N284JB
Service difficulty reports · 45
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 = 'N284JB' 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 = 'N284JB' 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 YENA2024121801568Seal · leakingFLT#2354, DCA-BOS. 'LOUD WIND SOUND FROM L1 DOOR FOR ENTIRE DURATION OF FLIGHT; REMOVED AND REPLACED L1 FWD PASS DOOR SEAL - REF AMM 52-11-21. OPS & LEAK CHECKS ON L/P# 4191373, ITEM 1.'SDR YENA2024121601563Door Sill · damagedFLT#216, BUS-BOS. 'FA & AO SAYS L1 DOOR MAKES AN UNUSUAL "POP" WHEN OPENING THE L1 DOOR; REPLACED L1 DOOR PROTECTIVE SILL PER AMM 53-10-22. OPS CHK OF L1 DOOR NORMAL. A/C OK TO CONT. SVC.'SDR YENA2024091601271Controller · malfunctionedFLT#455, BOS-JFK. 'INFLIGHT (WHILE ALREADY OPERATING W/MEL 36-00-00A) XBLEED FAIL EICAS MESSAGE PRESENTED AND AMBER X WAS DISPLAYED ON ECS SYNOPTICS PAGE; FOLLOWING FIM TASK 36-10-00-810-801-A00 FOUND AMS CH2 TO ERRONEOUSLY SHOW XBLEED VALVE X'D OUT. RESET AMSSDR YENA2024070800946Module · failedFLT#2186, PIT-BOS. (AIRCRAFT DECLARED AN EMERGENCY INTO BOS). 'AT FL 370 MO 78 SIGNIFICANT VIBRATION IN CONTROL YOKE. SUSPECT IN ROLL AXIS PSHMABAY APPROX 60HZ "SHAKER ANTICIPATED EICAS MESSAGE APPEARED. QRH CHECKLIST EXECUTED, ADDITIONAL INFO LIGHT ICING ENCOSDR YENA2024031200410Light · inoperativeDURING HEAVY MAINTENANCE: LH EMERGENCY EXIT DOOR SIDEWALL PANEL LIGHT IS INOP; REF. EAMS W/O: H9427 NR00721 - R&R EMERGENCY LIGHT ASSEM. #4 PER EMB 190-33-50-01-400-801-A. OPS OK.SDR YENA2023082500991Unknown · unknownFLT#655, SYR-MCO. 'COCKPIT EMER LIGHT NOT TURNING ON DURING EMER LIGHT TEST; CYCLED POWER OPERATIONAL CHECK NORMAL PER AMM 33-11-60.'SDR YENA2023072200848Unknown · unknownFLT#1954, DCA-BOS. 'UPON INSPECTION FOUND L2 DOOR SLIDE INTERFERE WITH L AFT FA SEAT; REMOVED AND REPLACED L2 DOOR SLIDE IAW AMM TASK CARD 25-65-01.SDR YENA2023051900542Unknown · unknownFLT#8448, CUN-BOS. 'GOUGE BELOW L1 DOOR NEEDS TO BE REPAIRED; DAMAGE REPAIRED PER EC# E23-355-02,' (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023040400313Power Supply · failedFLT#884, MCO-JFK. 'L1 DOOR EXIT SIGN INOP; REMOVED AND REPLACED FWD L/H ELPU IAW AMM 33-50-01. OPS TEST GOOD.'SDR YENA2023033100308Power Supply · failedFLT#884, MCO-JFK. 'L1 DOOR EXIT SIGN INOP; REMOVED AND REPLACED FWD L/H ELPU IAW AMM 33-50-01. OPS TEST GOOD.'SDR YENA2023030700216None · noneDURING HEAVY MAINTENANCE: CORROSION IN SEAT TRACK LOCATED Y= - 270.0 AND BETWEEN FR 84/85 AT CF III PASSENGER CABIN FLOOR STRUCTURE; ALL WORK ACCOMPLISHED ON TOMEX NRC 000110, SEAT TRACK LOCATED BETWEEN FR 84/85 AT CF III PASSENGER CABIN FLOOR STRUCTURE WAS RSDR YENA2023030700215None · noneDURING HEAVY MAINTENANCE: CORROSION IN DOUBLER OF WASTE ACCESS DOOR CUTOUT LOCATED BETWEEN FR 88/89 AND STRG 27R/28R AT CF III AFT CARGO COMPARTMENT INTERNAL STRUCTURE; ALL WORK ACCOMPLISHED ON TOMEX NRC 00128. DOUBLER OF THE WASTE