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.
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
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 C77A20151013014Floor Support · corrodedEXFOLIATION CORROSION ON AFT CABIN, RT FLOOR PANEL SUPPORT PN 170-66797-001 ON CROSS FRAME 87, Y=+736.6, X=23865, Y= +736. R & R CROSS FRAME 87, RT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 19451482G5 IAW EO E175-5300-125 REV IR WO 1965342.SDR C77A20151013013Floor Support · corrodedCORROSION ON AFT CABIN, LT FLOOR PANEL SUPPORT PN 170-92907-001, ON CROSS FRAME 84, Y=-1066.8, X=22847, Y= -1066. R & R CROSS FRAME 84, LT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 19451482E4 IAW EO E175-5300-125 REV IR WO 1965342.SDR C77A20151013012Panel · corrodedEXFOLIATION CORROSION ON AFT CABIN FLOOR, CTR SHEAR PANEL PN 170-65928-001, BETWEEN FRAME 87 - 88, FROM Y=-222 THRU Y=+222, X=23865 - 24048, Y= -222 TO +222. R & R AFT CABIN CTR SHEAR PANEL IAW SRM 51-41-01 & 51-43-01 ON WO 19451482F9 IAW EO E175-5300-125 REVSDR C77A20151013011Panel · corrodedEXFOLIATION CORROSION ON AFT CABIN FLOOR, RT SHEAR PANEL PN 170-91919-001, BETWEEN FRAME 87 - 88, FROM Y=+304 THRU Y=+1041, X=23865 - 24048, Y=+1041 TO +304. R & R AFT CABIN, RT SHEAR PANEL IAW SRM 51-41-01 & 51-43-01 ON WO 19451482G3 IAW EO E175-5300-125 REVSDR C77A20151013010Panel · corrodedEXFOLIATION CORROSION ON AFT CABIN FLOOR, LT SHEAR PANEL PN 170-65927-007, BETWEEN FRAME 87 - 88, FROM Y=-304 - Y=-1041.4, X=23865 - 24048, Y= -1041 TO -304. R & R AFT CABIN LT SHEAR PANEL IAW SRM 51-41-01 & 51-43-01 ON WO 19451482E7 IAW EO E175-5300-125 REVSDR C77A20151013009Doubler · corrodedCORROSION ON AFT CABIN, RT FWD FLOOR DOUBLER PN 170-92856-001, AT FRAME 84, Y=+330, X=22847, Y= +330. R & R AFT CABIN, RT FWD FLOOR DOUBLER IAW SRM 51-41-01 & 51-43-01 ON WO 19451482G8 IAW EO E175-5300-125 REV IR WO 1965342.SDR C77A20151013008Splice · corrodedCORROSION ON AFT CABIN, RT FLOOR SPLICE PN 170-65644-001, BETWEEN FRAME 87 - 88, Y=+1041.4, X=23865 - 24048, Y= +1041. R & R AFT CABIN, RT FLOOR SPLICE IAW SRM 51-41-01 & 51-43-01 ON WO 19451482G2 IAW EO E175-5300-125 REV IR WO 1965342.SDR C77A20151013007Upper Sheet · corrodedCORROSION ON AFT CABIN FLOOR, RT UPPER SHEET PN 170-86101-001, BETWEEN FRAME 85 - 86. R & R AFT CABIN RT UPPER SHEET IAW SRM 51-41-01 & 51-43-01.SDR C77A20151013006Upper Sheet · corrodedEXFOLIATION CORROSION ON AFT CABIN FLOOR, LT UPPER SHEET PN 170-86101-001, BETWEEN FRAME 85 - 86, Y=-260.4, X=23041 - 23453, Y= -260. R & R AFT CABIN LT UPPER SHEET IAW SRM 51-41-01 & 51-43-01 ON WO 19451482E5 IAW EO E175-5300-125 REV IR WO 1965342.SDR C77A20151013005Floor Support · corrodedCORROSION ON FWD CABIN FLOOR, LT PANEL SUPPORT PN 170-14734-001 AT FRAME 18 Y=-749.3, X=5323, Y= -749. R & R CROSS FRAME 18, LT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 19451471E3 IAW EO E175-5300-124 REV IR, WO 1965353.SDR C77A20151013004Floor Support · corrodedCORROSION ON FWD CABIN FLOOR, LT FLOOR PANEL SUPPORT PN 170-13633-001 AT FRAME 16 Y=-1140, X=4711, Y= -1140. R & R CROSS