N517JB
Service difficulty reports · 98
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 = 'N517JB' 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 = 'N517JB' 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 YENA20160801680Engine · failedEMERGENCY DECLARED, AIR RETURN TO DEPARTURE. CREW PERFORMED A RETURN TO FIELD AFTER ENGINE 2 EXPERIENCED POSSIBLE COMPRESSOR STALL. REPORTED SEVERAL AUDIBLE STALLS ON TAKEOFF FOLLOWED BY VIBRATION AND BURNED RUBBER/METALLIC ODOR IN THE CABIN. ACFT LANDING WASSDR YENA20160514460Relay · failedEMERGENCY DECLARED. LANDING GEAR WOULD NOT EXTEND. PERFORMED L/G GRAVITY EXTENSION. WHEN LOWERING GEAR, GOT LANDING GEAR CONTROL ON LANDING GEAR DISPLAY; PERFORMED TSM 32-31-00-810-808-A. FOUND LANDING GEAR SYS ISOLATION VALVE NOT RECEIVING ANY POWER, 49GA. SDR YENA20160415313Floor Support · corrodedAFT CABIN FLOORBEAM +Y464L AT STR 23R CORRODED AT FRAME 66 F/A SEAT MOUNTS; R & R AFT CABIN FLOORBEAM +Y464L AT STR 23R, FRAME 66 F/A SEAT MOUNTS IAW SRM 51-42-11.SDR YENA20160415312Floor Support · corrodedAFT CABIN FLOORBEAM -1292 , STR 23R AFT TRIPLE BEAM CORRODED NUT PLATE HOLES FROM FRAMES 68-69; R & R AFT CABIN FLOORBEAM FRAMES 68-69, -1292, STR 23R AS REQUIRED IAW SRM 51-42-11.SDR YENA20160415311Floor Support · corrodedAFT CABIN FLOORBEAM 1292R TRIPLE BEAM CORRODED AT SPLICE STR 23R 9" AFT FRAME 68, R & R AFT CABIN FLOORBEAM FRAME 68 -1292 AT STR 23R AS REQUIRED IAW SRM 51-42-11.SDR YENA20160415310Floor Support · corrodedCORROSION FOUND ON AFT CABIN FLOORBEAM -1292, FRAME 66, 18" AFT FRAME 67 AND 2" FWD OF FRAME 68 SPLICE; R & R AFT CABIN FLOORBEAM -1292, STR 23R IAW SRM 51-42-11.SDR YENA20160415309Floor Support · corrodedAFT CABIN FLOORBEAM -Y1292 CENTER TRIPLE BEAM CORRODED AT SPLICE STR 23R 9" FWD FRAME 68; R & R AFT CABIN FLOORBEAM -1292, STR 23R IAW SRM 51-42-11.SDR YENA20160415308Floor Support · corrodedAFT CABIN FLOORBEAM +Y1292L SPLICE AT STR 23L CORRODED AT NUT PLATE HOLES FROM FRAME 66-68; R & R AFT CABIN FLOORBEAM +Y1292 AT STR 23L FROM FRAME 66-68 IAW SRM 51-42-11.SDR YENA20160415307Floorbeam · corrodedAFT CABIN FLOORBEAM +Y1292 AT STR 23L CORRODED 2" AFT FRAME 66; R & R AFT CABIN FLOOR BEAM +Y1292 AT STR 23L 2" AFT OF FRAME 66 IAW SRM 51-42-11.SDR YENA20160415306Floorbeam · corrodedAFT CABIN FLOORBEAM +Y1292L CORRODED AT FRAME 68. R & R THE FLOORBEAM IAW SRM 51-42-11.SDR YENA20160415305Floor Support · corrodedAFT CABIN FLOOR SUPPORT 765R CORRODED AT FRAME 66. R & R FLOOR SUPPOPRT BETWEEN FRAMS 64-66 IAW SRM 51-42-11.SDR YENA20160415304Floor Support · corrodedAFT CABIN FLOOR SUPPORT -765R CORRODED FROM FRAMES 66-68. R & R THE FLOOR SUPPORT IAW SRM 51-42-11.SDR YENA20160415303Floor Support · corrodedAFT CABIN FLOOR SUPPORT CORRODED AT FRAMES 67 - 68. R & R THE FLOOR SUPPORT IAW SRM 51-42-11.SDR YENA20160415302Floor Support · corrodedAFT CABIN FLOOR SUPPORT CORRODED AT FRAME 66. R & R THE FLOOR SUPPORT FROM FRAME 64 TO 66 IAW SRM 51-42-11.SDR YENA20160415301Support · corrodedAFT CABIN SHEAR WEB SUPPORT CORRODED 6 INCHES FWD OF FRAME 70. R & R SHEAR WEB SUPPORT IAW SRM 51-42-11.SDR YENA20160415300Shear Web · corrodedAFT CABIN SHEAR WEB FRAMES 69-70 CORRODED. R & R SHEAR WEB IAW SRM 51-42-11.SDR YENA20160415299Floor Support · corrodedCABIN FLOOR SUPPORT +254 HAS SPOTS OF CORROSION BETWEEN FRAMES 16-20; R & R THE FLOOR SUPPORT.SDR YENA20160415298Shear Web · corrodedAFT CABIN SHEAR WEB CORRODED FROM FRAME 69-70. R & R SHEAR WEB IAW SRM 51-42-11.SDR YENA20160415297Support · corrodedAFT CABIN SUPPORT CORRODED 6 INCHES FWD OF FRAME 70 AND 16 INCHES AFT FRAME 69. R & R.SDR YENA20160415296Floorbeam · corrodedLEFT CABIN FLOORBEAM 1292 HAS CORROSION AT FRAME 20. R & R THE FLOORBEAM IAW SRM 51-42-11.SDR YENA20160415295Floorbeam · corrodedAFT CABIN FLOORBEAM +Y919L CORRODED AT FRAME 66. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-14-283-002. R & R THE FLOORBEAM IAW SRM 51-42-11, PG 1-6 & 51-72-11, PG 1-6.SDR YENA20160415294Floorbeam · corrodedCABIN FLOORBEAM 254 HAS CORROSION AT FRAME 20. R & R THE FLOORBEAM IAW SRM 51-42-11.SDR YENA20160415293Floorbeam · corrodedAFT CABIN FLOORBEAM -464 RT CORRODED AT FRAME 66. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-14-283-002. R & R THE FLOORBEAM IAW SRM 53-72-11, PG 1-4.SDR YENA20160415292Floorbeam · corrodedRIGHT CABIN FLOORBEAM Y-254 AND Y- 81 HAS CORROSION AT FRAME 12. R & R CABIN FLOORBEAM IAW SRM 51-7 & 51-42-11.SDR YENA20160415291Floor Support · corrodedCABIN FLOOR SUPPORT Y-503.4 HAS CORROSION AT FRAME 16. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11, AND SRM 51-42-11.SDR YENA20150709260Switch · malfunctionedRETURNED TO DEPARTURE, VHF 1 AND 2 EMMITING. R & R F/O PTT SWITCH IAW AMM 27-92-41, OPS CHECK GOOD.SDR YENA20150107002Bushing · wornDIVERTED, ACFT EXPERIENCE VIBRATION CLIMBING 15,000 FT- 25,000 FT, NO ENGINE ISSUES OR OTHER SYS ISSUES. VIBRATION RETURNED ON FINAL APPROACH DURING DIVERSION. SPEED TAPE REMOVED AND PANEL RESECURED NO DEFECT NOTED. DURING MAINTENANCE PERFORMED TSM 05-50-008SDR YENA20141005218Skin · corrodedDURING HEAVY MAINTENANCE, FOUND CORROSION OF THE RT WING TOP SKIN AT RIB 7A. REPAIRED THE WING SKIN IAW E/C A14-605-01.SDR