# Service difficulty reports: N521JB

A list on [N521JB](https://openairdocs.org/aircraft/N521JB.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 · 94 reports

- [SDR YENA2026091000789](https://openairdocs.org/sdr/YENA2026091000789.md): Shear Plate · not reported · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTEANCE, (CPCP) "REFERENCE AEROMAN W.O 202 266/1 NR 2026-432646 * REMOVED AND REPLACED SHEAR PLATE LOC. BTW FR69 TO FR7O AT LEVEL STR 23R AFT GALLEY AREA I.A.W A320 SRM 51-72-11, A320 SRM 51-42-11 AND DWG: D53474180
- [SDR YENA2026091000788](https://openairdocs.org/sdr/YENA2026091000788.md): Fitting · not reported · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTEANCE, (CPCP) REFERENCE AEROMAN WO 2026-266/1 NR 2026 432782_ REMOVED AND REPLACED CENTER FITTING LOC. BTW FR 66 THRU FR 68 AT LEVEL OF STR 23RH IN AFT GALLEY AREA I.A.W. A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG D53480505 WORK
- [SDR YENA2026091000787](https://openairdocs.org/sdr/YENA2026091000787.md): Floor Support · not reported · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTEANCE, (CPCP) REFERENCE AEROMAN WO 2026 266/1 NR 2026 432685 _ REMOVED AND REPLACED FLOOR BEAM -Y765 AT AFT GALLEY AREA I.A.W A320 SRM 51-72-11 AND A320 SRM 51- 42-11 DWG D53472809, D53472777 AND DWG D53472195.
- [SDR YENA2026091000786](https://openairdocs.org/sdr/YENA2026091000786.md): Floorbeam · not reported · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTEANCE, (CPCP) "REFERENCE AEROMA W.O.2026 266/1 NR 2026-432734. REMOVED AND REPLACED FLOOR BEAM -Y464.8 AT AFT GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11.
- [SDR YENA2026091000785](https://openairdocs.org/sdr/YENA2026091000785.md): Floor Support · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTEANCE, (CPCP) "REF AEROMAN N/R 2026-432684,REMOVED AND REPLACED FLOOR BEAM Y765 LOC.FR66 TO FR70 AT AFT GALLEY AREA I.A.W A320 SRM 51-72-11 AND A320 SRM 51-42-11 AND DWG D53472794, DWG D53472777 AND DWG 53472809804 AND TOOL USED: ELECTRONIC C
- [SDR YENA2026091000784](https://openairdocs.org/sdr/YENA2026091000784.md): Floor Support · not reported · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTEANCE, (CPCP) "REF AEROMAN N/R 2026-432640, REMOVED AND REPLACED FLOOR BEAM (Y765) LOC. BTW FR12 TO FR 24 AT FWD GALLEY AREA I.A.W SRM 51-42-11, 51-72-11-911-001, DWG D53112813 AND DWG D53110876.
- [SDR YENA2026091000783](https://openairdocs.org/sdr/YENA2026091000783.md): Floorbeam · not reported · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTEANCE, (CPCP) "REF AEROMAN N/R 2026-432642, REMOVED AND REPLACED FLOOR BEAM (Y1292) LOC.BTW FR 12 TO FR 24 AT AFT GALLEY AREA I.A.W A320 SRM 51-42-11, A320 SRM 51-72-11-911-001, DWG D53112813 AND DWG D53110876.
