N761CX
Service difficulty reports · 209
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 = 'N761CX' 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 = 'N761CX' 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 IXXA2024111301Frame · crackedR/H 1809.5 BULKHEAD FWD OUTER CHORD INBOARD FLANGE IS CRACKED AT FASTENER HOLE JUST ABOVE HORIZ STAB PIVOT PIN FITTINGSDR IXXA20240915064Engine · faultedWHILE CLIMBING THROUGH 31,000 FEET CREW REPORTED A LOUD BANG SUSPECT FROM RH ENGINE FOLLOWED BY A VIBRATION, RISE IN EGT AND LOSS OF ENGINE POWER. FOLLOWING ATI QUICK REFERENCE HANDBOOK COMPLIANCE, THE CREW SECURED RIGHT ENGINE, DECLARED AN EMERGENCY LANDING WSDR IXXA20240528035Escape Reel · unwanted deployPOST FLIGHT CREW REPORTED SUBSEQUENT TO HARD LANDING, INERTIAL REELS IN SUPERNUMERARY DEPLOYED. NO ADDITIONAL FAULTS NOTED. CONDITIONAL INSPECTIONS PHASE 1A AND 1B HARD LANDING INSPECTIONS SATISFACTORY PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 05-51-30. DEFERSDR IXXA20240528034Escape Reel · unwanted deployPOST FLIGHT CREW REPORTED SUBSEQUENT TO HARD LANDING, INERTIAL REELS IN SUPERNUMERARY DEPLOYED. NO ADDITIONAL FAULTS NOTED. CONDITIONAL INSPECTIONS PHASE 1A AND 1B HARD LANDING INSPECTIONS SATISFACTORY PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 05-51-30. DEFERSDR IXXA20240528033Escape Reel · unwanted deployPOST FLIGHT CREW REPORTED SUBSEQUENT TO HARD LANDING, INERTIAL REELS IN SUPERNUMERARY DEPLOYED. NO ADDITIONAL FAULTS NOTED. CONDITIONAL INSPECTIONS PHASE 1A AND 1B HARD LANDING INSPECTIONS SATISFACTORY PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 05-51-30. DEFERSDR IXXA2023112731079Unknown · unknownAFTER TAKE OFF, CREW REPORTED A LOUD POP FOLLOWED BY A RUSH OF AIR AND BODY DUCT LEAK EICAS MESSAGE DISPLAY. THE APU BLEED VALVE WAS TURNED OFF. ALTERNATIVELY, THE CENTER ISOLATION VALVE WOULD NOT CLOSE AND THE DUCT LEAK INDICATION FAILED TO CLEAR. ADDITIONALSDR IXXA20231031079Unknown · unknownAFTER TAKE OFF, CREW REPORTED A LOUD POP FOLLOWED BY A RUSH OF AIR AND BODY DUCT LEAK EICAS MESSAGE DISPLAY. THE APU BLEED VALVE WAS TURNED OFF. ALTERNATIVELY, THE CENTER ISOLATION VALVE WOULD NOT CLOSE AND THE DUCT LEAK INDICATION FAILED TO CLEAR. ADDITIONALSDR IXXA20230922066Plate · crackedPOST FLIGHT WALKAROUND, ATI QC IDENTIFIED CRACK ON LEFT WING AFT OF SLAT UNDER SLAT FAIRING INBOARD. REMOVED AND REPLACED INBOARD WING LEADING EDGE SKIN PLATE AT LEFT WING AFT OF INBOARD SLAT UNDER SLAT FAIRING INBOARD IAW B767 SRM 51-40-02.SDR IXXA20230126013None · noneRIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RIGHT ENGINE. AIR TURN BACK WITH EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRESDR IXXA202301276013Engine · faultedRIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RT ENGINE. AIR TURN BACK WITH EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUSDR IXXA20230121001Fitting · crackedBRACKET ABOVE DENSITOMETER IN L/H MAIN TANK, RIB 4 FOUND TO BE CRACKED.SDR IXXA2022090801Fitting · corrodedLEFT WHEEL WELL FITTING CORRODEDSDR IXXA2022090701None · corrodedSEAL RETAINER CORRODEDSDR IXXA2022090301Rub Strip · bentPYLON PANEL 441AT RUB STRIP BENTSDR IXXA2022090201Support · corrodedVERTICAL STAB LH AFT TE PANEL SUPPORT CORRODEDSDR IXXA2022083103None · corrodedAUTFLOW VALVE CAGE CORRODEDSDR IXXA2022083101Support · crackedFAIRING