ACCESS DOOR CUTOUT LOCATED BSDR YENA2023030700214None · noneDURING HEAVY MAINTENANCE: CORROSION IN SHEAR CLIP LOCATED IN FR 84 AND BETWEEN STRG 27R/28R AT CF III INTERNAL STRUCTURE AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00095: CORROSION IN SHEAR CLIP LOCATED IN FR 84 AND BETWEEN STRG 27R/28R AT CF IISDR YENA2023030700213None · noneDURING HEAVY MAINTENANCE: CORROSION IN THE SHEAR CLIP LOCATED IN FR 88 AND BETWEEN STRG 27R/28R AT CF III INTERNAL STRUCTURE AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00097, SHEAR CLIP LOCATED IN FR 88 AND BETWEEN STRG 27R/28R AT CF III INTERNSDR YENA2023030700212None · noneDURING HEAVY MAINTENANCE: CORROSION IN THE SHEAR CLIP LOCATED IN FR 86 AND BETWEEN STRG 27R/28R AT CF III INTERNAL STRUCTURE AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00098, SHEAR CLIP LOCATED IN FR 86 AND BETWEEN STRG 27R/28R WAS REPLACED PERSDR YENA2023030700211None · noneDURING HEAVY MAINTENANCE: CORROSION IN THE SHEAR CLIP LOCATED IN FR 87 AND BETWEEN STRG 27R/28R AT CF III INTERNAL STRUCTURE AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00096, SHEAR CLIP LOCATED IN FR 87 AND BETWEEN STRG 27R/28R WAS REPLACED PER SDR YENA2023030700210None · noneDURING HEAVY MAINTENANCE: [CPCP FINDING]: CORROSION ON SHEAR CLIP LOCATED ON FR-76 BETWEEN STRG-23L/24L; ALL WORK ACCOMPLISHED ON TOMEX NRC 00078, SHEAR CLIP LOCATED ON FR-76 BETWEEN STRG-23L/24L WAS REPLACED PER EMB190 SRM 51-41-01 AND SRM 51-41-02. (CONSIDERSDR YENA2023030700209None · noneDURING HEAVY MAINTENANCE: CORROSION IN THE SHEAR CLIP LOCATED IN FR 83 AND BETWEEN STRG 28R/27R AT CF III INTERNAL STRUCTURE AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00094, SHEAR CLIP LOCATED IN FR 83 AND BETWEEN STRG 28R/27R WAS REPLACED PER SDR YENA2023030700208None · noneDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FR84 & Y-270 SEAT TRACK EXISTING REPAIR / CORROSION -PERMANENT REPAIR. (CONSIDERED AS A MAOR REPAIR)SDR YENA2021010800023Not Reported · not reportedDURING HMV, EC E20-834-01. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR YENA2021010800022Rib · crackedDURING HMV, CRACK RIB 27 LEADING EDGE INTERNAL AREA ON LT WING, REF AEROMAN NR W/O 2020-368/1 WCC 2020-393240. REMOVED AND REPLACED NEW RIB 27 AND FASTENERS ON LT WING, IAW E190 SRM 51-40-08 AND DRAWING 191-03201-421.SDR YENA2021010800021Rib · crackedDURING HMV, CRACK RIB 17 LEADING EDGE INTERNAL AREA ON RT WING, REF AEROMAN NR W/O 2020-368/1 WCC 2020-393251. REMOVED AND REPLACED NEW RIB 17 AND FASTENERS ON RT WING, IAW E190 SRM 51-40-08 AND DRAWING 191-03201-421. PERFORMED APPLIED PROMOTER ADHESIVE ON RSDR YENA2021010800020Rib · crackedDURING HMV, CRACK RIB 17 LEADING EDGE INTERNAL AREA ON RT WING. REMOVED AND REPLACED NEW RIB 17 AND FASTENERS ON RT WING, IAW E190 SRM 51-40-08 AND DRAWING 191-03201-421. PERFORMED APPLIED PROMOTER ADHESIVE ON RIVETS RIB 17 LOCATED INSIDE THE