N603CZ
Service difficulty reports · 119
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 = 'N603CZ' 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 = 'N603CZ' 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 C77A2020031700040Panel Support · 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: FLOOR DOUBLER P/N 170-12118-001, RH FLOOR SILL P/N 170-05663-003, FR15 FLOOR PANEL SUPPORT P/SDR C77A2019012900001Seat Track · damagedACCOMPLISH REPLACEMENT OF A DAMAGED OR PREVIOUSLY REPAIRED LT FLOOR TRACK P/N 170-03264-001 BETWEEN FRAMES 12 AND 21. THE DAMAGED STRUCTURE WILL BE REPLACED BY USING PRODUCTION DRAWINGS. BECAUSE THE TRACK IS A PSE, ACCOMPLISHMENT OF THIS EO HAS BEEN CLASSIFIEDSDR C77A2019012500001Floorbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE TO THE UPPER FLANGE OF THE CENTER FUSELAGE III RT BEAM P/N 170-65669-004 BETWEEN FR88-89. THE DAMAGE MEASURES APPROXIMATELY 1.186 INCH X 1.038 INCH X 0.042 INCSDR C77A2018072400001Warning System · false activationAT TOP OF CLIMB DISPATCH RECEIVED AN ACARS MESSAGE FROM FLIGHT STATING "BLEED 2 FAIL GOIN 2 10000". THE AC DID HAVE 1 BLEED ALREADY ON DEFERRAL. THE FLIGHT DESCENDED TO FL100 AND SOC RECEIVED THE DL RADIO CALL. MESSAGE HAD CLEARED AND THEY WERE GOING TO ASCENDSDR C77A20171109001Warning Message · false activationSTEERING FAIL MESSAGE WHEN LANDING GEAR EXTENDED FOR LANDING. EMERGENCY WAS DECLARED. AIRCRAFT WAS TOWED TO THE GATE. MX COMPLIED WITH FIM 32-53-00-810-809-A. MESSAGE CLEARED. ACFT OK FOR SERVICE.SDR C77A20170228001Rib · crackedCRACKED LOWER FLANGE OF RIB 12A ON THE RT HORIZONTAL STABILIZER. REPAIRED IAW DRAWING 170-62400-441 AND SRM CHAPTER 5.SDR C77A20160309001Power Unit · dischargedEMERGENCY LIGHT BATTERY FAULT EICAS MSG. CHARGED ELPU IAW AMM 33-50-01. OPERATIONS CHECKED IAW AMM 33-50-01. OK FOR SERVICE.SDR C77A20150624001Battery · dischargedAFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM 33-51-01. OPERATIONS CHECKED GOOD AT THIS TIME.SDR C77A20150430002Flashlight · intermittentFORWARD FLIGHT ATTENDANT EMER FLASHLIGHT CHARGING INTERMITTENTLY. DEFERRED IAW MEL. TRANSFERRED TO SDI IAW MX. PLACARD INSTALLED, OK FOR SERVICE. ON 04 27 2015 R & R L1 FLIGHT ATTENDANT FLASHLIGHT IAW AMM. SDI SIGNED & PLACARD REMOVED.SDR C77A20150317001Seal Rest · corrodedFORWARD CARGO DOOR CUT OUT LOWER CTR SEAL REST HAS CORROSION. REMOVED & REPLACED CTR SEAL REST 170-85251-401 IAW SRM 51-40-01 & 51-40-02 WO 4751881A5 AND IAW EO E175-53MR-108 WO 904050.SDR C77A20150314011Gusset · corrodedAFT MAIN CABIN FUSELAGE CTL III LT UPPER GUSSET PLATE HAS CORROSION AT FRAME 90, Y=-508. R & R LT UPPER GUSSET PLATE 170-60261-001 ON WO 14914431H7 IAW SRM51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO 1841453.SDR C77A20150314010Gusset · corrodedAFT MAIN CABIN FUSELAGE