SUPPORT FRAME CRACKEDSDR IXXA202208241Flap · corrodedFLAP CORROSIONSDR IXXA2022090703Thrust Reverser · cracked#2 ENGINE, AFT SIDE OF I/B REVERSER, BELOW AND, AFT OF IDG ACCESS DOOR. WHERE LOWER SIDE CORE COWLING SITS ON THRUST REVERSER. RUB STRIP IS CRACKED ABOUT 3 INCHES AND, HAS DENT IN TRAILING EDGE.SDR IXXA2022090702Skate Angle · crackedLW #1 PYLON AFT STINGER FAIRING 437DB I/B AFT WING TO FAIRING SUPPORT ANGLE T/E CRACKEDSDR IXXA2022091301None · noneLEFT MLG BODY HAS DELAMINATIONSDR IXXA2022083102None · corrodedLEFT WHEEL WELL UPPER SURFACE OFF REAR SPAR FITTING WHERE THE DOG BONE FITTING ATTACHES TO REAR SPAR FITTING CORROSION UNDER HARDWARE BOLT.SDR IXXA20220630120Eicas · fault messageAT FL 300, FWD EQPT VALVE EICAS MESSAGE DISPLAYED. CREW COMPLIED WITH ATI QRH CHECKLIST, AND LIGHT REMAINED ANNUNCIATED. AFTER SEVERAL MINUTES CREW NOTED A LOSS PRESSURIZATION AND EQUIPMENT COOLING CB POPPED OVRD DURING DESCENT. DIVERSION TO KILN WITH A DECLASDR IXXA20191109021Unknown · faultedIN CRUISE VIA AIRLINK, CREW REPORTS POSSIBLE FUEL LEAK FROM LEFT MAIN TANK, UNABLE TO COMPENSATE, FUEL LEAK IS NOT INTERNAL, 2900LBS FUEL IN-BALANCE, UNABLE TO CONTROL WITH CROSSFEED. AS A PRECAUTIONARY MEASURE, AIR TURN BACK TO KPHX WITH AN EMERGENCY DECLARATSDR IXXA20161007077Torque Tube · bentCREW REPORTED THE MAIN CARGO DOOR LIGHT AND WARNING HORN SOUND ANNUNICATED AS AIRCRAFT PASSED THROUGH 19,000 FT. CREW DECLARED AN EMERGENCY. QRA PROCEDURE. NO LOSS OF CABIN PRESSURIZATION. AIR TURN BACK. INSPECTION AFTER LANDING NOTED MAIN CARGO DOOR WAS CLOSESDR IXXA20161003073Angle · crackedANGLE AT BS 1843 AFT SIDE OF FIRE WALL HAS SEVERAL CRACKS AT LBL 10 AND RBL 10. REMOVED AND REPLACED ANGLE IAW SRM 51-70-11. ACFT GROUNDED.SDR IXXA20161003072Stringer · chafedRRCA HYDRAULIC HOSE INSIDE VERTICAL STABILIZER STRINGER 3R DAMAGED IN TWO PLACES. REPAIRED VERTICAL STABILIZER STRINGER IAW SRM 65-30-03. ACFT GROUNDED.SDR IXXA20161004074Support · corrodedLEFT WING TRAILING EDGE UPPER AFT PANEL SUPPORT AT BS 400 CORRODED. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-02. AIRCRAFT GROUNDEDSDR IXXA20160920070Firewall · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. APU FIRE WALL FORWARD SIDE HAS SEVERAL CRACKS AT VERTICAL STIFFENERS, ACCESS 313AL. APU FIREWALL FORWARD SIDE WEB CRACKS REPAIRED IAW SRM 53-80-30, FIG 201, REPAIR 1, DWG 353T0400, IAW 47233REA01.SDR IXXA20160920069Angle · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 AFT STRUT TOP ANGLE JUST FORWARD OF MOUNTING FLANGE 437DB IS CRACKED. R & R TOP ANGLE JUST FORWARD OF MOUNT FLANGE 437 DB.SDR IXXA20161003071Structure · corrodedCORROSION ON THE LEFT WING TRAILING EDGE SUPPORT STRUCTURE UPPER CHORD JUST FORWARD OF THE NR 6 SPOILER IN BOARD FORWARD CORNER. CORROSION ON THE LEFT WIN TRAILING EDGE SUPPORT STRUCTURE UPPER CHORD FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH SRM 57-51-02. NESDR IXXA20160920065Skin · dentedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT FUSELAGE EXTERNAL SKIN HAS A DENT AT STA 1794, S37R. REPAIRED AFT FUSELAGE EXTERNAL SKIN AT STATION 1794 IAW 47233, REA 04 & SRM 53-00-01.SDR IXXA20160920067Gusset · chafedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 PYLON UNDER 431AT FORWARD CORNERS ON SKIN CHAFED. R & R FORWARD CORNER GUSSETS ON NR 1 PYLON UNDER 431AT IAW SRM 51-40-02, PARA 