & PLACARD INSTALLED. ACFT OK FOR SERVICE. REPLACED NR 1 NAPRSOV IAW AMM 36-11-03. OPERATIONS CHECK REQUIRED. DM REMAINS OPEN. PERFORMED A CRSDR C77A20151006001Flashlight · inoperativeFLIGHT ATTENDANT FLASHLIGHT BY R1 DOOR INOPERATIVE. DEFERRED FLIGHT ATTENDANT FLASHLIGHT BY R1 DOOR IAW MEL 25-62-07-1. TRANSFERRED TO SDI, NO MX ACTION REQUIRED. PLACARD INSTALLED. ACFT OK FOR SERVICE, MEL 25-62-07-1 CAT C. R & R FLIGHT ATTENDANT FLASHLISDR C77A20150811004Retainer · corrodedAFT INTERIOR FUSELAGE WASTE CUT OUT DOOR STRUCTURE RETAINERS HAS CORROSION, BETWEEN STATION 22270.0 & 22680.0 & STRINGER 26R. REMOVED & DISCARDED WASTE PAN RETAINERS 170-86654-003 & 170-86655-003 IAW EO-E175X-5300-004.2 WO 1938853.SDR C77A20150811003Retainer · corrodedAFT INTERIOR FUSELAGE WASTE CUT OUT DOOR STRUCTURE RETAINERS HAS CORROSION, BETWEEN STATION 22270.0 & 22680.0 & STRINGER 26R. REMOVED & DISCARDED WASTE PAN RETAINERS 170-86654-003 & 170-86655-003 IAW EO-E175X-5300-004.2 WO 1938853.SDR C77A20150811021Crossbeam · corrodedMAIN CABIN FLOOR STRUCTURE HAS CORROSION AT FRAME 17 & RBL 13 - 42. FOUND DURING OK TO CLOSE. ACCOMPLISHED PERMANENT REPAIR IAW EO E175-53MR-205 REV IR WO 1944007. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSISDR C77A20150811020Panel · corrodedAFT MAIN CABIN, RT SHEAR PANEL PN 170-91919-001, BETWEEN FRAME 87 & 88 FROM Y=11 - Y=41, Z=19.29 HAS CORROSION. REPLACED RT SHEAR PANEL IAW SRM 51-42-01, 51-43-01 & EO E175-5300-119 REV IR WO 1941393.SDR C77A20150811019Gusset · corrodedAFT MAIN CABIN, RT UPPER GUSSET PLATE PN 170-60259-001 AT FRAME 90, Y=23, Z= -19.29. REPLACED RT UPPER GUSSET IAW SRM 51-41-02 & EO E175-5300-119 REV IR WO 1941393.SDR C77A20150811018Panel · corrodedAFT MAIN CABIN, CTR SHEAR PANEL PN 170-65928-001, BETWEEN FRAME 87 & 88 FROM Y=-11 - Y=11, Z=-19.29. REPLACED CTR SHEAR PANEL IAW SRM 51-41-02 & EO E175-5300-119 REV IR WO 1941393.SDR C77A20150811017Panel · corrodedAFT MAIN CABIN, LT SHEAR PANEL PN 170-65927-007, BETWEEN FRAME 87 & 88, Y= -11 - Y=41, Z=19.29. REPLACED LT SHEAR PANEL IAW SRM 51-41-02 & EO E175-5300-119 REV IR WO 1941393.SDR C77A20150811016Support · corrodedAFT MAIN CABIN FLOOR STRUCTURE, LT GALLEY SUPPORT PN 170-86132-003, HAS CORROSION AT FRAME 90, Y=42. REPLACED LT GALLEY SUPPORT IAW SRM 51-41-02 & EO E175-5300-119 REV IR WO 1941393.SDR C77A20150811015Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT AT FRAME 19, Y=-43, Z=-19.29 HAS CORROSION. R & R MAIN CABIN FLOOR SUPPORT PN 170-29704-001 IAW SRM 51-41-02 & EO E175-5300-118 REV IR WO 1941779.SDR C77A20150811014Crossbeam · corrodedFORWARD MAIN CABIN, FRAME 17, CROSSBEAM 170-21769-405, Y= 4, Z= -19.29 HAS CORROSION. REPAIRED IAW EO E175-53 MR-203 REV IR. THIS EO IS ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH PERMANENT REPAIR OF CORROSION DAMAGE IAW ETD 2015-170-071373. BECAUSE THIS ISDR C77A20150811013Door Sill · corrodedFORWARD MAIN CABIN, LT FLOOR SILL PN 170-03275-005 AT FRAME 16, FROM Y= -46 - Y= -49 HAS CORROSION. R & R LT FLOOR SILL IAW SRM 51-41-02 & EO E175-5300-118 REV IR WO 1941779.SDR C77A20150811012Floor Support · corrodedFORWARD MAIN CABIN LT FLOOR SUPPORT PN 170-13633-001 AT FRAME 16, Y= -45, Z=19.29 HAS CORROSION. R & R LT FLOOR SUPPORT IAW SRM 51-41-02 & EO E175-5300-118 REV IR WO 1941779.SDR C77A20150811011Doubler · corrodedFORWARD MAIN