# Service difficulty reports: N640JB

A list on [N640JB](https://openairdocs.org/aircraft/N640JB.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 · 58 reports

- [SDR YENA2026102200991](https://openairdocs.org/sdr/YENA2026102200991.md): Unknown · odor · Oct 21, 2026 · N640JB · Airbus A320232 · Air Distribution System
  > FLT#1161, LGA-DJT. AFTER DESCENDING THROUGH 4,000 FEET, F3/F4 COMPLAINED OF AN ODOR EVENT INCLUDING BURNING EYES AND HEADACHE CONCENTRATED IN THE AFT CABIN.; COMPLIED WITH INFORMATION NOTICE 2017-T015, STEP 1, ISOLATED FAULT TO TYPE 1. ACCOMPLISHED DE-CONTAMIN
- [SDR YENA2026092500904](https://openairdocs.org/sdr/YENA2026092500904.md): Unknown · odor · Sep 23, 2026 · N640JB · Airbus A320232 · Air Distribution System
  > FLT 1938, SDQ-SJU. NR 4 IFC SMELLED STRONG CHLORINE LIKE ODOR ON TAKEOFF, FOR 3-5 MINUTES. DISSIPATED ON ITS OWN.; COMPLIED WITH INFORMATION NOTICE 2017–T015 STEP 1 ISOLATED FAULT TO TYPE 10, CHLORINE ODOR, TO TSM 05–50–00–810–085–B/TSM 05–50–00–810–085–D.
- [SDR YENA2026080300643](https://openairdocs.org/sdr/YENA2026080300643.md): A/C Pack · odor · Aug 1, 2026 · N640JB · Airbus A320232 · Cabin Cooling System
  > FLT 914, HPN-PBI. PASSING THRU 10000FT STRONG ODOR COMING FROM PACKS MADE BOTH PILOTS COUGH. COMPLETED MX-270/271 ODOR REPORT, COMPLIED WITH INFORMATION NOTICE 2017-T015, STEP 1, ISOLATED FAULT TO TYPE 10, AMBIENT AIR DURING DESCENT, IAW TSM 05-50-00-810-085
- [SDR YENA2025102801057](https://openairdocs.org/sdr/YENA2025102801057.md): Unknown · odor · Oct 26, 2025 · N640JB · Airbus A320232 · Air Distribution System
  > FLT#2321, BOS-PBI. "DESCENDING THROUGH 9,000 AFT FLIGHT ATTENDANT REPORTED HOT PLASTIC ODOR EMITTING FROM AFT GALLEY THE ODOR WAS TRANSIENT. FOLLOWED A320 ODOR RECOGNITION & ISOLATION GUIDANCE FCOM PAGE 4-54 STEPS 1,2,14; COMPLIED WITH INFORMATION NOTICE 2017-
- [SDR YENA2025091500932](https://openairdocs.org/sdr/YENA2025091500932.md): Unknown · odor · Sep 13, 2025 · N640JB · Airbus A320232 · Air Distribution System
  > FLT#1310, JAX-BOS. "ELECTRICAL BURING SMELL BETWEEN ROWS 19-24 REPORTED BY FLIGHT ATTENDANTS AND PAX. NO SMOKE VISIBLE DURING TROUBLESHOOTING FA TURNED OFF PED AND SMWLL DISSAPTED. BURNING SMELL LASTED APPROX 5 MIN DURING CRUISE. ( THALES-AVANT IFE (ENTIRE SY
- [SDR YENA2024102101384](https://openairdocs.org/sdr/YENA2024102101384.md): Control Unit · damaged · Oct 20, 2024 · N640JB · Airbus A320232 · Weather Radar System
  > FLT#255, JFK-PLS. (AIRCRAFT DIVERTED TO FLL) 'INFLIGHT WX RADAR FAILURE DIVERT TO FLL THUNDER STORMS AND HURRICANE OSCAR IN THE AREA OF PLS; REMOVED AND REPLACED WX RADAR CONTROL UNIT IAW AMM 34-41-12 OPS CHECK GOOD. WEATHER RADAR CHECK GOOD.'