FRAME 16, LT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 19451471E3 IAW EO E175-5300-124 REV IR, WO 1965353.SDR C77A20151013003Support Angle · corrodedFORWARD CABIN FLOOR, RT SUPPORT ANGLE PN 170-04075-001 ON FRAME 14 Y=+711.2 HAS CORROSION, X=4270, Y= +711. R & R CROSS FRAME 14, RT FLOOR PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WO 19451471D2 IAW EO E175-5300-124 REV IR, WO 1965353.SDR C77A20151013002Door Sill · corrodedCORROSION ON FWD CABIN FLOOR LT FWD SILL PN 170-03275-005, AT FRAME 16 Y=-1149, X=4711, Y= -1149. R & R LT FWD SILL IAW SRM 51-41-01 & 51-43-01 ON WO 19451471E4 IAW EO E175-5300-124 REV IR WO 1965353.SDR C77A20151013001Door Sill · corrodedFORWARD CABIN FLOOR, RT FWD SILL PN 170-05663-003, BETWEEN FRAME 12 - 14, FROM Y=+914.4 - Y=+1219.2 HAS CORROSION ON SEVERAL AREAS, X=3679 - 4270, Y= 914 - 1219. R & R RT FWD SILL IAW SRM 51-41-01 & 51-43-01 ON WO 19451471D1 IAW EO E175-5300-124 REV IR WO 196SDR C77A20151005001Spar · damagedDURING BASIC CHECK, INSPECTION DISCOVERED MIGRATING BUSHINGS PN 171-12123-001 & 171-12122-001 ON THE WING STUB FITTING IN SPAR III AT Y=1118 & -1118. THESE BUSHINGS WERE INSTALLED IAW EO E17X-57MA-004 IAW SB 170-57-0038. VT-SAA REQUESTED A REPAIR & RECEIVED SDR C77A20151004005Floorbeam · corrodedEXFOLIATION CORROSION ON MULTIPLE AREAS OF AFT CABIN RT FLOORBEAM PN 170-65669-004, BETWEEN FRAME 86 - 89, Y=+260.4, X=23453 - 24458, Y= +260. R & R AFT CABIN RT FLOORBEAM IAW SRM 51-41-01 & 51-43-01 ON WO 19451482G4 IAW EO E175-53MR-094 REV 4 WO 1963022.SDR C77A20151004004Floorbeam · corrodedEXFOLIATION CORROSION IN MULTIPLE AREAS OF AFT CABIN LT FLOORBEAM PN 170-65669-003, BETWEEN FRAME 86 - 88, Y=-260.4, X=23453 - 24048, Y= 260. R & R AFT CABIN LT FLOORBEAM IAW SRM 51-41-01 & 51-43-01 ON WO 19451482E6 IAW EO E175-53MR-093 REV 3 WO 498289.SDR C77A20151004003Seat Track · corrodedCORROSION ON MULTIPLE AREAS OF FUSELAGE MAIN CABIN, RT FLOOR TRACK PN 170-03263-01, BETWEEN FRAME 13 - 17, Y=+260.4, X=4011 - 5064, Y= 260. R & R FWD CABIN RT SEAT TRACK IAW SRM 51-41-01 & 51-43-01 ON WO 19451471D8 IAW EO E175-53MR-062 REV 5 WO 1962749.SDR C77A20151004002Seat Track · corrodedCORROSION ON MULTIPLE AREAS OF FWD CABIN LT SEAT TRACK PN 170-03264-001, BETWEEN FRAME 15 - 19, X=4520 - 5645 Y= -260. R & R FWD CABIN LT SEAT TRACK IAW SRM 51-41-01 & 51-43-01 ON WO 19451471E1 IAW EO E175-53MR-061 REV 5, WO 1962745.SDR C77A20151004001Crossbeam · corrodedDURING BASIC CHECK, INSPECTION DISCOVERED CORROSION ON THE AFT CABIN CROSSBEAM FRAME 87, PN 170-86056-003, UPPER FLANGE LOCATED APPROX AT Y=-260.4. REQUESTED A REPAIR & RECEIVED ETD2015-170-091494 WHICH PROVIDES A PERMANENT REPAIR BY INSTALLING A REPAIR NESTESDR C77A20151001002Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE AFT CABIN FLOOR STRUCTURE RT AFT SEAT TRACK PN 170-86082-003 AT FRAME 84. THE APPROX DAMAGE DIMENSIONS ARE AS FOLLOWS, 1.40 INCHES X 1.10 INCHES TO ASDR C77A20151001001Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CROSSBEAM FRAME 14 UPPER FLANGE, REF ETD2015-170-088972A & FIGURES FOR DAMAGE DIMENSIONS & LOCATIONS. BECAUSE THE FLOOR CROSSBEAM FRAME 14 IS PSE & FSDR C77A20150707001Seal Depressor · crackedDURING A TURN ON 06 18 2015, DISCOVERED INCOMING DAMAGE TO THE FWD CARGO, FWD CORNER SEAL REST & LOWER CTR SEAL REST. THE DAMAGE DIMENSIONS ARE THE AS FOLLOWS. CORNER SEAL REST PN 170-66803-401, 2.9 INCHES LENGTH & DENTED TO 0.4 INCH DEEP. THE SUBJECT SEAL SDR C77A20150129001Battery · dischargedFLASHLIGHT BY L1 DOOR INOPERATIVE. R & R L1 FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM 33-51-00. OPERATIONS CHECKED GOOD. OK FOR SERVICE.SDR C77A20140909001Flashlight · inoperativeCAPTAINS EMER FLASHLIGHT WILL NOT ILLUMINATE. REPLACED CAPTAINS FLASHLIGHT IAW AMM.SDR C77A20140207003Fitting · damagedORIGINALLY FOUND DAMAGE TO FWD CARGO DOOR SEAL REST FITTING PN 170-69099-002. ACCOMPLISHED PERMANENT REPAIR BY REPLACEMENT OF FWD CARGO SEAL REST FITTINGS IAW EO E175-53MR-108 REV 2.SDR C77A20140207002Retainer · damagedORIGINALLY FOUND DAMAGE TO FWD CARGO DOOR SEAL RETAINERS PN 170-69777-003. CONTOURED FWD CARGO DOOR SEAL RETAINERS TO ORIGINAL CONFIGURATION IAW SRM II 52-00-02.SDR C77A20140207001Retainer · damagedORIGINALLY FOUND DAMAGE TO FWD CARGO DOOR SEAL RETAINERS PN 170-69776-003 CONTOURED FWD CARGO DOOR SEAL RETAINERS TO ORIGINAL CONFIGURATION IAW SRM II 52-00-02.SDR C77A20131002001Girt Bar · malfunctionedL2 DOOR WILL NOT DISARM. SECURED L2 GIRT BAR IAW AMM 52-12-41. OPS CHECKED GOOD.SDR C77A20130929019Seal · tornRT ENGINE OTBD THRUST REVERSER DRAIN MAST SEAL IS TORN. R & R DRAIN MAST SEAL IAW EO E17X-7800-002.4, REV 1.SDR C77A20130929018Seal · tornRT ENGINE INBD THRUST REVERSER DRAIN MAST SEAL IS TORN. R & R DRAIN MAST SEAL IAW EO E17X-7800-002.3, REV I.SDR C77A20130929014Flap Track · wornLT WING INBD FLAP TRACK NR 5. R & R FLAP TRACK NR 5 IAW AMM 21-51-08.SDR C77A20130929010AFlap Track · wornLEFT WING AFT FLAP INBD FLAP TRACK NR 5 IS WORN OUT OF LIMITS. R & R LT WING INBD AFT FLAP INBD TRACK NR 5 IAW AMM 21-51-08.SDR C77A20130929009Flap Track · wornLT WING AFT FLAP OTBD FLAP TRACK NR 6 WORN OUT OF LIMITS. R & R LT WING INBD AFT FLAP OTBD TRACK NR6 IAW AMM 27-51-08.SDR C77A20130929004Flap Track · wornLT WING FLAP TRACK NR 2 INBD, PN 170-39313-003, WORN OUT OF LIMITS. ACCOMPLISHED PERMANENT REPAIR IAW EA E175-57-169.1 REV IR.SDR C77A20130929017Seal · wornRT ENGINE OTBD THRUST REVERSER FRONT 12 O'CLOCK PLATFORM SEAL IS TORN. REPLACED UPPER SEALS IAW EO E17X-7800-001.4, REV 2.SDR C77A20130929016Seal · wornRT ENGINE INBD THRUST REVERSER FRONT12 O'CLOCK CORE COWL SEAL IS TORN. REPLACED UPPER SEALS IAW EO E17X-7800-001.3, REV 1.SDR C77A20130929015Seal · wornLEFT ENGINE INBD THRUST REVERSER FRONT 12 O'CLOCK PLATFORM SEAL IS TORN. REPLACED UPPER SEALS IAW EO E17X-7800-001.2, REV 3.SDR C77A20130929013Firewall · wornAPU FIREWALL PANEL 351BZ FLANGE IS CRACKED AT TOP AND BOTTOM. REPAIRED IAW ETD 2013-170-0400673-.SDR C77A20130929012Flap Track · wornRT WING FLAP TRACK NR 2A OTBD WORN OUT OF LIMITS THICKNESS REDUCTION D=.017" REF SRM 57-52-03, TABLE 101. ACCOMPLISHED PERMANENT REPAIR IAW EA E175-57-169.2, REV IR.
