N219CY
Service difficulty reports · 109
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 = 'N219CY' 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 = 'N219CY' 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 ABXA20230828179Pressure Valve · faultyAT FL340 CABIN ALT EICAS MESSAGE AND DISCRETE LIGHT ILLUMINATED AND STAYED ON UNTIL DESCENT TO 13,000. CREW DECLARED AN EMERGENCY AND OXYGEN MASKS WERE USED. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT FURTHER INCIDENT. MAINTENANCE GROUNDED AIRCRAFT. MAINTSDR ABXA20230824178Unknown · unknownCABIN ALT WARNING AT FL340 CABIN WAS AT 10,000 ZERO RATE OF CLIMB, DIFFERENTIAL AT 6 PSI. RT PACK INDICATED 27 PSI- LEFT 0 PSI. DESCENDS TO FL300 CABIN INDICATED 9500 FT. ALL OTHER INDICATIONS DID NOT CHANGE. IT TOOK APPROX 45 MINUTES FOR DIFF TO CLIMB TO 7 PSSDR ABXA20230809156Unknown · unknownAIRCRAFT BLOCKED OUT AND DURING TAXI THE FLIGHT CREW WAS NOTIFIED THAT THE LOG BOOK HAD AN OPEN ENTRY FOR THE MAIN CARGO DOOR REINSPECT. THE AIRCRAFT RETURNED TO BLOCK AND MAINTENANCE PERFORMED MAIN CARGO DOOR REINSPECT AND VERIFIED THE DOOR WAS CLOSED AND LOCSDR ABXA20230807154Unknown · unknownINFLIGHT MAIN CARGO DOOR INDICATION ILLUMINATED DURING CLIMB OUT OF CVG. FLIGHT CREW ELECTED TO RETURN TO CVG. AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE PLACED ON D.I. IAW MEL 52-71-1-2 MBCB 8-14-23 PLACARD ISDR ABXA20230803153Unknown · unknownAIRCRAFT DEPARTED SKBO. AT ABOUT 2000Z AT FL240 WE GOT A MASTER WARNING ASSOCIATED WITH A “MN CARGO DOOR” DISCRETE LIGHT. WE RAN THE QRH AND RETURNED TO BOG. THE CABIN PRESSURIZATION GAVE NO INDICATION OF AN OPEN DOOR AND THE DISCRETE LIGHT WENT OUT ON APPROACSDR ABXA20230726151Unknown · unknownBLEED ISLN VALVE EICAS MSG AFTER PUSH-BACK. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND LH ISOL VALVE LOCKOUT PIN IN THE LOCKED DETENTS. ROTATED LOCK PIN TO UNLOCK DETAIN AND FOUND SYSTEM TO OPERATE NORMAL IAW B767 AMM 36-11-04. AIRCRSDR ABXA20230622122Unknown · unknownCABIN HEAT FWD/AFT/CABIN INOP CAME ON AFTER ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE BITE CHECKED ZONE TEMP CONTROLLER IAW B767 21-61-00 NO MESSAGES PRESENT. ALL FAULTS ON EICAS CLEARED. A/C REMAINS ETOPS 180. AIRCRAFT RETUSDR ABXA20230615121Unknown · unknownNOTICED A L ENG EGT OVERTEMP OF 657 DURING PUSHBACK PRIOR TO ENGINE START. CONTACTED MAINTENANCE CONTROL AND ADVISED TO RETURN TO GATE. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET INDICATION PER FIM 71-05 FAULT TREE 810. OKAY TO CONTINSDR ABXA20230515100Web · crackedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED LH WING L/E BULLNOSE WEB (BEAM) AT APPROX. OSS 679.82 (AT FUEL PANEL) IS CRACKED. THE B767-300 SRM 57-41-13 FIG. 201 REPAIR 3 IS FOR THIS SPECIFIC AREA. THE REFERENCED SRM REPAIR IS FOR THE CSDR ABXA20230515102Nose Cowl · wornDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE FOUND THAT NO. 2 INLET, (BULKHEAD ASSY.) LOWER CHORD (314T4013-17) HAVE WEAR MARK ON THE INBOARD AND OUTBOARD SIDE (AT THE GROOVE). THE INBOARD SIDE HAS MATERIAL LOSS OF 0.015” AND OUTBOARD SIDE HAS MSDR ABXA20230515106Pivot · corrodedDURING C21 IN HAECO AMERICAS C21 MAINTENANCE CHECK. DURING ACCOMPLISHMENT OF T/C ABX-55-552-00-01, MAINTENANCE DISCOVERED CORROSION DAMAGE