N583JB
Service difficulty reports · 87
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 = 'N583JB' 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 = 'N583JB' 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 YENA2026051500460Battery · no testFLT 1501, JFK-FLL. EMERGENCY LIGHTS BY L1 DOOR NOT TURNING ON; R & R EPSU BATTERY ABOVE L1 DOOR REF 33-51-38 OPS CHECK GOOD.SDR YENA2026051500459Battery · failedFLT 1501, JFK-FLL. EMERGENCY LIGHTS ON L/H SIDE OF CABIN NOT TURNING ON, REMOVED AND REPLACED EPSU BATTERY L/H MID CABIN REF 33-51-38 OPS CHECK GOOD.SDR YENA2026042800434Unknown · odorFLT 1103, BDL-RSW. DECENDING THROUGH APPROXAMETLY 5-8 K FEET A STRONG ODOR CAME INTO THE FLIGHT DECK. I ATTEMPTED TO ISOLATE WITH TURNING PACK 2 OFF WHICH WAS UNSUCCESFUL CABIN CREW CALLED UP AROUND 4K FT AND NOTIFIED ODOR WAS IN THE CABIN PILOTS DONNED ON MASSDR YENA2026021600198Ecs · contaminatedFLT 1030, RSW-JFK. INFLIGHT NR 4 FA REPORTED A MIGRAINE HEADACHE AND SMELLED BURNED HYDRAULIC FLUID ODOR AT CRUISE. TURNED HYDRAULICS OFF & ON, ON THE GROUND TO RESET COMPUTERS.; COMPLIED WITH INFORMATION NOTICE 2017-T015 STEP 1. IDENTIFIED ODOR A TYPE 10 MISDR YENA2026012600063Unknown · odorFLT # 1471 LGA-FLL." DESCENDING THROUGH 10000 WE HAD A STRONG METALIC ACRID ODOR THAT PERSISTED HEAVILY UNTIL 6000 THEN ABATED SLIGHTLY BUT RETURNED HEAVILY THOUGHOUT THE CABIN UNTIL LANDING ALL CREW MEMBERS IFC PILOTS SMELLED IT STILL TASTE IT UPON LANDING.;CSDR YENA2025123001312Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RT IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 6 OCLOCK, CRAC K DEPTH IS 0.105 INCH APPROX, AT AFT GALLEY AREA (1 EA); REF AEROMAN WO 2025 278/1 NR 2025-622954 SDR YENA2025123001311Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBO ARD AT DOOR STOP FITTING 1 POSITION, CRACKDIRECTION IS 12 OCLOCK, CRA CK DEPTH IS 0.095 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1409520 TASKCARD: SDR YENA2025123001310Structure · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN HOLE C LOCATED IN DOUBLE JOGGLE AREA FR16 LH SIDE. CRACK DIRECTION IS 3 OCLOCK LOOKING OUTBOARD. CRACK DEPTH IS 0. 080 INCHES APROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED OSDR YENA2025123001309Structure · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN HOLE B LOCATED ON DOUBLE JOGGLE AREA FR16 LH SIDE. CRACK DIRECTION IS 3 OCLOCK LOOKING OUTBOARD. CRACK DEPTH IS 0. 