- [SDR YENA2024073001062](https://openairdocs.org/sdr/YENA2024073001062.md): Control System · faulted · Jul 29, 2024 · N640JB · Airbus A320232 · Drag Control System
  > FL698, MCO-LGA. (AIRCRAFT DIVERTED TO JFK) 'SPOILER 3/4 FAULT ( GRND SPOILER CNTRL SYS -1 & 2 OR 3 & 4). OPEN
- [SDR YENA2024052900796](https://openairdocs.org/sdr/YENA2024052900796.md): O-Ring · leaking · May 23, 2024 · N640JB · Airbus A320232 · Hydraulic System, Main
  > FLT#2836, LAX-SFO. (AIRCRAFT DECLARED AN EMERGENCY INTO SFO) ' HYD Y RSVR LO LVL ECAM; FOUND PINCHED O-RING ON PUT MANIFOLD, REPLACED O-RING PER AMM 29-13-15. PERFORMED OPS CHECK NO LEAKS NOTED, OK FOR SVC, REPLACED HYD LOW & HIGH FILITERS, OPS CK GOOD, NO LEA
- [SDR YENA2023120401521](https://openairdocs.org/sdr/YENA2023120401521.md): Unknown · unknown · Nov 30, 2023 · N640JB · Airbus A320232 · Emergency Lighting
  > FLT#128, MCO-EWR. 'EPSU (EMERGENCY POWER SUPPLY UNIT) AT 11WL INOP; REMOVED AND REPLACED LH AFT EMERGENCY LIGHT AFT LAMP IAW AMM 33-51-15. OPS CHECK GOOD.'
- [SDR YENA2023111501385](https://openairdocs.org/sdr/YENA2023111501385.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC. FR28 BTW STR41L TO STR42L IN FWD CARGO COMPARTMENT (CPCP REFER TO MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00007) REF AEROMAN W/O 2023 280/1 WCC 2023-640699 REMOVED AND RE
- [SDR YENA2023111501384](https://openairdocs.org/sdr/YENA2023111501384.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC FR28 BTW STR41R TO STR42R IN FWD CARGO COMPARTMENT (CPCP REFER TO MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00008) REF AEROMAN W/O 2023 280/1 WCC 2023-640698 REMOVED AND REP
- [SDR YENA2023111501383](https://openairdocs.org/sdr/YENA2023111501383.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC. FR30 BTW STR40L TO STR41L I N FWD CARGO COMPARTMENT (CPCP REFER TO MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00009) REF AEROMAN W/O 2023 280/1 WCC 2023-640700 REMOVED AND R
- [SDR YENA2023111501382](https://openairdocs.org/sdr/YENA2023111501382.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC. FR30. BTW STR40R TO STR41R IN FWD CARGO COMPARTMENT (CPCP REFER TOTHE MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00010) REF AEROMAN W/O 2023 280/1 WCC 2023-640701 REMOVED AN
- [SDR YENA2023111501381](https://openairdocs.org/sdr/YENA2023111501381.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC. FR31 BTW STR40R TO STR41R I N FWD CARGO COMPARTMENT (CPCP REFER TOTHE MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00011) REF AEROMAN W/O 2023 280/1 WCC 2023-640715 REMOVED AN
- [SDR YENA2023111501380](https://openairdocs.org/sdr/YENA2023111501380.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE TIE CLIP LOC. FR32 BTW STR40R TO STR41R I N FWD CARGO COMPARTMENT (CPCP REFER TO THE MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00012) REF AEROMAN W/O 2023 280/1 WCC 2023-640725 REMOVED A
- [SDR YENA2023111501379](https://openairdocs.org/sdr/YENA2023111501379.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H3 OF INTERCOSTAL FITTING AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 6 O CLOCK, CRACK DEPTH IS 0.120 INCH, AT FWD GALLEY AREA (1 EA); REF AEROMAN W/O 2023 280/1 WCC 2