AT TWO FASTENER HOLES COMMON TO THE RIGHT HAND AFT HORIZONTAL STABILIZER PIVOT FITTING AND SPLICE STRAP. SUBJECT HOLES WESDR ABXA20230516108Support · corrodedDURING C21 IN HAECO AMERICAS C21 MAINTENANCE CHECK. HAECO NR 22798 - LH HAND REAR SPAR HYD LINE SUPPORT FOR CLAMP BLOCK IS CORRODED.REMOVED AND REPLACED -13 BRKT IAW BAC DWG 272T1338 REV "A". SUPPORT FABRICATED PER BAC DWG 272T1338 REV "A"SDR ABXA20230515105Vapor Barrier · damagedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE FOUND NO. 1 PYLON OUTBOARD VAPOR BARRIER WEB APPROXIMATELY AT NAC STA. 230 DAMAGED AT THE D4044J MOUNT (CUTOUT). THE D4044J MOUNT WAS PULLED-OUT FROM THE WEB. THE SUBJECT BARRIER IS SUBJECT TO SB-767-SDR ABXA20230516107Pin · failed inspDURING C21 IN HAECO AMERICAS C21 MAINTENANCE CHECK WHILE PERFORMING JOB CARD FOR MCD PIN INSPECTION IT WAS DICOVERED THAT PINS #1,3.6 AND 7 FAILED DIMENSIONAL CHECK.. REMOVED AND REPLACED MCD LATCH CAM PINS OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED PER B767SDR ABXA20230515104Elevator · damagedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED R/H TRAILING EDGE ELAVATOR HAS DAMGE DUE TO IMPACT TO LIFT. REPAIRED IMPACT DAMGE ON R/H ELEVATOR O/B T/E WITH 350 DEGREE CARBON GRAPHITE DOUBLER WITH CORE REPAIR IAW B767-300 51-40-02, 55-20SDR ABXA20230515103Panel · damagedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED THAT THE NO. 2 PYLON AFT HYDRAULIC BAY CLOSE UP PANEL (313T3381-212) HAS NUMEROUS DAMAGES. SINCE THERE ARE AREAS HAVE MULTIPLE AND HEAT DAMAGES, MAINTENANCE OPTED TO REPLACE THE OUTER SKIN ANSDR ABXA20230515101Splice Plate · corrodedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED CORROSION DAMAGE ON THE LH WING OUTBOARD UPPER SPLICE PLATE (114T0223-19), APPROXIMATELY AT OSS 630.945. (2) RIVETS WERE REMOVED PER B767-300 SRM 51-40-02. THE DAMAGE WAS BLENDED PER SRM 51-2SDR ABXA2023051599Skin · corrodedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, AIRCRAFT MAINTENANCE DISCOVERED (2 EA.) AREAS OF CORROSION ON THE LOWER OUTER SKIN PANEL (P/N 113T3143-3) OF THE LEFTWING OUTBOARD FLAP ASSEMBLY (P/N 113T3100-77, S/N 000664) CURRENTLY INSTALLED ON AIRCRAFT N219CSDR ABXA202209298100Controller · faultedCABIN TEMP CONTROLLERS INDICATED INOP ON EICAS FOR "FWD" , "AFT", AND "FLT DK" ON OVHD PANEL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET CABIN TEMP ZONE CONTROLLER REF AMM 21-61-00 OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2022081882None · noneSTARTING LEFT ENGINE STATUS MESSAGE "L ENG PRV" AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK OF BITE AIR SUPPLY CONTROLLER IAW AMM 36-23-00 OPS CHECK GOOD. NO FAULTS AT THIS TIME. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED SDR ABXA2022072988Cabin Pressure · failedDURING CRUISE FLIGHT AT 28000, THE MASTER WARNING HORN / LITES AND EICAS MESSAGE, CABIN ALT WAS ON. CABIN ALT WAS 11,000. WE SWITCHED FROM CONTROLLER 2 TO 1. HAD A STATUS MESSAGE "CABIN ALT AUTO2/CAB. CREW DESCENDED TO 10,000 FEET AND DECLARED AN EMERGENCY. AISDR ABXA2022060564None · noneCARGO FIRE "B" INDICATOR LIGHTS "6" & "8" AMBER ILLUMINATED. CREWMEMBER VISUALLY INSPECTED CARGO COMPARTMENT AND VERIFIED NO SMOKE OR FIRE. THE CREW DECIDED TO DIVERT AND LAND AT NEAREST AIRPORT (CYYR) AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED OVERWEIGHT WSDR ABXA2022010301None · noneAPU BLEED VALVE CYCLED CLOSED AND REMAINED IN THE COLSED POSITION WHEN AC PACKS WERE TURNED OFF ON ENGINE START CHECKLIST, APU BLEED POWER CONTROL C/B OPENED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE RESET APU BLEED CONTROL C/B SATIS. IASDR ABXA2021219022Floor Support · corrodedDURING C-CHECK AMES TAMPA FACILITY, FWD CARGO FLOOR DECK SUPPORT ANGLE UNDER FLOOR WEB AT I/B SIDE OF POWER DRIVE 6R CORRODED. REMOVED INTERCOSTAL. FOUND ORIG MAT .100", MAT LOSS .018", MAT REMAINING .082". AREA FOUND TO BE OUT OF LIMIT. LOCATED AND DRILLED NESDR ABXA2021215021Floorbeam · corrodedDURING C-CHECK, CORROSION ON FWD CARGO STA 654 FLOOR BEAM UPPER CAP BOTTOM SIDE ARPOUND NUT PLATES LBL 10. REMOVED CORROSION AT FWD CARGO STA 654 FLOOR BEAM UPPER CAP IAW B767-300 SRM 51-10-02. EVALUATED DAMAGE, ORIGINAL MATERIAL THICKNESS IS .102, MAT LOSS ISDR ABXA20200803219Start Valve · bindingRIGHT ENGINE START VALVE WILL NOT OPEN. AIRCRAFT BTB AND GROUNDED. R & R RT ENGINE START VALVE, IAW B-767 AMM 80-11-02. OPERATIONS GOOD. AIRCRAFT RELEASED.SDR ABXA20200803200Pressure Switch · intermittentDURING ENGINE START RIGHT ENGINE OIL PRESSURE DISCRETE LIGHT INTERMITTENT, AICRAFT RETURNED TO GATE WHERE MAINTENANCE GROUNDED AIRCRAFT UNTIL REPAIRED. REMOVED AND REPLACED RT ENGINE LOW OIL PRESSURE WARING SWITCH, PER AMM 79-33-01. OPERATIONAL TEST C/W NO DSDR ABXA20200720128Warning Light · illuminatedMASTER WARNING LIGHT ILLUMINATES DURING CRUISE FLIGHT, NO OTHER INDICATIONS OR EICAS MESSAGES NOTED. AIRCRAFT WAS GROUNDED.SDR ABXA20200716125Latch · unsecureENTRY DOOR SAFETY LATCH POPPED IN FLIGHT CAUSING A FORWARD ENTRY DOOR EICAS MESSAGE. UNABLE TO RE-SECURE LATCH IN FLIGHT. AIRCRAFT WAS GROUNDED.SDR ABXA20200710124Warning Light · illuminatedWHEN RTO SELECTED AUTO BRAKE EICAS MSG AND BRAKE DISCRETE LIGHT ILLUMINATED W/RTO SWITCH ENGAGED. AIRCRAFT WAS GROUNDED.SDR ABXA20190207004Structure · corrodedCORROSION ON THE RIGHT WING TRAILING EDGE LOWER CHORD BETWEEN WING STATIONS 344 AND 433. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA20190203003Nose Rib · crackedA 1.5 INCH CRACK IN THE NOSE RIB ANGLE AT RIGHT WING LEADING EDGE STATION 488. THE NOSE RIB ANGLE WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA20180126001Handle · dirtyTHE LEFT FORWARD ENTRY DOOR WAS EXTREMELY HARD TO ARM. THE ACFT WAS GROUNDED AND THE DOOR LATCH AND LOCK MECHANISM WAS INSPECTED INTERNALLY AND EXTERNALLY IAW AMM 52-12-25. THE ASSEMBLY WAS CLEANED AND A SATISFACTORY OPERATIONAL CHECK OF THE DOOR LATCH AND LOSDR ABXA20171115126Handle · malfunctionedTHE LEFT FORWARD ENTRY DOOR ARMING HANDLE WOULD NOT SEAT AFTER THE DOOR WAS CLOSED. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE EXTERNAL EMERGENCY RELEASE HANDLE WAS RESET, ALLOWING THE INTERIOR ARMING HANDLE TO SEAT. THE CAUSE OF THE ARMING HANDLE NOT SEATSDR ABXA20150528065Computer · malfunctionedFUMES IN COCKPIT AFTER LOSS OF AUTOPILOT. REPLACED FAULTY CTR FLIGHT CONTROL COMPUTER.SDR ABXA20150325033Channel · corrodedTHE RIGHT HORIZONTAL STABILIZER OTBD TE WEDGE REAR SPAR HAS MULTIPLE DOUBLE DRILLED HOLES & CORROSION. REMOVED DAMAGED SECTION OF RT OTBD TE WEDGE. FABRICATED NEW SECTION & REPAIRED DOUBLED IAW SRM 51-70-11. SDR INFO, CORRODED, LEVEL 2, PN 183T1141-6, PART SDR ABXA20150318035Structure · crackedRIGHT WING LE SUPPORT, STATION LES 525 CRACKED. R & R RT WING LE LOWER CHORD IAW SRM 51-40-02. SDR INFO, CRACKED, LENGTH: 0.75" PN 114T2206-6, PART NAME CHORD, SN NSN, STRINGER & WS LOCATION: LES 525. ACFT WAS GNDED.SDR ABXA20150318034Repair · crackedFOUND A CRACK ON RT WING LE STATION 651 ON A PREVIOUS REPAIR OF A STRUT RIB. R & R AIR LOAD RIB LOWER CHORD AT STATION 651 IAW SRM 51-40-02 & DWG 114T2212. SDR INFO, CRACKED, LENGTH 1.2", PN 114T2212-6, PART NAME CHORD, SN N/A, STRINGER & WC LOCATION WS 651.SDR ABXA20130607453Skin · corrodedLOWER FUSELAGE SKIN AT FWD MIDDLE MOUNTING AREA WHERE RADIO ALTIMETER ANTENNA IS SECURED HAS CORROSION. REMOVED CORROSION AT FUSELAGE SKIN REPAIR DOUBLER UNDER FWD MIDDLE RADIO ALTIMETER ANTENNA IAW SRM 51-40-02, AND INSTALLED A NEW REPAIR DOUBLER IAW SRM 53-SDR ABXA20130605440Skin · corrodedCORROSION AT FASTENERS AND AFT SKIN EDGE OF LT WING UPPER SKIN WS 798. REMOVED CORROSION IAW SRM 57-20-01, DETAIL I AREA WAS REPAIRED ON REA NR B657-60562.SDR ABXA20130605439Skin · corrodedCORROSION ON UPPER WING SURFACE ALONG SKIN T/E ABOVE REAR SPAR FROM INBD EDGE OF OTBD AILERON TO APPROX WS 990.5. REMOVED CORROSION IAW SRM 57-20-01, DETAIL I. WS LOCATION FROM 912 TO 1008; ACFT WAS GROUNDED.SDR ABXA20130605438Skin · corrodedCORROSION ON LT UPPER WING SURFACE LOCATED AT REAR SPAR APPROX WBL 710. REMOVED CORROSION IAW SRM 57-20-01, DETAIL I AREA WAS REPAIRED ON ABX REA NR B657-60562-MR; ACFT WAS GROUNDED.SDR ABXA20130531454Skin · gougedFORWARD UPPER TCAS ANTENNA MOUNTING AREA HAS SCRATCHES AND GOUGES IN THE FUSELAGE. R & R DOUBLER IAW REA B653-60557-MR, ACFT WAS GROUNDED.SDR ABXA20130528448Stiffener · corrodedR1 DOOR FWD CUTOUT SILL HAS CORROSION. R & R R1 DOOR FWD CUTOUT SILL STIFFENER IAW SRM 51-40-02 AND DWG 141T8313. CORR LEVEL 2. ON ACFT: FROM DOOR STA 79 TO DOOR STA 86; ACFT WAS GROUNDED.SDR ABXA20130528442Skin · dentedOUTWARD DENT STA 1654-1678 ABOVE S36L. DENT IS OUT OF LIMITS, REPAIRED IAW SRM 53-00-01 FIG 201, REPAIR 6, ACFT WAS GROUNDED.SDR ABXA20130528441Skin · dentedOUTWARD DENT, STA 1654-1678, S32R-S33R. DENT IS OUT OF LIMITS, REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 6; ACFT WAS OUT OF LIMITS AND GROUNDED.SDR ABXA20130524451Splice Plate · corrodedSTRINGER 39, SPLICE PLATE HAS SURFACE CORROSION AT END. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FABRICATED NEW SPLICE IAW SRM 53-00-03. ACFT WAS GROUNDED.SDR ABXA20130524450Web · corrodedFLOOR WEB PANEL CORRODED AROUND SCREW HOLES. FABRICATED NEW WEB IAW ENGINEERING DWG 143T5010. ACFT WAS GROUNDED.SDR ABXA20130523446Support Channel · corrodedR1 DOOR CUTOUT CENTER LOWER SILL HAS CORROSION IN SEVERAL PLACES. R & R R1 DOOR CUTOUT CENTER LOWER SILL SUPPORT CHANNEL IAW SRM 51-40-02 AND DWG 141T8313. CORROSION LEVEL 2, ACFT WAS GROUNDED.SDR ABXA20130521449Panel · corrodedLOWER CARGO STRESS PANEL STA 1129-1351 HAS CORROSION AT 2 SPOTS AT EDGE. BLENDED AND CHECKED LIMITS (OUT OF LIMIT) FABRICATED NEW PANEL, TREATED, PRIMED, PAINTED, AND REASSEMBLED IAW SRM 53-60-53, DETAIL III, B767-300 PRINT, SRM 51-20-01, SRM 51-40-02 LBL20 L
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