120 INCHES APROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED OSDR YENA2025123001308Structure · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN HOLE C LOCATED AT DOUBLE JOGGLE AREA, FR16 R H SIDE. CRACK DIRECTION IS 3 OCLOCK LOOKING OUTBOARD. CRACK DEPTH IS 0 .130 INCHES APROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVEDSDR YENA2025123001307Intercostal · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN UPPER INBOARD HOLE LOCATED AT DOOR STOP 7, F R16, LH SIDE. CRACK DIRECTION IS 1 AND 9 OCLOCK LOOKING FWD. CRACK DEP TH IS 0.100 INCHES APPROX; REF AEROMAN NR 2025-622881 WO 2025 278/1 REMOVED AND REPLACED INTSDR YENA2025123001306Support · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. BTW FR66/FR68 AT LEVEL STR23L AFT GALLEY ARE A (CPCP RELATED); (RESOLVED ON W/O: 1409520 TASKCARD: NR-00043) REF AEROMAN NR 2025-622947 WO 2025 278/1 EMOVED AND REPLACED LOWER SILL LOCATED BTW FR66/FR68 AT LSDR YENA2025123001305Seat Track · corrodedDURING HEAVY MAINTENANCE: CORROSION SEAT TRACK +Y1162.5 LOC. BTW FR69/70 AFT GALLEY AREA (1 EA) (CPCP RELATED);(RESOLVED ON W/O: 1409520 TASKCARD: NR-00044) REF AEROMAN NR 2025-622946 WO 2025 278/1 REMOVED AND REPLACED SEAT TRACK Y1162.5 LOC BTW FR69/70, IN ASDR YENA2025123001304Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT C ONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKP IT (1 EA); REF AEROMAN WO 2025 278/1 NR 2025-622906 PERFORMED REPAIR IAW AEROMAN EA 53-0068-2SDR YENA2025123001303Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT IN TERNAL AREA, LH SIDE, FROM UPPER TENSION BOLT, CRACK DIRECTION IS 2 OC LOCK, CRACK LENGTH IS 0.105 INCH APPROX, IN COCKPIT (1 EA); RESOLVED ON W/O: 1409520 TASKCARSDR YENA2025123001302Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT IN TERNAL AREA, LOWER INBOARD CORNER, LH SIDE, CRACK LENGTH IS 0.230 INCH APPROX, IN COCKPIT (1 EA); (RESOLVED ON W/O: 1409520 TASKCARD: NR-00050) REF AEROMAN WO 2025SDR YENA2025123001301Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT IN TERNAL AREA, LOWER INBOARD CORNER, RHSIDE, CRACK LENGTH IS 0.080 INCH APPROX, IN COCKPIT (1 EA); REF AEROMAN WO 2025 278/1 NR 2025-622907 PERFORM PERMANENT REPAIRSDR YENA2025123001300Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOC. FR10 TO FR11 BTW STR2R TO STR3R ON UPPER FUSELAGE; (RESOLVED ON W/O: 1409520 TASKCARD: NR-00048) REF AEROMAN WO 2025 278/1 NR 2025-622588 EVALUATED DENT LOC. FR10 TO FR11 BTW STR2R TO STR3R ON UPPER FUSELAGE ASDR YENA2025123001299Stringer · corrodedDURING HEAVY MAINTENANCE: CORRODED STR 32, FR 58 LH SIDE ON AFT CARGO COMPARTMENT; REF AEROMAN W.0 2025 278/1 N.R. 2025-622963 **PERFORMED PERMANENT REPAIR LOCATED ON STR32, AT LEVEL FR58, LH SIDE IN AFT CARGO COMPARTMENT I.A.W. A320 SRM 53-00-13-300-001; THISDR YENA2025123001298Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND AT OPEN FASTENER HOLE, ZONE 1 VERTICAL STRINGER RADIUS Ñ4 IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.095 INCH. CRACK DIRECTION 12 OCLOCK VIEW FWD TO AFT; REF AEROMAN NR 2025-623139 WO 2025 278/1 CCOMPLISHEDSDR YENA2025123001297Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT OPEN FASTENER HOLE LOC. ZONE 2 VERTICAL STRINGER RADIUS Ñ4 IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.115 INCH . CRACK DIRECTION 11 AND 12 OCLOCK VIEW FWD TO AFT; REF AEROMAN NR 2025-623135 WO 2025 278/1 CSDR YENA2025123001296Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT OPEN FASTENER HOLE LOC. ZONE 2 VERTICAL STRINGER RADIUS Ñ2 IN CENTER FUSELAGE ON FRAME36. CRACK DEPTH 0.118 INCH . CRACK DIRECTION 12 OCLOCK VIEW FWD TO AFT; REF AEROMAN NR 2025-623119 WO 2025 278/1 ACCOMPLISSDR YENA2025123001295Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT OPEN FASTENER HOLE LOC. ZONE 1 VERTICAL STRINGER RADIUS Ñ2 IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.108 INCH . CRACK DIRECTION 12 OCLOCK VIEW FWD TO AFT; REF AEROMAN NR 2025-623122 WO 2025 278/1 CCOMPLISSDR YENA2025123001294Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND AT FASTENER HOLE, LOCATED AT PRESSURE DECK MEMBRANE TO CENTER BOX AREA, ON FR 36, Y1292 + 9 INCHES TO OTBD, LT SIDE, CRACK DIRECTION IS 12 OCLOCK LOOKING AFT, CRACK DEPTH IS 0.089 INCH REF AEROMAN NR 2025-62326SDR YENA2025123001293Pressure Deck · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MEMBRANE TO ENTER BOX AREA, ON FR36 AND -Y1292 PLUS 6 INCHES TO OUTBOARD, RH SIDE, CRACK DIRECTION IS 1 OCLOCK LOOKING AFT, CRACK DEPTH IS 0.115 INCH; REF AEROMAN NR 202SDR YENA2025123001292Pressure Deck · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MEMBR ANE TO CENTER BOX AREA, ON FR36AND Y1292 PLUS 4 INCHES TO OUTBOA RD, LH SIDE, CRACK DIRECTION IS 12 OCLOCK LOOKING AFT, CRACKK DEPTH IS 0.184 INCH; REF AEROMAN NR SDR YENA2025123001291Pressure Deck · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MEMBR ANE TO CENTER WING BOX AREA, ON FR36 AND Y1292 PLUS 5 INCHES TO OUTBOA RD, LH SIDE, CRACK DIRECTION IS 12 OCLOCK LOOKING AFT, CRACK DEPTH IS 0.119 INCH; REF AEROMASDR YENA2025123001290Pressure Deck · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MEMBR ANE TO CENTER WING BOX AREA, ON FR3 AND -Y1292 PLUS 2 INCHES TO OUTBO ARD, RH SIDE, CRACK DIRECTION IS 12 OCLOCK LOOKING AFT, CRACK DEPTH IS 0.109 INCH; REF AEROMASDR YENA2025123001289Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION INTERNAL SKIN LOC BTW FR65 TO FR 66, STRINGER 31RH ON AFT C ARGO COMPARTMENT; REF AEROMAN NR 2025-623339 WO 2025 278/1 PERFORMED REPAIR ON EXTERNAL SKIN BTW FR65 TO FR 66 , STRINGER 31RH IAW EA#53-0077-25 PART 1-3, EA COVER SDR YENA2025123001288Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 31RH LOC BTW FR65 TO FR 66 ON AFT CARGO COMPARTMENT (CPCP FINDING); REF AEROMAN WORK ORDER 2025 278/1 NR 2025-623177 REMOVED AND REPLACED STRINGER 31R LOCATED BTW FRAME 64 TO FRAME 67 IN AFT CARGO COMPARTMENT I.A.W.SDR YENA2025123001287Door Sill · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL DOOR LOC AFT POSITION ON BULK CARGO COMPARTMENT ( CPCP FINDING); REF AEROMAN WO 2025 278/1 NR 2025-623038 REMOVED