- [SDR YENA2023111501378](https://openairdocs.org/sdr/YENA2023111501378.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE H3 OF INTERCOASTAL FITTING AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.120 INCH, AT FWD GALLEY AREA (1 EA); REF AEROMAN W/O 2023 280/1 WCC
- [SDR YENA2023111501377](https://openairdocs.org/sdr/YENA2023111501377.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H1 OF INTERCOSTAL FITTING AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION ARE 6 AND 12 OCLOCK, CRACK DEPTH IS 0.120 INCH, AT FWD GALLEY AREA (2 EA); REF AEROMAN W/O 2023 280/
- [SDR YENA2023111501376](https://openairdocs.org/sdr/YENA2023111501376.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H3 OF INTERCOSTAL FITTING AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 6 O CLOCK, CRACK DEPTH IS 0.120 INCH, AT FWD GALLEY AREA (1 EA); REF AEROMAN W/O 2023 280/1 WCC 2
- [SDR YENA2023111501375](https://openairdocs.org/sdr/YENA2023111501375.md): Unknown · unknown · Nov 13, 2023 · N640JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION SPLICE LOC. BTW FR30 TO FR31 AT LEVEL STR41R IN FWD CARGO COMPARTMENT (CPCP REFER TO THE MPD TASK 532180-01); (RESOLVED ON W/O: 1266781 TASKCARD: NR-00013) REMOVED AND REPLACED SPLICE LOC. BTW FR30 TO FR31 AT LEVEL STR41R I
- [SDR YENA2023032700289](https://openairdocs.org/sdr/YENA2023032700289.md): Unknown · unknown · Mar 26, 2023 · N640JB · Airbus A320232 · Air Conditioning System
  > FLT#751, JFK-CUN. '#3 #4 F/A'S BOTH NOTICED A STRONG BURNING ODOR FROM THE AFT GALLEY ON DESCENT; C/W INFORMATION NOTED 2017 -T015J, SECTION A, ISOLATED FAULT TO TYPE 10A1 C TSM 05-50-00-810-085-B TSM 05-50-00-810-085-D. A/C OK FOR SERVICE AND PERFORMED TSM 24
- [SDR YENA2022062800632](https://openairdocs.org/sdr/YENA2022062800632.md): Frame · cracked · Jun 27, 2022 · N640JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK INDICATION WAS FOUND ON FWD INNER FRAME SEGMENT (1)LOC EMERG EXIT DOOR 833 CRACK LENGTH 0.380 INCH AND LOCATED AT SIXTEENTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC#A320-52-114-01 ON EMERGENCY EXIT DOOR 833 FOR REPLACEMENT OF F
- [SDR YENA2022062800631](https://openairdocs.org/sdr/YENA2022062800631.md): Frame · cracked · Jun 27, 2022 · N640JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK INDICATION WAS FOUND ON AFT INNER FRAME SEGMENT (1)LOC EMERG EXIT DOOR 843 CRACK LENGTH 0.240 INCH AND LOCATED AT SIXTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC#A320-52-1144-02 ON EMERGENCY EXIT DOOR 843 FOR REPLACEMENT OF FRAM
- [SDR YENA2022062800630](https://openairdocs.org/sdr/YENA2022062800630.md): Frame · cracked · Jun 27, 2022 · N640JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK INDICATION WAS FOUND ON FWD INNER FRAME SEGMENT (1)LOC EMERG EXIT DOOR 843. CRACK LENGTH 0.030 INCH AND LOCATED AT SIXTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC#A320-52-1144-02 ON EMERGENCY EXIT DOOR 843 FOR REPLACEMENT FO F