YENA20141005217Skin · corrodedDURING HEAVY MAINTENANCE CHECK, LT WING TOP SKIN FOUND CORRODED AT RIB 7. REPAIRED IAW E/C A14-604-01.SDR YENA20141004213Frame · crackedDURING HEAVY MAINTENANCE, FUSELAGE FRAME SPLICE 47 HAS AN 18 INCH CRACK INDICATION AT STRINGER 5R-7R REAMED HOLES UP TO DIAMETER, PERFORMED ROTO TEST INSPECTION IN THE AFFECTED HOLES. REPORT BACK EDGE MARGINS FOR ALL LOCATIONS, SPECIFY IF THE CRACKS ARE STILLSDR YENA20131106227Wire Harness · damagedDURING MAINTENANCE CHECK, FOUND ROW 1 ACFT LT EMERGENCY PATH LIGHT INOPERATIVE. R & R EMERGENCY PATH HARNESS AT ROW 1 ACFT LT AMM 33-51-00.SDR YENA20130202031Rod · lack of lubeFLT 6411 MCO-TPA, ON HEAVY MAINTENANCE CHECK FOUND R1 DOOR GOES FROM DISARMED TO ARMED WITH DOOR OPEN. ADJUSTED ESCAPE SLIDE CONTROL IAW AMM 52-11-00. LUBED SPRING ROD OF ESCAPE SLIDE CONTROL MECHANISM AS PER AMM 12-22-52. OPS CHECK NORMAL.SDR YENA20120219443Control Panel · failedFLT 772, FLIGHT CREW REPORTED THAT CABIN EMERGENCY EXIT LIGHTS REMAINED ON WITH EMERGENCY EXIT SWITCH IN THE OFF POSITION. REMOVED AND REPLACED FORWARD ATTENDANT PANEL PER MM 23-73-12. OPS TESTED GOOD.SDR YENA20101111150Unknown · odorFLT 702 SJU-JFK, BURNING SMELL ROW 15, NO VISIBLE SMOKE, TURNED OFF LTV SYSTEM SMELL DISSIPATED. COMPLIED WITH TSM 23-39-00-810-801 "ELECTRICAL ODORS OR FUMES IN CABIN TSM" NO FAULT FOUND. ALSO ACCOMPLISHED TSM TASK 24-00-00-810-823 FOR BURNING SMELL IN THE SDR YENA20090225016Actuator · failedFLT JB705 - JFK-SJU - AIR TURNBACK TO JFK, ENG 1 COMPRESSOR VANE ECAM, FAULT CYCLING EVERY COUPLE OF MINUTES, PER TSM 75-30-00-810-852. FOUND TO BE VSV INTERACTION FAULT. REMOVED AND REPLACED 2.5 MASTER ACTUATOR PER AMM 75-31-42. LUBRICATE NR 1 ENG VSV SYSTSDR YENA20090106002Structure · corrodedON WEEKLY INSP, AFT CARGO DOOR PROFILE SEAL BETWEEN FR 52 TO FR 56 HAS CORROSION AT WITH THE 5 FOLLOWING SIZE OF DEFECT LENGTH AND DEPTH. PERMANENT REPAIR FUSELAGE/AFT CARGO DOOR SEALING SECTION/CORROSION WAS ACCOMPLISHED IAW EC A08-690-02 REPLACED AFFECTED DOSDR YENA200812190130Outflow Valve · failedFLT NR 1729, JFK-SDQ, RETURNED TO JFK, PRESSURIZATION-V/S VARIABLE FROM -1250 TO +1250 FPM IN SYS 1 & SYS 2 AS WELL AS MANUAL-OUTFLOW VALVE FLUCTUATED IN CLIMB CRUISE AND DESCENT. V/S STABILIZED AFTER LEVELING AT 10,000. R&R OUTFLOW VALVE (10HL). ACCOMPLISHESDR YENA2007068Check Valve · failedFLT 1012, JFK TO BOS, DECLARED EMERGENCY, YELLOW RSVR OVERHEAT INDICATION BOTH ON ECAM & OVERHEAD ON ENG & ELECTRIC PUMPS. T/S TSM 29-13-00-810-802. FOUND ELEC PUMP DELIVERY CHECK VALVE BAD. REMOVED AND REPLACED CHECK VALVE