AND REPLACED DOOR SILL BEAM LOCATED BTW FR60 THRU FR62, AT LEVEL STR38R, IN BULK CARGO COMPARTMENT SDR YENA2025123001286Dummy Rail · corrodedDURING HEAVY MAINTENANCE: CORROSION RAIL DUMMY Y503.2 LOC. BTW FR12/FR16 FWD GALLEY AREA (1 EA) (CPCP FINDING); REF AEROMAN WO #2025-278/1 NR # 2025-623108 REMOVED AND REPLACED NEW RAIL DUMMY (FLOOR BEAM) Y503.2 LOC. BTW FR12/FR16 FWD GALLEY AREA I.A.W A320 SSDR YENA2025123001285Seat Track · corrodedDURING HEAVY MAINTENANCE: "CORROSION FLOOR BEAM +Y1292 LOC. BTW FR12/FR24 AT FWD GALLEY AREA (1 EA) (CPCP FINDING); REF AEROMAN WO # 2025-278/1 NR# 2025-623109 REMOVED AND REPLACED FLOOR BEAM Y1292 LOC. BTW FR12 AND FR24 AT FWD GALLEY AREA IAW A320 SRM 51-11-1SDR YENA2025123001284Seat Track · corrodedDURING HEAVY MAINTENANCE: CORROSION FLOOR BEAM +Y765 LOC. BTW FR12/FR24 AT FWD GALLEY AREA (1 E A) (CPCP FINDING); REF AEROMAN WO # 2025-278/1 NR # 2025-623113 REMOVED AND REPLACED FLOOR BEAM Y765 LOC. BTW FR12 AND FR24 AT FWD GALLEY AREA IAW A320 SRM 51-42-11SDR YENA2025123001283Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER NODE AREA & CONTINUITY FITTING RH/LH SIDE / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0068-25 (COVER + PARTS 1-6) /2/ AIRBUS DOSSIER 81677616 /3/ AIRBUSDR YENA2025123001282Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / LOWER SKIN PANEL / FR64-FR65 BETWEEN STGR43L-STGR44 / CORROSION AND ELONGATED HOLE - TIME LIMITED REPAIR; REFERENCES: /1/ AEM EA 53-0094-25 (COVER + PARTS 1-4) /2/ AIRBUS DOSSIER 81702291 /3/ AIRBUS RDAF 817SDR YENA2025123001281Pressure Panel · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 36 LH & RH SIDES / PRESSURE PANEL / CRACK DAMAGES AT MULTIPLE HOLES – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0071-25 REV. 0 (COVER + PARTS 1-11) /2/ AIRBUS RDAF 81680593/005/2025#A /3/ AIRBUSDR YENA2025123001280Pressure Panel · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 36 LH & RH SIDES / PRESSURE PANEL / CRACK DAMAGES AT MULTIPLE HOLES – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0071-25 REV. 0 (COVER + PARTS 1-11) /2/ AIRBUS RDAF 81680593/005/2025#A /3/ AIRBUSDR YENA2025123001279Structure · crackedDURING HEAVY MAINTENANCE: WINGS / CENTER BOX / FRONT SPAR VERTICAL STRINGERS & HORIZONTAL FLOOR BEAMS / @ LEVEL OF FR36 & Y-254 & Y+765 / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-0108-25 REV. 0 (COVER + PARTS 1-3) /2/ AIRBUS RDAF 81679714/004/2SDR YENA2025123001278Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 65-66 & STR 31R / INNER SKIN / CORROSION DAMAGE - TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0077-25 REV. 1 (COVER + PARTS 1-3) /2/ AIRBUS RDAF 81680476/005/2025 ISSUE B /3/ AIRBUS TD/81680476/037SDR YENA2025081800845A/C Pack · odorFLT # 1567. PBI-HPN.AT 10,000' WE GOT A LVL 1 ODOR FUMES EVENT. TURNED OFF PACK #1 FUMES ODOR WENT AWAY. ODOR WAS IN COCKPIT; COMPLIED WITH INFO NOTICE 2017-T01, SECTION A, ISOLOATED FAULT TO TYPE 10, INSULATION FOUND IN DUCT TO HOT AIR VALVE (REMOVED) PERSDR YENA2025021700161A/C Pack · contaminatedFLT#545, ISP-PBI. 