- [SDR YENA2022062800629](https://openairdocs.org/sdr/YENA2022062800629.md): Frame · cracked · Jun 27, 2022 · N640JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, SEVERAL CRACK INDICATIONS WERE FOUND ON FWD INNER FRAME SEGMENT (1)LOC. EMERG EXIT DOOR 834. CRACK LENGTH 0.300 INCH AND LOCATED AT SIXTH FASTENER FROM UPPER SIDE, CRACK LENGTH 0.335 INCH LOC AT FOURTEENTH FASTENER L= 0.250" LOC AT F
- [SDR YENA2022062800628](https://openairdocs.org/sdr/YENA2022062800628.md): Frame · cracked · Jun 27, 2022 · N640JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, SEVERAL CRACK INDICATIONS WERE FOUND ON THE AFT INNER FRAME SEG(1)LOC. EMERG EXIT DOOR 834. CRACK LENGTH 0.325 INCH AND LOCATED AT SIXTH FASTENER FROM UPPER SIDE. CRACK LENGTH 0.335 INCH LOC AT SEVENTH FASTENER, CRACK LENGTH 0.290"
- [SDR YENA2022062800627](https://openairdocs.org/sdr/YENA2022062800627.md): Frame · cracked · Jun 27, 2022 · N640JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, SEVERAL CRACK INDICATIONS WERE FOUND ON FWD INNER FRAME SEGMENT (1)LOC EMERG EXIT DOOR 844. CRACK LENGTH 0.350 INCH AND LOCATED AT FIFTH FASTENER FROM UPPER SIDE CRACK LENGTH 0.315 INCH LOC AT FIFTEENTH FASTENER FROM UPPER SIDE; ACC
- [SDR YENA2022062800626](https://openairdocs.org/sdr/YENA2022062800626.md): Frame · cracked · Jun 27, 2022 · N640JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, SEVERAL CRACK INDICATIONS WERE FOUND ON AFT INNER FRAME SEGMENT (1) LOC EMERG EXIT DOOR 844. CRACK LENGTH 0.150" AT FOURTEENTH FASTENER. CRACK LENGTH 0.250 INCH LOCATION FIFTEENTH FASTENER FROM UPPER SIDE; ACCOMPLISHED EC# A320-52-1
- [SDR YENA2022062800625](https://openairdocs.org/sdr/YENA2022062800625.md): Frame · cracked · Jun 27, 2022 · N640JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK INDICATIONS WERE FOUND ON AFT INNER FRAME SEGMENT(1) LOC EMERG EXIT DOOR 833. CRACK LENGTH 0.100 INCH AND LOCATED AT SIXTEENTH FASTENER FROM UPPER SIDE AND SEVENTEENTH FASTENER FROM UPPER SIDE, CRACK LENGTH 0.120 INCH; ACCOMPLI
- [SDR YENA2021033100198](https://openairdocs.org/sdr/YENA2021033100198.md): A/C Pack · odor · Mar 25, 2021 · N640JB · Airbus A320232 · Cabin Cooling System
  > FLT 165, BOS-RSW. ON TAKE OFF & DECENT AROUND 5K HAD A STRONG SMELL IN THE CABIN. ALMOST LIKE VHEMICAL OF SOME KIND. FA SAID MAYBE DIRTY SOCK SMELL. SEEMS NOW AT GATE APU RUNNING HERE FAINT DIRTY SOCK SMELL. ( APU BLEED VALVE); REACTIVATED APU AFTER ECS DECON
- [SDR YENA2019042950238](https://openairdocs.org/sdr/YENA2019042950238.md): Battery Pack · failed · Apr 25, 2019 · N640JB · Airbus A320232 · Emergency Lighting
  > FT # 1692, LIR-JFK. SEAT MOUNTED EMR LIGHT AT SEAT 3C AND 7C FOUND INOP; R & R OF SEAT MOUNTED EMER LIGHT AT SEAT 3C AND 7C IAW AMM 33-51-18. NO HELP. R & R OF EPSU & EMER LIGHT BATTERY AT 11WL IAW AMM 33-51-38. ALL OPS NML OK FOR SVC.
- [SDR YENA2019042950237](https://openairdocs.org/sdr/YENA2019042950237.md): Epsu · failed · Apr 25, 2019 · N640JB · Airbus A320232 · Emergency Lighting
  > FT # 1692, LIR-JFK. SEAT MOUNTED EMR LIGHT AT SEAT 3C AND 7C FOUND INOP; R & R OF SEAT MOUNTED EMER LIGHT AT SEAT 3C AND 7C IAW AMM 33-51-18. NO HELP. R & R OF EPSU & EMER LIGHT BATTERY AT 11WL IAW AMM 33-51-38. ALL OPS NML OK FOR SVC.