CTL III RT UPPER GUSSET PLATE HAS CORROSION AT FRAME 90, Y=-609.6. R & R UPPER GUSSET PLATE 170-60259-001 ON WO14914431H3 IAW SRM 51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO 1841453.SDR C77A20150314009Splice · corrodedAFT MAIN CABIN FUSELAGE CTL III SPLICE HAS CORROSION AT FRAME 90, Y=-260.4. R & R SPLICE 170-86119-001 ON WO 14914431G4 IAW SRM 51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO1841453SDR C77A20150314008Gusset · corrodedAFT MAIN CABIN FUSELAGE CTL III RT UPPER GUSSET PLATE HAS CORROSION AT FRAME 90, Y=-260.4. R & R RT UPPER GUSSET PLATE 170-60257-001 ON WO 14914431H5 IAW SRM 51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO 1841453.SDR C77A20150314013Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE CROSSBEAM FRAME 90 UPPER FLANGE & SIDES. REF FIGURES 1 -4 FOR CROSSBEAM FRAME 90 DAMAGE BLEND OUT DIMENSIONS. RECEIVED RELIEF IN THE FORM OF ETD 201SDR C77A20150314007Gusset · corrodedAFT MAIN CABIN FUSELAGE CTL III LT GUSSET PLATE HAS CORROSION AT FRAME 90, Y=-260.4. R & R LT GUSSET PLATE 170-60257-001 ON WO 14914431G3 IAW SRM 51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO 1841453.SDR C77A20150314006Panel Support · corrodedAFT MAIN CABIN FUSELAGE CTL III RT PANEL SUPPORT HAS CORROSION BETWEEN FRAME 89 & 90, Y=-939.8 TO 1041.4, R & R RT PANEL SUPPORT 170-86131-001 ON WO 14914431H1 IAW SRM 51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO 1841453.SDR C77A20150314005Splice · corrodedAFT MAIN CABIN FUSELAGE CTL III LT SPLICE HAS CORROSION AT FRAME 89, Y=-260.4. R & R LT SPLICE 170-86107-001 ON WO 14914431G1 IAW SRM 51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO 1841453.SDR C77A20150314004Panel · corrodedAFT MAIN CABIN FUSELAGE CTL III RT SHEAR PANEL HAS CORROSION BETWEEN FRAME 87 & 88, Y=-304.8 TO 1041.4. R & R RT SHEAR PANEL 170-91919-001 ON WO 14914431G8 IAW SRM 51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO 1841453.SDR C77A20150314003Panel · corrodedAFT MAIN CABIN FUSELAGE CTL III CTR SHEAR PANEL HAS CORROSION BETWEEN FRAME 87 & 88, Y=-223.2. R & R CTR SHEAR PANEL 170-65928-001 ON WO 14914431F9 IAW SRM 51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO 1841453.SDR C77A20150314002Upper Sheet · corrodedAFT MAIN CABIN FUSELAGE CTL III RT UPPER SHEET HAS CORROSION BETWEEN FRAME 86 & 85, Y=-260.4. R & R UPPER SHEET 170-86101-001 ON WO 14914431H9 IAW SRM 51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO 1841453.SDR C77A20150314001Upper Sheet · corrodedAFT MAIN CABIN FUSELAGE CTL III LT UPPER SHEET HAS CORROSION BETWEEN FRAME 85 & 86, =-260.4. R & R UPPER SHEET 170-86101-001 ON WO 4914431F7 IAW SRM 51-40-03 & 51-40-02 IAW EO E175-5300-102 REV IR WO 1841453.SDR C77A20150314012Seat Track · corrodedDURING BASIC CHECK, INSPECTION DISCOVERED CORROSION ON THE