PER AMM 29-24-21-04. DID VISUAL SDR YENA2007066Hydraulic System · overservicedFLT 24, TPA TO JFK, AIR RETURN TO TPA. HYD YELLOW RESERVOIR OVERHEAT ECAM ON CLIMBOUT. PERFORMED TSM TASK 29-13-00-810-802. FOUND YELLOW RESERVOIR OVERSERVICED AT 17L. DRAINED AND SERVICED YELLOW RESERVOIR. SYSTEM NOW CHECKS GOOD DURING ENG RUN, TAXI AND SDR YENA200667Fan · inoperativeVENT EXTRACT FAULT. CREW REPORTED BURNING ODOR INBOUND TO PBI. REMOVED AND REPLACED EXTRACT FAN (18HQ) AND OPS CHECKED NORMAL IAW 21-26-51.SDR YENA200559Control Servo · out of rigCLIMBING THROUGH FL180 FELT VIBRATION IN FLIGHT CONTROLS, RUDDERS AND PILOTS SEAT. AFT F/A'S REPORTED NOTICEABLE VIBRATION IN AFT PART OF AIRCRAFT. VIBRATION ALSO FELT IN LEVEL FLIGHT AND DESCENT. FLIGHT CONTROL STATUS PAGE NORMAL (AP WAS ON AND OFF) ACCOMPSDR YENA200558Access Panel · looseON CLIMBOUT THRU FL220 FELT SIGNIFICANT VIBRATION IN FRONT PART OF AIRCRAFT IN BOTH PILOTS SEATS AND RUDDER PEDALS, REDUCED POWER AND LEVELED OFF AND STILL FELT SAME VIBRATION. ALL ENGINE INDICATIONS NORMAL. PERFORMED PROCESS OF TSM TASK 05-50-00-810-801. NSDR YENA200539Odor · detectedF/A NOTICED ODOR OF BURNT WIRES STARTING AT ROW 12ABC AND STRONGEST AT ROW 14ABC. LIVE TV AND CABIN FANS TURNED OFF AND PUT AC FLOW TO HIGH AND ODOR DISSIPATED. A/C WAS DIVERTED. GROUND INSPECTION OF SUSPECT AREA REVEALED NO DEFECTS. SEVERAL SEB'S, DPCU'S SDR YENA200339Contactor · malfunctionedAT START OF TAKEOFF ROLL GOT ECAM, MADE A LOW SPEED, ABORT AT APPROX 80 KNOTS & RETURNED TO GATE. REMOVED AND REPLACED THE DC SHED ESSENTIAL BUSS CONTACTOR 8PH IAW 24-62-55-000-001. OPS CHECK OK.SDR YENA200311Power Supply · failedWHILE ACCOMPLISHING WEEKLY CHECK, EMERGENCY LIGHT FAILED TEST; T/S TO EPSU AT RIGHT EMERGENCY EXIT. REPLACED EPSU AT RIGHT EMERGENCY EXIT WITH BORROWED PART FROM UAL; NO DELAY INCURRED.SDR YENA200219Hydraulic System · lack of lubeAT JFK FLT 17, JFK TO FLL, ON TAKEOFF, B-HYDRAULIC SYSTEM LOW ECAM MESSAGE. ABORTED TAKEOFF AT APPROX 75 KTS, RETURNED TO GATE. FOUND BLUE SYSTEM LOW, FOUND NO EVIDENCE OF LEAK. SERVICED TO FULL, OPERATED ALL FLIGHT CONTROLS, UNABLE TO FIND LEAK AS PER AMM SDR YENA200103Power Supply · faultyON DAILY MAINTENANCE CHECK EPSU FWD LEFT FAULT. REMOVED AND REPLACED EPSU UNIT IAW AMM 33-51-38. OPS CHECK GOOD.SDR YENA200102Windshield · crackedBEFORE DESCENT FLT 43, JFK TO MCO, AT 39,000 FT, FLIGHT CREW REPORTED CRACKED CAPTAIN'S FRONT WINDSHIELD. REMOVED AND REPLACED CAPT WINDSHIELD PER AMM 56-11-11-000001 AND OPS CHECKED OK PER AMM 56-11-11-501.
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