- [SDR YENA2018121950857](https://openairdocs.org/sdr/YENA2018121950857.md): Battery Pack · inoperative · Dec 15, 2018 · N640JB · Airbus A320232 · Emergency Lighting
  > FT # 878, LAS-BOS. RH OVERWING EMERGENCY LIGHTS INOP; R & R RH OVER-WING EMERGENCY LIGHT BATTERY IAW AMM 33-51-00, OPS CHECK GOOD.
- [SDR YENA201710250869](https://openairdocs.org/sdr/YENA201710250869.md): Seat Track · corroded · Oct 25, 2017 · N640JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE SEAT TRACK -Y1292, BETWEEN FRAMES 12 AND 24. REPLACED THE SEAT TRACT IAW SRM 51-72-11.
- [SDR YENA201702220117](https://openairdocs.org/sdr/YENA201702220117.md): Battery · no test · Feb 22, 2017 · N640JB · Airbus A320232 · Emergency Lighting
  > DURING ROUTINE WEEKLY CHECK, A FAULTY EPSU BATTERY WAS FOUND. R & R THE BATTERY IAW AMM 31-51-00. OPS CHECK PASSED.
- [SDR YENA20160810689](https://openairdocs.org/sdr/YENA20160810689.md): Battery · failed · Aug 10, 2016 · N640JB · Airbus A320232 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, EMERGENCY LIGHT FAILED TEST; R & R EMERGENCY LIGHT BATTERY 12WL. PERFORMED BITE CHECK. BITE CHECK PASSED.
- [SDR YENA20160619551](https://openairdocs.org/sdr/YENA20160619551.md): Switch · failed · Jun 19, 2016 · N640JB · Airbus A320232 · Emergency Lighting
  > PILOT REPORTED EMERGENCY LIGHTS CAME ON AFTER 2ND ENGINE START. REPLACED EMERGENCY LIGHT ARM SWITCH, TOGGLE, 4WL IAW AMM 33-51-08. PERFORMED OPS CHECK AND ENGINE RUN. NO FAULTS FOUND.
- [SDR YENA20160510404](https://openairdocs.org/sdr/YENA20160510404.md): Battery Pack · failed · May 10, 2016 · N640JB · Airbus A320232 · Emergency Lighting
  > DURING MAINTENANCE IT WAS DISCOVERED THAT EMERGENCY LIGHTS TEST FAILED FOR THE FWD LT, R & R EPSU BATTERY AT 10 WL IAW AMM 33-51-38-000-002-A, 33-51-38-400-002-A. OPS CHECK WAS PERFORMED IAW AMM 33-51-38-710-052-B AND OPS CHECK PASSED.
- [SDR YENA20160509403](https://openairdocs.org/sdr/YENA20160509403.md): Floorbeam · corroded · May 9, 2016 · N640JB · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT MAIN CABIN FLOORBEAM HAS CORROSION, 765, FRAME 68. R & R AFT MAIN CABIN FLOORBEAM 765 FRAME IAW SRM 51-42-11 & 53-00-14.
- [SDR YENA20160509402](https://openairdocs.org/sdr/YENA20160509402.md): Shear Plate · corroded · May 9, 2016 · N640JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA SHEAR PLATE HAS CORROSION, LOCATION: Y1732, FRAME 69+8", STR 23 LT. R & R SHEAR PLATE IAW SRM 51-42-11 AND 53-41-14.
- [SDR YENA20160509401](https://openairdocs.org/sdr/YENA20160509401.md): Floor Support · corroded · May 9, 2016 · N640JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN FLOOR SUPPORT HAS CORROSION, LOCATION: Y1292, FR 67 +10", R & R FLOOR SUPPORT SRM 51-44-11, 53-41-14, 53-00-14.