AFT CABIN RT AFT SEAT TRACK AT FRAME 84, Y260.4. RECEIVED RELIEF IN THE FORM OF ETD 2015-170-022567 WHICH PROVIDES A PERMANENT REPAIR BY INSTALLING A DOUBLER. ENGINEERING HAS CLASSIFIED THIS REPAIR ASSDR C77A20150313011Crossbeam · corrodedCORROSION ON CROSSBEAM FRAME 14 UPPER FLANGE. DAMAGE BLENDED OUT.SDR C77A20150313008Crossbeam · 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 E175-53 MR-067 IAW ETD 2011-170-101290. SDR C77A20150313007Door Sill · corrodedFWD CARGO DOOR CUT OUT FWD LOWER CORNER SEAL REST HAS CORROSION X=8604.4 TO 8843.2, STRINGER 24R TO 26R. R & R FWD CORNER LOWER SEAL REST 170-66803-401 IAW SRM 51-41-02 WO 14751881A4 & EO E175-53 MR-108 WO 904050.SDR C77A20150313006Door Sill · corrodedFORWARD CARGO DOOR CUT OUT FWD LOWER CORNER SEAL REST HAS CORROSION X=8604.4 TO 8843.2, STRINGER 24R TO 26R. R & R FWD CORNER LOWER SEAL REST 170-66803-401 IAW SRM 51-41-02.SDR C77A2015031300006Floor Support · corrodedFORWARD CABIN RT FLOOR SUPPORT HAS CORROSION AT FRAME 16, RBL 28 +711.2. R & R FLOOR SUPPORT IAW SRM 51-41-02.SDR C77A20150313005Door Sill · corrodedFORWARD CABIN RT FLOOR SILL HAS CORROSION BETWEEN FRAME 17 TO 18, RBL 41 TO 49+1041.4 TO +1244.6. R & R FLOOR SILL 170-05661-003 IAW SRM 51-41-02 ON WO 6211852E6 IAW EO E175-5300-103 WO 1839418.SDR C77A20150313004Door Sill · corrodedFORWARD CABIN RT FLOOR SILL IS EXFOLIATED BETWEEN FRAME 12 TO 1, RBL 37 TO 49+939.8 TO +1244.6. R & R FLOOR SILL 170-05663-003 IAW SRM 51-41-02 ON WO 6211852D8 IAW EO E175-5300-103 WO 1839418.SDR C77A20150313003Floor Support · corrodedFORWARD CABIN RT FLOOR PANEL SUPPORT HAS CORROSION BETWEEN FRAME 15, RBL 28+279.4. R & R FLOOR PANEL SUPPORT 170-04071-001 IAW SRM 51-41-02 ON WO 6211852F5 IAW EO E175-5300-103 WO 1839418.SDR C77A20150313002Angle · corrodedFORWARD CABIN RT FLOOR ANGLE HAS CORROSION AT FRAME 14, RBL 28+711.2. R & R FLOOR ANGLE 170-04075-001 IAW SRM 51-41-02 ON WO 6211852F2 & ON WO 1839418 IAW EO E175-530-103.SDR C77A20150313001Floor Support · corrodedFORWARD CABIN RT FLOOR PANEL SUPPORT HAS CORROSION AT FRAME 13, RBL 28+711.2. R & R FLOOR PANEL SUPPORT 170-04071-001 IAW SRM 51-41-02 ON WO 6211852E2 & ON WO 1839418 IAW EO E175-530-103.SDR C77A20150312002Seat Track · corrodedFORWARD CABIN RT SEAT TRACK HAS CORROSION BETWEEN FRAME 13 TO 17, RBL 11+279.4. R & R SEAT TRACK BETWEEN FRAME 12 TO 20 IAW SRM 51-41-02 ON WO 6211852D6 IAW MR-062 WO 411170.SDR C77A20150312001Seat Track · corrodedFORWARD CABIN RT SEAT TRACK HAS CORROSION BETWEEN FRAMES 13 - 17 RBL 11+279.4. R & R SEAT TRACK IAW SRM 51-41-02.SDR C77A2015031200001Floor Support · corrodedAFT CABIN RT FLOOR SUPPORT HAS CORROSION AT FRAMES 86 - 89, Y 260.4. R & R THE FLOOR SUPPORT IAW SRM 51-41-02 & 51-43-01.SDR C77A20140613001Battery · dischargedFLIGHT ATTENDANT FLASHLIGHT AT R1 