CABIN, FLOOR DOUBLER PN 170-12118-001 AT FRAME 16, FROM Y= -13 - Y=36, Z=19.29. R & R DOUBLER SRM 51-41-02 & EO E175-5300-118 REV IR.SDR C77A20150811010Seat Track · corrodedFORWARD MAIN CABIN, LT FLOOR TRACK PN 170-03264-001, BETWEEN FRAME 16 & 19, Y= -11, Z= -19.29 HAS CORROSION IN SEVERAL AREAS. R & R LT SEAT TRACK IAW SRM 51-41-02 & EO E175-53MR-061 REV 5 WO 1939696.SDR C77A20150811009Seat Track · corrodedFORWARD MAIN CABIN, RT FLOOR TRACK PN 170-03263-001, BETWEEN FRAME 17 & 13, Z= -19.29 HAS CORROSION IN SEVERAL AREAS. R & R RT SEAT TRACK IAW SRM 51-41-02 & EO E175-53MR-062 REV 5 WO 1939698.SDR C77A20150811008Door Sill · corrodedFORWARD MAIN CABIN, RT FLOOR SILL PN 170-05661-003, BETWEEN FRAME 17 & 20 FROM Y=31 - Y=38, Z=19.29. R & R RT FLOOR SILL IAW SRM 51-41-02 & EO E175-5300-118 REV IR WO 1941779.SDR C77A20150811007Floor Support · corrodedFORWARD MAIN CABIN FLOOR PANEL SUPPORT PN 170-13939-001 AT FRAME 17, Y= 29:Z=-19.29 HAS CORROSION. R & R MAIN CABIN FLOOR PANEL SUPPORT IAW SRM 51-41-02 & EO E175-5300-118 REV IR WO 1941779.SDR C77A20150811006Crossbeam · corrodedFORWARD MAIN CABIN FRAME 14, CROSSBEAM PN 170-21766-409, BETWEEN Y=13 - Y=36 HAS CORROSION. REPAIRED IAW EO-E175-53 MR-202 REV 1 WO 1941725. THIS EO IS ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH PERMANENT REPAIR OF CORROSION DAMAGE TO THE CROSSBEAM UPPER FSDR C77A20150811005Door Sill · corrodedFORWARD MAIN CABIN RT FLOOR SILL PN 170-05663-003 BETWEEN FRAME 12 & 14, FROM Y=37 - Y=49, Z=19.29. R & R RT FLOOR SILL IAW SRM 51-41-02 & EO E175-5300-118 REV IR WO 1941779.SDR C77A20150811002Mount Bracket · corrodedAFT PAX DOOR, AFT SLIDE FITTING LOWER MOUNT BRACKET HAS CORROSION AROUND NUTPLATE. DURING BASIC CHECK, INSPECTION FOUND THE AFT PAX DOOR SURROUNDING STRUCTURE ANGLE, NUT HOLDER PN 170-85282-401 WITH CORROSION DAMAGE. THE CORROSION DAMAGE MEASURES THE FOLLOWISDR C77A20150811001Seat Track · corrodedPASSENGER CABIN FLOOR SEAT TRACK BETWEEN FRAME 19 - 20, RBL10 IS CORRODED AT UPPER SURFACE. R & R SEAT TRACK 170-03263-001 IAW SRM 51-41-02 & EO E175-53MR-062 REV 5 WO 1939698. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON CONDITION RESDR C77A20150810001Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CROSSBEAM FRAME 17, UPPER FLANGE LOCATED BETWEEN Y=15 & Y=42.7, OTBD OF TRACK Y=11. REFERENCE ETD2015-170-073605B & FIGURES 1 & 2. THE APPROX DAMAGESDR C77A20150806002Seat Track · corrodedDURING BASIC CHECK, INSPECTION DISCOVERED CORROSION DAMAGE ON THE CABIN SEAT TRACKS PN 170-27305-003 & 170-67861-005. PERMANENT REPAIRS BY REPLACEMENT IS ACCOMPLISHED IAW DWG LISTED IN TABLE 2 & SRM CHAPTER 51 PRINCIPLES, REF ATTACHED FIGURES IDENTIFYING THE SDR C77A20150806001Seat Track · corrodedDURING BASIC CHECK, INSPECTION DISCOVERED CORROSION DAMAGE ON THE CABIN SEAT TRACKS PN 170-27305-003 & 170-67861-005. PERMANENT REPAIRS BY REPLACEMENT IS ACCOMPLISHED IAW DWG LISTED IN TABLE 2 & SRM CHAPTER 51 PRINCIPLES, REF ATTACHED FIGURES IDENTIFYING THE SDR C77A20150805005Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CROSSBEAM FRAME 17 UPPER FLANGE, REF ETD2015-170-071373, & FIGURES FOR DAMAGE DIMENSIONS & LOCATIONS, 3.0 INCHES X .50 INCH X .095 INCH. REQUESTED & SDR C77A20150805002Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CROSSBEAM FRAME 14 UPPER FLANGE, REF ETD2015-170-071303A, & FIGURES