# Service difficulty reports: N583JB

A list on [N583JB](https://openairdocs.org/aircraft/N583JB.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 87 reports

- [SDR YENA2026051500460](https://openairdocs.org/sdr/YENA2026051500460.md): Battery · no test · May 14, 2026 · N583JB · Airbus A320232 · Emergency Lighting
  > FLT 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 YENA2026051500459](https://openairdocs.org/sdr/YENA2026051500459.md): Battery · failed · May 14, 2026 · N583JB · Airbus A320232 · Emergency Lighting
  > FLT 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 YENA2026042800434](https://openairdocs.org/sdr/YENA2026042800434.md): Unknown · odor · Apr 26, 2026 · N583JB · Airbus A320232 · Air Distribution System
  > FLT 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 MAS
- [SDR YENA2026021600198](https://openairdocs.org/sdr/YENA2026021600198.md): Ecs · contaminated · Feb 13, 2026 · N583JB · Airbus A320232 · Air Distribution System
  > FLT 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 MI
- [SDR YENA2026012600063](https://openairdocs.org/sdr/YENA2026012600063.md): Unknown · odor · Jan 23, 2026 · N583JB · Airbus A320232 · Air Distribution System
  > FLT # 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.;C
- [SDR YENA2025123001312](https://openairdocs.org/sdr/YENA2025123001312.md): Door Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 YENA2025123001311](https://openairdocs.org/sdr/YENA2025123001311.md): Door Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 YENA2025123001310](https://openairdocs.org/sdr/YENA2025123001310.md): Structure · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 O
- [SDR YENA2025123001309](https://openairdocs.org/sdr/YENA2025123001309.md): Structure · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 O
- [SDR YENA2025123001308](https://openairdocs.org/sdr/YENA2025123001308.md): Structure · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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; (RESOLVED
- [SDR YENA2025123001307](https://openairdocs.org/sdr/YENA2025123001307.md): Intercostal · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING 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 INT
- [SDR YENA2025123001306](https://openairdocs.org/sdr/YENA2025123001306.md): Support · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING 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 L
- [SDR YENA2025123001305](https://openairdocs.org/sdr/YENA2025123001305.md): Seat Track · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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 A
- [SDR YENA2025123001304](https://openairdocs.org/sdr/YENA2025123001304.md): Window Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 53-0068-2
- [SDR YENA2025123001303](https://openairdocs.org/sdr/YENA2025123001303.md): Window Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 TASKCAR
- [SDR YENA2025123001302](https://openairdocs.org/sdr/YENA2025123001302.md): Window Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 2025
- [SDR YENA2025123001301](https://openairdocs.org/sdr/YENA2025123001301.md): Window Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 REPAIR
- [SDR YENA2025123001300](https://openairdocs.org/sdr/YENA2025123001300.md): Skin · dented · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING 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 A
- [SDR YENA2025123001299](https://openairdocs.org/sdr/YENA2025123001299.md): Stringer · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING 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; THI
- [SDR YENA2025123001298](https://openairdocs.org/sdr/YENA2025123001298.md): Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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 CCOMPLISHED
- [SDR YENA2025123001297](https://openairdocs.org/sdr/YENA2025123001297.md): Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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 C
- [SDR YENA2025123001296](https://openairdocs.org/sdr/YENA2025123001296.md): Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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 ACCOMPLIS
- [SDR YENA2025123001295](https://openairdocs.org/sdr/YENA2025123001295.md): Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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 CCOMPLIS
- [SDR YENA2025123001294](https://openairdocs.org/sdr/YENA2025123001294.md): Pressure Deck · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 2025-62326
- [SDR YENA2025123001293](https://openairdocs.org/sdr/YENA2025123001293.md): Pressure Deck · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 202
- [SDR YENA2025123001292](https://openairdocs.org/sdr/YENA2025123001292.md): Pressure Deck · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 YENA2025123001291](https://openairdocs.org/sdr/YENA2025123001291.md): Pressure Deck · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 AEROMA