DOOR INOPERATIVE. R & R BATTERY IAW AMM, OPERATIONS CHECKED NORMAL.SDR C77A20130806001Pin · looseL1 DOOR SLIDE HAS A LOOSE AFT BUSTLE PIN. R & R L1 DOOR SLIDE.SDR C77A20130507002Door · out of adjustPRIOR TO DEPARTURE THE FLIGHT CREW REPORTED THE FWD PASSENGER L1 DOOR SLIDE WOULD NOT ARM. INVESTIGATION FOUND THE DOOR OUT OF ADJUSTMENT. ADJUSTED L1 DOOR IAW AMM 52-11-00 AND OPS CHECKED GOOD.SDR C77A20130507001Power Supply · failedPRIOR TO DEPARTURE THE LT FWD EMERGENCY LIGHT POWER UNIT HAD A FAILED EICAS MESSAGE. R & R FWD LT ELPU AND OPS CHECKED GOOD IAW AMM 33-50-01.SDR C77A20130505018Frame · damagedEVIDENCE OF DRILL MARKS AND DAMAGED RIVET VERIFIED ON LT AFT SIDE OF REAR PRESSURE BULKHEAD ON BULKHEAD ATTACH RING BETWEEN STRINGERS 12L AND 13L. R & R RIVET AND BLENDED OUT DRILL MARK IAW SRM PART II 51-40-01 AND 51-10-03.SDR C77A20130505017Spar · crackedRT WING STUB IN SPAR III FASTNER HOLE SHOWS CRACK INDICATIONS. HOLE DIA IS AT 0.314". REAMED SPAR III AND FITTING TO 0.350" SRM PART II 51-40-02, CRACK INDICATION STILL EXISTS. SPOT FACED SPAR III MATERIAL AT 0.500" NDT AND INSTALLED BUSHING.SDR C77A20130505016Flap Track · wornLEFT WING INBD FLAP TRACK 2 INBD, PN 170-39313-003, WORN OUT OF LIMITS THICKNESS REDUCTION D= .020", REF SRM 57-52-03, TABLE 101. SRM LIMITS: 0.013" BLENDED WORN AREA IAW SRM PART II 51-10-03.SDR C77A20130505015Flap Track · wornLT WING INBD FLAP TRACK NR 2 OTBD,WORN OUT OF LIMITS IAW SRM 57-52-03, TABLE 101. BLENDED WORN AREA IAW SRM PART II, 51-10-03.SDR C77A20130505014Flange · damagedVERTICLE STAB LT SIDE L/E ATTACH FLANGE HAS DRILL/ SCREW DAMAGE, 2ND LT FASTENER HOLE UP FROM FUSELAGE SKIN. ENLARGED THE FASTENER HOLE, REMOVE THE HIGH METAL AND FILL IN VOID WITH SEALANT IAW SRM PART II 51-40-02 AND 51-10-03.SDR C77A20130505013Heat Shield · chafedLT PYLON NR 1 HEAT SHIELD IS CHAFED ON THE T/E. BLENDED SMOOTH THE CHAFED AREA ON UPPER HEAT SHIELD AND FABRICATED DOUBLER AND FILLER IAW SRM II 51-40-02-51.SDR C77A20130505010Seal · wornLEFT ENGINE INBD THRUST REVERSER FRONT 12 O'CLOCK PLATFORM SEAL IS DAMAGED. REPLACED SEALS IAW EO E17X-7800-001.1.SDR C77A20130505012Seal · wornRT ENGINE INBD THRUST REVERSER, FRONT 12 O'CLOCK CORE FIRE SEAL IS TORN. IAW THE EFFECTIVITY OF THESE THRUST REVERSER, THE SEALS REQUIRED ARE NO LONGER MANUFACTURED. REPLACED SEALS.SDR C77A20130505011Seal · wornRT ENGINE OTBD THRUST REVERSER FRONT 12 O'CLOCK CORE FIRE SEAL IS TORN. IAW THE EFFECTIVITY OF THESETHRUST REVERSER, THE SEALS REQUIRED ARE NO LONGER MANUFACTURED, PN 14G0058-202. REPLACED SEALS.SDR C77A20130505009Fitting · gougedLEFT MLG SIDE STAY FWD UPPER ATTACH POINT BUSHING HSG INTERNAL SIDE HAS GOUGE= .020". REMOVED HIGH METAL FROM LT MLG SIDE STAY FWD FITTING BY HAND IAW SRM 51-10-03.
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