FUEL TANK ON RTSDR YENA2021010800019Support Web · crackedDURING HMV, CRACK INTERNAL STRUCTURES SUPPORT WEB LOCATED CENTER WING TO FUSELAGE FAIRING AREA ON LOWER FUSELAGE, REF AEROMAN N/R 2020-393373 WO 2020 368/1. PERFORMED PERMENANT REPAIR TO CENTER FUSELAGE II WF RT REAR WEB CRACK AND CORROSION, PER AEROMAN EA53-SDR YENA2020021730173Battery · failedFT # 1579, DCA-FLL. R/H EXTERIOR EMERG LIGHT BELOW EMERG EXIT WON'T COME ON; R & R BATT POWER UNIT AMM 33-50-01. OPS CHECK NORM. A/C OK TO CONT.SDR YENA2019103010626Mount · crackedFT # 2601, BUF-JFK. FOUND CRACK ON PYLON LOWER LINK LUG ENG #1 INBD SIDE; REF LOGPAGE # 2482048-1 W/O# 1019537 FOR WORK PERFORMED. REF AEROMAN NR 2019-341092 WO 2019 35211 ACCOMPLISHED THE REPLACEMENT OF THE LH PYLON INBOARD UPPER SPAR WING USING ALTERNATE TOOSDR YENA2018120620811Life Raft · damagedFT # 395, HPN-MCO. INFLIGHT REPORTED AFT LIFE-RAFT BINDING IS UNRAVELING; REMOVED + REPLACED R/H AFT LIFE-RAFT IAW EMM 21-66-01SDR YENA201701010001Cable · failedFLT 79, DCA-FLL. FLIGHT CREW NOTIFIED MAINTENANCE THAT R1 SERVICE DOOR UNABLE TO DISARM. R & R R1 DOOR BALL FLEX CABLE IAW SB 190-52-0042 & EC E17-001-01.SDR YENA20150611191Shear Tie · corrodedDURING HEAVY MAINTENANCE, FOUND A CORRODED SHEAR TIE AT FRAME 78 BETWEEN STRINGERS 27 & 28L R & R THE SHEAR TIE AND TOP COATED RIVET HEADS. IAW SRM 51-40-01, 51-40-02, AND 51-23-06.SDR YENA20150611190Beam · corrodedDURING HEAVY MAINTENANCE FOUND CORROSION AFT CABIN PASSENGER DOOR LOWER BEAM FRAMES 85-87, STR 17L AROUND GIRT BAR . BLENDED AFFECTED AREA IAW SRM 51-10-08 PERFORMED HFEC PRIMED AND PAINTED AFFECTED AREA.SDR YENA20150611189Shear Tie · corrodedDURING HEAVY MAINTENANCE FOUND CORRODED SHEAR TIE AT FR 88 BETWEEN STR 27 & 28R. INSTALLED A NEW SHEAR TIE IAW SRM 51-41-01 AND 51-41-02 PRIMED TOPCOATED RIVETS HEADS IAW SRM 51-23-05 51-23-06.SDR YENA20130807171Unknown · odorAFTER TAKEOFF, A PUNGENT, STAGNANT, DIRTY, MUSKY ODOR UNLIKE BURNING OR SMOKE, FILLED THE ACFT COCKPIT AND CABIN. WENT AWAY WITHIN 10 MINUTES. NO EICAS OR OTHER DEFECTS NOTED. ACCOMPLISHED TC 21-20-00-810-803A. REPLACED BOTH RECIRCULATING FILTERS IAW 21-24-SDR YENA20130604124Light · inoperativeDURING HEAVY MX CHECK, DISCOVERED RT AFT EMERGENCY EXTERIOR EXIT LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED RT AFT EMERGENCY EXIT LIGHT IAW AMM 33-50-25.SDR YENA20130508098Audio Panel · failedFLT 1717 MCO-SDQ, #2 ACP (AUDIO CONTROL PANEL) FAILED IN FLIGHT (WENT BLACK) WITH COMM AUDIO 2 BREAKER POPPED. BREAKER POPPED 1 HOUR AFTER TAKEOFF WITH A NOTICEABLE BURNING SMELL. SMELL WENT AWAY AFTER BREAKER POPPED. REMOVED AND REPLACED NR 2 DAP (DIGITALSDR YENA20120922607Controller · failedFLT 559 HPN-TPA, CREW DECLARED EMERGENCY DUE TO DESCENDING THRU 17000, CAPTAIN WINDSHIED SHATTERED. EICAS MESSAGE APPEARED "WINDSHIELD 1 HEATER FAIL". REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER IAW AMM 