SDR C77A20130929011Flap Track · wornRT WING FLAP TRACK NR 2 OTBD WORN OUT OF LIMITS THICKNESS REDUCTION D=.015" REF SRM 57-52-03, TABLE 101. ACCOMPLISHED PERMANENT REPAIR IAW EA E175-57-169.2, REV IR.SDR C77A20130929010Flap Track · wornLT WING AFT FLAP OTBD FLAP TRACK NR 6 IS WORN OUT OF LIMITS THICKNESS REDUCTION D=.040" REF SRM 57-53-03, TABLE 101, R & R FLAP TRACK IAW AMM 21-51-08.SDR C77A20130929008Flap Track · wornLT WING FLAP TRACK NR 2A OTBD, PN 170-39321-003, WORN OUT OF LIMITS THICKNESS REDUCTION D=.012" REF SRM 57-52-03, TABLE 101. ACCOMPLISHED PERMANENT REPAIR IAW EA E175-57-169.1, REV IR.
SDR C77A20130929007Flap Track · wornLT WING FLAP TRACK NR 2A INBD, WORN OUT OF LIMITS THICKNESS REDUCTION D=.013" REF SRM 57-52-03, TABLE 101. ACCOMPLISHED THE PERMANENT REPAIR IAW EA E175-57-169.1 REV IR.SDR C77A20130929006Flap Track · wornLT WING FLAP TRACK OTBD WORN OUT LIMITS THICKNESS REDUCTION D=.021" REF SRM 57-52-03, TABLE 101. ACCOMPLISHED THE PERMANENT REPAIR IAW EA E175-57-169.1, REV IR.
SDR C77A20130929005Flap Track · wornLEFT WING FLAP TRACK NR 1A WORN OUT OF LIMITS. R & R LEFT WING INBD FLAP TRACK 1A IAW AMM 57-54-25.SDR C77A20130929003Panel · damagedRACK, 2, SHELF (B)- (9009)- ELONGATED HOLE ON PANEL 516DB. ACCOMPLISHED PERMANENT REPAIR TO LT WING PANEL 516DB DAMAGED FASTENER HOLE IAW EA E175-57-170.SDR C77A20130929002Bushing · migratedNLG ACTUATOR MOUNTING LUG INBD BUSHING MIGRATED. ACCOMPLISHED THE PERMANENT REPAIR OF BUSHING MIGRATION OF THE NLG ACTUATOR IAW EO E17X-3200-007, REV IR.SDR C77A20130929001Bracket · bentRIGHT SLAT, NR 3 SCREW GOUGE ON OTBD UNDER SIDE AT SLAT TRACK AND BENT BRACKET. ACCOMPLISHED PERMANENT REPAIR ON THE RT NR 3 SLAT SKIN AND T/E IAW EA E175-57-171, REV IR, REFER TO WP H4004, SEQ 6501, MAXIMO 737057-602 FOR ALL WORK ACCOMPLISHED.SDR C77A20130927002Threshold · corrodedFWD CARGO LOWER HORIZONTAL BEAM, HAS CORROSION . REPLACED FWD CARGO THRESHOLD BEAM IAW EO E175-53MR-128.
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