5 AND 7.SDR IXXA201609200066Longeron · corrodedACFT GROUNDED FOR HEAVY MAINTENANCE. FUSELAGE STA 1046-1049, & 1055, RT BUTT LINE 95 ON TOP OF OVER WING LONGERON IS CORRODED. REMOVED ANGLE AND FASTENERS, BLENDED, CORROSION REA 47233, REA 02, COMPLETED IN AREA BLENDED. REINSTALLED ANGLE AND FASTENERS IAW SDR IXXA20160920068Beam · chafedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 PYLON OTBD HYDRAULIC BAY LOWER BEAM IS CHAFED VERY THIN AT FORWARD END. R & R LOWER BEAM IN NR 1 OTBD HYDRAULIC BAY IAW SRM 51-40-02, SECTION 5, PARA B AND SECTION 7, PARA D.SDR IXXA20160512026Skin · corrodedCORROSION LT UPPER WING AT STATION 1075.2, TEMPORARY REPAIR OF LT WING SKIN AT STATION 1090 IAW 46971REA28. PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C CHECK IAW 46971REA28 STEP 9 REFERENCE ATI COI 47257.SDR IXXA20141113033Unknown · unserviceableNUMBER 5 EMER DESCENT DEVICE EXTENDED & UNSERVICEABLE. R & R NR 5 EMER DESCENT DEVICE IAW AMM 25-61-03.SDR IXXA20141113032Unknown · unserviceableNUMBER 4 EMER DESCENT DEVICE EXTENDED & UNSERVICEABLE. R & R NR 4 EMER DESCENT DEVICE IAW AMM 25-61-03.SDR IXXA20150115016Skin · corrodedLEFT HORIZONTAL STAB CORROSION ON TOP SURFACE AT REAR SPAR 16, 108 INCHES FROM FUSELAGE, RS STATION 24 - 26.15 & 127.25 - 129.5 ABOVE REAR SPA. REPAIRED IAW REPAIR EO 47120REA08. INBOUND BLEND ACCOMPLISHED IAW EO 47120REA08.SDR IXXA20150115012Rib · corrodedPANEL 652HB REAR SPAR TO TE RIB UPPER & LOWER CHORDS CORRODED AROUND NUTPLATES. R & R LOWER CHORD IAW SRM 51-40-02.SDR IXXA20150115011Rib · corrodedPANEL 661AB REAR SPAR TO TE ATTACH RIB UPPER CHORD CORRODED AROUND NUTPLATE WS 435. R & R TE UPPER RIB CHORD IAW SRM 51-40-02 & REA 47120REA04.SDR IXXA20150115009Attach Fitting · corrodedUPPER TE PANEL ATTACH CHORD CORRODED AROUND NUTPLATE AS SEEN THRU PANEL 652CB OPENING. R & R TE CHORD IAW SRM 51-40-02.SDR IXXA20150115004Beam · corrodedREAR SPAR TO TE PANEL ATTACH BEAM AT WS 285 UPPER CHORD CORRODED AROUND NUTPLATES. UPPER PANEL ATTACH CHORD WAS FABRICATED REA 47120REA03 & REPLACED IAW SRM 51-40-02.SDR IXXA20150115017Intercostal · corrodedHINGED PANEL 651XB HAS CORROSION AROUND NUTPLATE. REMOVED CORROSION BEYOND LIMITS. NEW INTERCOSTAL FABRICATED. INSTALLED TO PANEL 651XB IAW SRM 51-40-02.SDR IXXA20150115008Attach Fitting · corrodedPANEL 652CB AFT ATTACH CHORD SPLIT ON EDGE. R & R AFT ATTACH CHORD AT PANEL 652GB IAW SRM 51-40-2.SDR IXXA20150115015Attach Fitting · corrodedTRAILING EDGE PANEL 652EB ATTACH FITTING CORRODED AROUND NUTPLATE. R & R TE PANEL 652EB ATTACH FITTING IAW SRM 51-40-02.SDR IXXA20150115006Attach Fitting · corrodedAFT UPPER WING PANEL ATTACH CHANNEL CORRODED AROUND NUTPLATES AS SEEN THRU PANEL 651TB. R & R WING PANEL ATTACH CHANNEL IAW SRM 51-40-02 & REA 47120REA02.SDR IXXA20150115005Attach Fitting · corrodedHINGED PANEL 651TB REAR SPAR TO TE OTBD ATTACH CHANNEL SPLIT ON EDGE. R & R ATTACH CHANNEL FOR HINGED PANEL 651TB REAR SPAR TO TE OTBD IAW SRM 51-40-02.SDR IXXA20150115014Bulkhead · corrodedNOSE WHEEL BULKHEAD FWD FACE WL 170, RBL 25 CHORD CRACKED. REMOVED DAMAGE SECTION OF CHORD & REPAIRED AREA IAW SRM 51-70-12.SDR IXXA20150115013Bulkhead · corrodedNOSE WHEEL BULKHEAD FWD FACE WL 170, LBL 25 CHORD CRACKED. REMOVED DAMAGE SECTION OF CHORD & REPAIRED AREA IAW SRM 51-70-12.
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