30-42-01. OPS TEST IAW AMM 30-42-00 TASK 30-42-00-SDR YENA20120922606Windshield · crackedFLT 559 HPN-TPA, CREW DECLARED EMERGENCY DUE TO DESCENDING THRU 17000, CAPTAIN WINDSHIELD SHATTERED. EICAS MESSAGE APPERARED "WINDSHIELD 1 HEATER FAIL". REMOVED AND REPLACED CAPTAINS SIDE WINDSHIELD IAW AMM 56-11-00. OPS TEST OK.SDR YENA20120620531Acm · failedFLT 1109 JFK-RDU, CREW DECLARED EMERGENCY DUE TO SMELL IN COCKPIT DURING DESCENT. F/A'S CALLED TO REPORT SMOKE IN CABIN OVER EMERGENCY EXIT ROWS. DONNED O2 MASKS AND RAN QRH. AFTER LANDED AND STOPPED ON RUNWAY NO INTERNAL OR EXTERNAL INDICATION OF SMOKE/FIRSDR YENA20110514253Sensor · failedFLT 581 HPN-PBI, AIRCRAFT DIVERTED TO JFK DUE TO WING LEAK MSG AND TO AVOID ICING CONDITION. HOWEVER, DURING APPROACH THE CREW DECLARED EMERGENCY DUE TO SLAT FAIL. QRH COMPLIED WITH, ALSO GOT THE FOLLOWING EICAS MESSAGE, SHAKER ANTICIPATED, AOA LIMIT FAIL, SPSDR YENA20100329044Transceiver · failedFLT 572 PBI-HPN, EN ROUTE TO WHITE PLAINS WX RADAR BEGAN TO MALFUNCTION F/O WAS CHANGING SCALE AND CA RADAR SLAVED THEN WENT AWAY, F/O TILT ANGLE KEPT FLUCTUATING TO 3 THEN JUST SAWED ADJUST TO ANY ANGLE LOCKED UP. RADAR WOULD PAINT AT 12 MILE RING BUT ONLY SSDR YENA20100112006Sensor · malfunctionedFLT JB907 JFK-ORD ON APPROACH TO ORD CREW DECLARED AN EMERGENCY FOR A "SLAT FAIL" CAS MESSAGE WHEN SELECTING FLAPS SLATS FROM ZERO TO 1. CREW ACCOMPLISHED QRH PROCEDURES AND LANDED UNEVENTFULLY. MX RETRIEVED CMC CODE 27811014ACE AND COMPLIED WITH AMM FIM 27-SDR YENA20091220176Pump · failedFLT 1244 CLT-BOS DURING CRUISE AT FL350 PILOT DECLARED EMERGENCY DUE TO EICAS MESSAGE "HYD 2 EDP FAIL" LOSE OF NR 2 HYDRAULIC SYSTEM. RETURNED BACK TO CLT AND LANDED AIRCRAFT UNEVENTFULLY AND TAXIED TO THE GATE. MX REMOVED AND REPLACED ENGINE DRIVEN HYD PUMPSDR YENA20090713073Fadec · malfunctionedTHE ENG 1 TLA EICAS MSG APPEARED IN FLIGHT. FOLLOWED QRH AND DIVERTED TO NEAREST SUITABLE AIRPORT. THE NUMBER 1 ENGINE FAILED WHILE TAXIING IN TO THE GATE. MSG PRESENT FAIL ICON ON NR 1 N1 GAUGE. ENGINE 1 FAIL MSG ACCOMPANIED ENG 1 NO DISPATCH ENG SHORT DISDR YENA20090531058Unknown · odorF/A SMELLED FUMES IN AREA OF SEAT ROW 23 & 24 CLOSE TO FLOOR SMELL OF BURNING RUBBER. PERFORMED FIM 21-20-00-810-801-A. FOUND NO FAULTS. AS PRECAUTION LTV WILL BE DEACTIVATED REF LP 533524 DUE TO ENTRY INTO CENTER E-BAY BUY BACK REQUIRED. NOTE: FLIGHT WASSDR YENA200812190129Sensor · failedFLT NR 1304, IAD-JFK, SLAT FAIL WHEN MOVING FLAP HANDLE TO 1. AFTER FOLLOWING QRH SLAT INDICATION OF ZERO AND AMBER FLAPS 2 (FLAP HANDLE 2) GREEN. OTHER MSGS, SHAKE ANTICIPATED, AOA LIMIT FAIL, SPOILER FAULT, SLAT FAIL. FOUND SLAT SENSOR AT FAULT OB, R&R PREVSDR YENA200812110127Sensor · failedFLT NR 1219, BOS-BUF, SLAT FAIL IN FLIGHT WHEN FLAPS SELECTED TO POSITION ON APPROACH. R&R LT OTBD SKEW SENSOR IAW 27-83-01. OPS CHECK OK.
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