- [SDR YENA20160509400](https://openairdocs.org/sdr/YENA20160509400.md): Floorbeam · corroded · May 9, 2016 · N640JB · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT CABIN FLOORBEAM HAS CORROSION, 765, FRAME 68, STR 23L. R & R FLOORBEAM IAW SRM 53-00-14, 51-41-14, 51-42-11.
- [SDR YENA20160509399](https://openairdocs.org/sdr/YENA20160509399.md): Floorbeam · corroded · May 9, 2016 · N640JB · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM, 1292, FRAME 68, STR 23R, HAS CORROSION; R & R FLOORBEAM IAW SRM 51-42-11, 53-41-14 AND 51-42-11.
- [SDR YENA20160509398](https://openairdocs.org/sdr/YENA20160509398.md): Floorbeam · corroded · May 9, 2016 · N640JB · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT CABIN FLOORBEAM, 765, FRAME 68, STR 23 RT, HAS CORROSION; R & R FLOORBEAM IAW SRM 53-42-11.
- [SDR YENA20160509397](https://openairdocs.org/sdr/YENA20160509397.md): Floorbeam · corroded · May 9, 2016 · N640JB · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM, LOCATION: 1292, FRAME 68, STR 23L, HAS CORROSION. R & R MAIN CABIN FLOORBEAM 1292, FRAME 68, STR 23L.
- [SDR YENA20160509396](https://openairdocs.org/sdr/YENA20160509396.md): Door Sill · corroded · May 9, 2016 · N640JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > LEFT PASSENGER DOOR SILL LOWER, 1762, FRAME 16, STR 23LT, AFT TWO HOLES HAS CORROSION. SPOTFACED AREA AND INSTALLED REPAIR WASHERS IAW SRM 53-11-14.
- [SDR YENA20141020223](https://openairdocs.org/sdr/YENA20141020223.md): Wire · damaged · Oct 20, 2014 · N640JB · Airbus A320232 · Light System Wiring
  > CREW REPORTED THAT EMERGENCY EXIT FLOOR LIGHTING RED LIGHT AFT END OF AISLE IS INOPERATIVE. IDENTIFIED LIGHT TO BE INSTALLED ON LAV D WALL. REPAIRED WIRING IAW ESPM 20-43-00. LIGHT OPS CHECK NORMAL.
- [SDR YENA20141020222](https://openairdocs.org/sdr/YENA20141020222.md): Connector · damaged · Oct 20, 2014 · N640JB · Airbus A320232 · Light System Wiring
  > CREW REPORTED EMERGENCY LIGHT AT 9C INOPERATIVE. REPINNED CONNECTOR 7261VC1A IAW AWM 33-51-07. OPS CHECK OK.
- [SDR YENA20140201019](https://openairdocs.org/sdr/YENA20140201019.md): Fan · failed · Feb 2, 2014 · N640JB · Airbus A320232 · Air Distribution Fan
  > DURING MAINTENANCE, ELECTRICAL BURNING ODOR IN THE CABIN WAS NOTED. FUTHER TROUBLESHOOTING INDICATED ODOR COMING FROM RECIRCULATING FAN NR 1. R & R NR 1 FAN IAW AMM 21-21-51-000-001-A, OPS CHECK OK. NO ODOR NOTED.
- [SDR YENA20131115228](https://openairdocs.org/sdr/YENA20131115228.md): Lamp · inoperative · Nov 15, 2013 · N640JB · Airbus A320232 · Emergency Lighting
  > DURING WEEKLY CHECK, CIDS MESSAGE FOR EXTERNAL POWER SUPPLY UNIT EXT LOAD EMERGENCY RT POPPED UP. SLAVED IN RT OVER WING ESCAPE SLIDE IAW FIM TASK 33-51-00-810-808-A. NO HELP RE-INSTALLED ORIGINAL SLIDE. FOUND OVER WING LIGHT ASSEMBLIES AT FAULT. REPLACED

Next page: https://openairdocs.org/aircraft/N640JB/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 = 'N640JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N640JB/reports

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