- [SDR YENA2026091000782](https://openairdocs.org/sdr/YENA2026091000782.md): Floorbeam · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ2 FRAME 36. CRACK L= 0.320 INCH.; REF AEROMAN WO 2026 280/1 NR 2026-346060 ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE C
- [SDR YENA2026091000781](https://openairdocs.org/sdr/YENA2026091000781.md): Floorbeam · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ3 FRAME 36. CRACK L= 0.405 INCH.; REF AEROMAN WO 2026 280/1 NR 2026-346061, ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE
- [SDR YENA2026091000780](https://openairdocs.org/sdr/YENA2026091000780.md): Floorbeam · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ4 FRAME 36. CRACK L= 0.316 INCH.; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00078) REF AEROMAN WO 2026-280/1, NR 2026 - 346062: ACC
- [SDR YENA2026091000779](https://openairdocs.org/sdr/YENA2026091000779.md): Floorbeam · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ5 FRAME 36. CRACK L= 0.450 INCH.; REF AEROMAN WO 2026 280/1 NR 2026-346063ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE CE
- [SDR YENA2026091000778](https://openairdocs.org/sdr/YENA2026091000778.md): Frame · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE MIDD LE LOWER COMMON TO SKIN, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.105 INCH, IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1458309 TASKCARD: NR-00065) RE
- [SDR YENA2026091000777](https://openairdocs.org/sdr/YENA2026091000777.md): Frame · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE AFT LOWER COMMON TO SKIN, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.12 0 INCH, IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1458309 TASKCARD: NR-00066) REF A
- [SDR YENA2026091000776](https://openairdocs.org/sdr/YENA2026091000776.md): Frame · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE LOWE R OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTION IS 3 OCLOCK, CRA CK DEPTH IS 0.110 INCH, IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1458309 TASKCARD:
- [SDR YENA2026091000775](https://openairdocs.org/sdr/YENA2026091000775.md): Stringer · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON STR 5 LH FR 74 PLUS 1 INCH.CRACK DIRECTION PARALEL TO RADIUS OF STRINGER.CRACK LENGTH 0.250INCH; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00069) REF AEROMAN W/O 2026 280/1 NR 346167. ACCOMPLISHED THE REPAIR O
- [SDR YENA2026091000774](https://openairdocs.org/sdr/YENA2026091000774.md): Frame · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME 35 AT STGR30LH LEVEL OPEN FASTENER HOLE FWD MIDDLE COMMON TO SKIN,CRACK DIRECTION IS 12OCLOCK, CRACK DEPTH IS0.085INCH,IN FWD CARGO COMPARTMENT (1EA); (RESOLVED ON W/O: 1458309 TASKCARD: NR-00070) REF AEROM
- [SDR YENA2026091000773](https://openairdocs.org/sdr/YENA2026091000773.md): Door · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON OPEN HOLE LOC FR38RH STR19. CRACK DIRECTION 6 OCLOCK AND DEPTH =0.100 INCH PAX CABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00071) REF AEROMAN WO 2026-280/1, NR 2026 - 346115, ACCOMPLISHED REPAIR OF LH/RH E
- [SDR YENA2026091000772](https://openairdocs.org/sdr/YENA2026091000772.md): Frame · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND O N OPEN HOLE LOC FR39RH STR14 PLUS 4 INCH. CRACK DIRECTION 6 OCLOCK AND DEPTH =0.100 INCH)PAX CABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00072) REF AEROMAN WO 2026-280/1,
- [SDR YENA2026091000771](https://openairdocs.org/sdr/YENA2026091000771.md): Frame · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND O N OPEN HOLE LOC FR41LH STR14 PLUS 3 INCH. CRACK DIRECTION 6 OCLOCK AND DEPTH =0.100 INCH)PAX CABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00073) REF AEROMAN WO 2026-280/1,
- [SDR YENA2026091000770](https://openairdocs.org/sdr/YENA2026091000770.md): Door Frame · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND O N OPEN HOLE LOC FR41LH STR14 PLUS 4. CRACK DIRECTION 3 OCLOCK AND DEPT H =0.100 INCH)PAX CABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00074) REF AEROMAN WO 2026-280/1, NR
- [SDR YENA2026091000769](https://openairdocs.org/sdr/YENA2026091000769.md): Door Frame · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTEANCE, CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND O N OPEN HOLE LOC FR39LH STR14 PLUS 3 INCH. CRACK DIRECTION 9 OCLOCK AND DEPTH =0.100 INCH)PAX CABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00075) REF AEROMAN WO 2026-280/1,
- [SDR YENA2026091000768](https://openairdocs.org/sdr/YENA2026091000768.md): Frame · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTEANCE,DURING HEAVY MAINTEANCE,CRACK INDICATION ON FRAME (1 EA) (CRACK INDICATION FOUND ON OPENHOLE LOC FR39LH STR14 PLUS 4 INCH. CRACK DIRECTION 9 OCLOCK AND DEPTH =0.100 INCH)PAXCABIN; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00076) REF AERO
- [SDR YENA2026091000767](https://openairdocs.org/sdr/YENA2026091000767.md): Power Supply · no test · Sep 5, 2026 · N521JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTEANCE,EPSU 10WL DOES NOT PASS EMERGENCY LIGHT TEST; REF AEROMAN NR 2026-346269 W/O:2026 280/1: REMOVED AND REPLACED EPSU 10WL IAW AMM 33-51-38-400-001-A AND AMM 33-51-38-000-001-A. PERFORMED OPERATIONAL TEST, TEST IS OK.