'ON DECENT THROUGH 12K ENTERING VISIBLE MOISTURE FUME / ODOR IN COCKPIT PACK1 OFF/ON/OFF IAW FUME CHECKLIST HP VALVE OPEN AT THRUST IDLE; COMPLIED W/ INFO NOTICE 2017-T015, SECTION B2. IDENTIFIED ODOR TYPE 5 (PACK 1). DECONTAMINATION LEVEL A SDR YENA2025021700158O-Ring · leakingFLT#2143, EWR-PBI. 'ON INITIAL DESCENT,DEPARTING FL340, 2 ENG ON , APU OFF, AFT CABIN REPORTED DIRTY SOCKS SMELL. ( APU SYSTEM ); REMOVED AND REPLACED APU DEOILER VALVE O-RINGS IAW AMM 49-91-49 LEACK CK GOOD MDDR# 573947 CLEARED MX-4 UPDATED PLACARD REMOVEDSDR YENA2025010700021Unknown · odorFLT#803, JFK-SJU. ' ALL 4 FAS REPORTED FUMES OR DIRTY SOCK SMELL ON SHORT FINAL INTO RWY 10 FOR SJU. OUR POSITION WAS APPROX. 5.10 DME ON THE FINAL APP. COURSE; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10 CABIN HEMS & AMBIESDR YENA2024032600466A/C Pack · odorFLT#871, JFK-SLC. AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK AND DECLARED AN EMERGENCY. DURING BOARDING TURNED ON APU AND NOTICED SLIGHT DIRTY SOCK ODOR. SMELL SLIGHTLY DISSIPATED IN FLIGHT DECK DURING TAXI. ON CLIMB OUT AFT F/A'S REPORTED STRONG DIRTY SOCK SDR YENA2024021400264Oil Cooler · leakingFLT#1145, RIC-FLL. 'FLT ATT REPORTED LVL 1 ODOR IN FWD GALLEY; C/W INFO NOTICE 2017-T015J TROUBLE SHOT ODER PER T/S/M 05-50-00-810-085B AND FOUND APU OIL COOLER AND SURROUNDING AREA CONTAMINATED WITH OIL PERFORMED ECS DECONTAMINATION PER AMM 49-00-00 APU REQUISDR YENA2024012900101Unknown · odorFLT#361, JFK-BGI. 'INFORMED BY FLIGHT ATT'S ON ARRIVAL AT AIRCRAFT OF ODER EVENT ON DESCENT WITH STRONG ODOR FROM MIDDLE BACK OF AIRCRAFT WITH COMPLAINT OF BURNING THROAT EYES AND LUNGS. ( APU SYSTEM ). (SUPPLEMENTAL INFORMATION TO FOLLOW)'SDR YENA2023122901663Unknown · unknownFLT#667, HPN-PBI. 'F/A'S REPORT DIRTY SOCK SMELL ON FINAL; ACCOMPLISHED INFO NOTICE 2017-T015.ACCOMPLISHED TSM 05-50-00-810-831-A. ODOR EVENT CLASSIFIED AS A LEVEL 1. ALL SSYTEMS OPERATE WITH NO ODOE NOTED. A/C OK FOR SERVICE.'SDR YENA2023122101622Unknown · unknownFLT#2357, EWR-MBJ. 'DIRTY SOCK SMELL IN CABIN IN DESCENT AFT OF ROW 18 TO AFT GALLEY LEVEL 1. ( PACKS ); REF ITEM 1, LP 3819108 (COMPLIED WITH INFO NOTICE 2017-T015, SECTION B2. DECONTAMINATION LEVEL 1 ACCOMPLISHED PER STM 05-50-00-810-085. A/C OK FOR SERVICESDR YENA2023022100178None · noneFLT#813, HPN-FLL. 'FA REPORT A " BURNING RUBBER SMELL" CENTERED ON 2ABC OVER THE NEXT 10 MINUTES THE SMELL ABATED; PERFORMED TSM 24-00-00-810-823 AND TSM 05-50-00-810-831, AND NO ISSUES WERE FOUND WITH A/C. OK TO CONTINUE SERVICE PLEASE SEE L/P 3697404, ITEM 2
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