FOR DAMAGE DIMENSIONS & LOCATIONS, 35 INCHES X .70 INCH TO A MAXIMUM DEPTH OF .047SDR C77A201507300033Floor Support · corrodedAFT CABIN FLOOR SUPPORT HAS CORROSION AT FRAME 87 Y 29, X 23865 Y 737. R & R THE FLOOR SUPPORT IAW SRM 51-41-01 & 51-43-01.SDR C77A20150327003Battery · dischargedL2 FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. DEFERRED IAW MEL 25-62-07-1. TRANSFERRED TO SDI. PLACARD INSTALLED. OK FOR SERVICE. MEL APPLIED, MEL 25-62-07-1 CAT C. L2 FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R L2 FLASHLIGHT BATTERY IAW AMM 33-51-01. SDR C77A20130816004Finger Doubler · corrodedFORWARD CARGO DOOR CUTOUT STRUCTURE AFT FINGER DOUBLER HAS CORROSION AT X= 7505-7685 Y= 280-390. R & R AFT FINGER DOUBLER IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130816003Finger Doubler · corrodedFWD CARGO DOOR CUTOUT STRUCTURE FWD FINGER DOUBLER HAS CORROSION AT X= 6820-7150, Y=290-300. R & R FWD FINGER DOUBLER IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130814005Floorbeam · corrodedCORROSION WAS FOUND ON LT FLOORBEAM SPLICE PLATE AT FR 87 X=23850 Y= -273. R & R LT FLOORBEAM SPLICE IAW SRM 51-41-01 AND 51-43-01.SDR C77A20130814004Floor Support · corrodedFLOOR SUPPORT FROM FRAME 89 TO 90 HAS CORROSION AT X=24434 TO 24867, Y=-273. REMOVED CORROSION IAW SRM 51-10-03 & 51-12-01 IAW ETD 2013-170-028346 AND EO E175-53MR-144, REV 1.SDR C77A20130820026Seal · wornLEFT ENGINE INBD THRUST REVERSER LOWER DRAIN MAST SEAL IS TORN. REPLACED LOWER SEALS BY INCORPORATION OF SB 78-0050 R01 IAW EO E17X-7800-002.2, REV IR.SDR C77A20130820025Seal · wornLEFT ENGINE INBD THRUST REVERSER FRONT 12 O'CLOCK CORE COWL SEAL IS TORN. REPLACED UPPER SEALS BY INCORPORATION OF SB 78-0055 R01 IAW EO E17X-7800-001.2, REV 3.SDR C77A20130820024Seal · wornLT ENGINE INBD THRUST REVERSER FRONT 12 O'CLOCK PLATFORM SEAL IS TORN. REPLACED UPPER SEALS ON WO 736585-411 BY INCORPORATION OF SB 78-0055 R01 IAW EO E17X-7800-001.2, REV 3.SDR C77A20130820023Flap Track · wornRT WING INBD FLAP, NR 2A OTBD TRACK, WORN OUT OF LIMITS THICKNESS REDUCTION D=.014" IAW SRM 57-52-03. BLENDED WORN AREA IAW SRM PART II 51-10-03.SDR C77A20130820022Flap Track · wornLEFT WING INBD FLAP, NR 2 OTBD TRACK, WORN OUT OF LIMITS THICKNESS REDUCTION D=.015" IAW SRM 57-52-03. BLENDED WORN AREA IAW SRM PART II 51-10-03.SDR C77A20130820021Skin · chafedLT PYLON INBD FACE HAS A CHAFE AT THE LOWER FWD CORNER OF THE AFT CUT OUT. BLENDED DAMAGE SMOOTH IAW SRM II 51-10-03.SDR C77A20130820020Wire · damagedEVIDENCE OF ARCING ON AFT RT CENTER OF LICC, FROM CONTACT WITH WIRE W120-01391-20. REPAIRED DAMAGED WIRES W120-01391-20, W120-00975-24W, W120-00975-24BL, W120-00975-240R, W120-01456-24, W120-01392-20 IAW STANDARD WIRING PRACTICES MANUAL 20-41-20.SDR C77A20130820019Nut · looseLOW TORQUE INDICATED ON LT PYLON INBD-AFT PYLON ATTACH BOLT BY LOOSE WASHER AT PYLON LOWER LINK FITTING. REMOVED CASTELLATED NUT, RETORQUED AND SAFETIED IAW EO E17X-5400-001, REV IR.SDR C77A20130820018Nut · looseLOW TORQUE INDICATED ON LT PYLON OTBD AFT ATTACH BOLT. REMOVED CASTELLATED NUT, RETORQUED AND SAFETIED IAW EO E17X-5400-001, REV IR.SDR C77A20130820017Lug · gougedNLG HAS GOUGE ON INBD RETRACT ACTUATOR LUG ON INSIDE BUSHING FLANGE BLENDED DAMAGE SMOOTH IAW SRM 51-10-03 & 51-12-01.
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