- [SDR YENA2025123001290](https://openairdocs.org/sdr/YENA2025123001290.md): Pressure Deck · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 AEROMA
- [SDR YENA2025123001289](https://openairdocs.org/sdr/YENA2025123001289.md): Skin · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING 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 YENA2025123001288](https://openairdocs.org/sdr/YENA2025123001288.md): Stringer · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING 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 YENA2025123001287](https://openairdocs.org/sdr/YENA2025123001287.md): Door Sill · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 YENA2025123001286](https://openairdocs.org/sdr/YENA2025123001286.md): Dummy Rail · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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 S
- [SDR YENA2025123001285](https://openairdocs.org/sdr/YENA2025123001285.md): Seat Track · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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 51-11-1
- [SDR YENA2025123001284](https://openairdocs.org/sdr/YENA2025123001284.md): Seat Track · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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 51-42-11
- [SDR YENA2025123001283](https://openairdocs.org/sdr/YENA2025123001283.md): Window Frame · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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/ AIRBU
- [SDR YENA2025123001282](https://openairdocs.org/sdr/YENA2025123001282.md): Skin · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING 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 817
- [SDR YENA2025123001281](https://openairdocs.org/sdr/YENA2025123001281.md): Pressure Panel · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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/ AIRBU
- [SDR YENA2025123001280](https://openairdocs.org/sdr/YENA2025123001280.md): Pressure Panel · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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/ AIRBU
- [SDR YENA2025123001279](https://openairdocs.org/sdr/YENA2025123001279.md): Structure · cracked · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 81679714/004/2
- [SDR YENA2025123001278](https://openairdocs.org/sdr/YENA2025123001278.md): Skin · corroded · Dec 27, 2025 · N583JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING 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/81680476/037
- [SDR YENA2025081800845](https://openairdocs.org/sdr/YENA2025081800845.md): A/C Pack · odor · Aug 15, 2025 · N583JB · Airbus A320232 · Cabin Cooling System
  > FLT # 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) PER
- [SDR YENA2025021700161](https://openairdocs.org/sdr/YENA2025021700161.md): A/C Pack · contaminated · Feb 15, 2025 · N583JB · Airbus A320232 · Cabin Cooling System
  > FLT#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 YENA2025021700158](https://openairdocs.org/sdr/YENA2025021700158.md): O-Ring · leaking · Feb 14, 2025 · N583JB · Airbus A320232 · APU Oil System
  > FLT#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 REMOVED
- [SDR YENA2025010700021](https://openairdocs.org/sdr/YENA2025010700021.md): Unknown · odor · Jan 4, 2025 · N583JB · Airbus A320232 · Air Distribution System
  > FLT#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 & AMBIE
- [SDR YENA2024032600466](https://openairdocs.org/sdr/YENA2024032600466.md): A/C Pack · odor · Mar 23, 2024 · N583JB · Airbus A320232 · Cabin Cooling System
  > FLT#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 YENA2024021400264](https://openairdocs.org/sdr/YENA2024021400264.md): Oil Cooler · leaking · Feb 8, 2024 · N583JB · Airbus A320232 · APU Oil System
  > FLT#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 REQUI
- [SDR YENA2024012900101](https://openairdocs.org/sdr/YENA2024012900101.md): Unknown · odor · Jan 26, 2024 · N583JB · Airbus A320232 · Air Distribution System
  > FLT#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 YENA2023122901663](https://openairdocs.org/sdr/YENA2023122901663.md): Unknown · unknown · Dec 26, 2023 · N583JB · Airbus A320232 · Air Distribution System
  > FLT#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 YENA2023122101622](https://openairdocs.org/sdr/YENA2023122101622.md): Unknown · unknown · Dec 17, 2023 · N583JB · Airbus A320232 · Air Distribution System
  > FLT#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 SERVICE
- [SDR YENA2023022100178](https://openairdocs.org/sdr/YENA2023022100178.md): None · none · Feb 19, 2023 · N583JB · Airbus A320232 · External Power System
  > FLT#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

Next page: https://openairdocs.org/aircraft/N583JB/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N583JB/reports

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