- [SDR YENA2026091000766](https://openairdocs.org/sdr/YENA2026091000766.md): Floorbeam · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTEANCE,FRONT SPAR STRINGERS & HORIZONTAL FLOORBEAMS FR36 CRACKED. PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026091000765](https://openairdocs.org/sdr/YENA2026091000765.md): Stringer · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTEANCE, REAR FUSELAGE, TAILCONE STGR 5LH AT LEVEL OF FR74, CRACK DAMAGE. PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026091000764](https://openairdocs.org/sdr/YENA2026091000764.md): Attach Angle · cracked · Sep 5, 2026 · N521JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTEANCE,FUSELAGE. CENTER FUSELAGE FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT AT LEVEL OF STGR 30LH, FASTENER HOLES, CRACK DAMAGE – TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR A26-646-01)
- [SDR YENA2026022500236](https://openairdocs.org/sdr/YENA2026022500236.md): Terminal · detached · Feb 19, 2026 · N521JB · Airbus A320232 · Light System Wiring
  > FLT #1014 CUN-MCO. "RED EMERGENCY EXT LIGHT AT SEAT 9C INOPERATIVE. FOUND TERMINAL END DISCONNECTED FROM THE SOCKET, RECONNECTED THE TERMINAL END AND INSTALLED THE HARNESS PER AMM 31-50-00 OPS CHECK GOOD.
- [SDR YENA2025063000661](https://openairdocs.org/sdr/YENA2025063000661.md): Socket · loose · Jun 27, 2025 · N521JB · Airbus A321232 · Light System Wiring
  > FLT#2584, MCO-JFK. "FWD BULK HEAD LH SIDE RED EMERGENCY LIGHT INOP REPORTED BY CA; ACCOMPLISHED TEMP REPAIR OF EMERGENCY LIGHT SOCKET, INSTALLED HEAT SHRINKABLE CONDUITS IAW AWM 33-51-06 AND ESPM 20-33-34. PARTS-REQ # 2739382 FOR PERMANENT REPAIRS.
- [SDR YENA2025030300216](https://openairdocs.org/sdr/YENA2025030300216.md): Rib · corroded · Feb 27, 2025 · N521JB · Airbus A320232 · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE: LEFT WING T/E STRUCTURAL RIB IS CORRODED ON THE UPPER ATTACH FLANGE BETWEEN APPROX RIB 20 AND 21 ON THE AFT SIDE OF THE AFT SPAR; (RESOLVED ON W/O: 1355989 TASKCARD: NR-00004) REF HAECO WO 169006 NR 32271 FOR WORK PERFORMED; REMOVED
- [SDR YENA2025030300215](https://openairdocs.org/sdr/YENA2025030300215.md): Door Frame · cracked · Feb 27, 2025 · N521JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: MAIN CABIN L2 DOOR FRAME FR68 AT STOP FITTING #1 #3 HOLE HAS A CRACK; (RESOLVED ON W/O: 1355989 TASKCARD: NR-00006) REF GSO-HAECO WO# 169006 NR 32433. REPAIRED L/H FRAME 68 AT L-2 #1 STOP FITTING IAW A320 SRM 53-41-12-300-011. REVISIO
- [SDR YENA2024092701310](https://openairdocs.org/sdr/YENA2024092701310.md): Valve · failed · Sep 26, 2024 · N521JB · Airbus A320232 · Hydraulic System, Main
  > FLT#1230, CUN-EWR. (AIRCRAFT DECLARED AN EMERGENCY INTO EWR) 'HYD G LO LVL CAUTION LIGHT ON- NO GREEN PRESSURE OR QTY; FOUND GREEN HYD PRIORITY VALVE LEAKING HEAVILY. REMOVED AND REPLACED GREEN PRIORITY VALVE IAW AMM 29-11-33. OPS CK AND LEAK CK OK. A/C OK FOR
- [SDR YENA2022101701024](https://openairdocs.org/sdr/YENA2022101701024.md): None · none · Oct 16, 2022 · N521JB · Airbus A320232 · Fuel Indicating System
  > FLT#204, BDA-BOS. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN ABCK TO BDA) 'ANOMALOUS FUEL DECREASE FROM LEFT MAIN TANK AFTER T.O. RTB TXKF, NO FUEL LEAKS NOTED BY CRF ( ECAM FUEL PAGE INDICATIONS 1) I) FUEL QUANTITY INNER TANK).' (SUPPLEMENTAL T
- [SDR YENA2022083000834](https://openairdocs.org/sdr/YENA2022083000834.md): Window Post · cracked · Aug 25, 2022 · N521JB · Airbus A320232 · Flight Compartment Windows
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCHES, IN COC KPIT (1 EA); REF AE NR 2022-420038, WO 2022-175/1. REMOVED AND REPLACED CONTINUITY FITTING
- [SDR YENA2022083000833](https://openairdocs.org/sdr/YENA2022083000833.md): Battery · inoperative · Aug 25, 2022 · N521JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENACE: FAULT EPSU EMERGENCY POWER SUPPLY UNIT BATTERY 10WL, 11WL,12WL, 13WL IN PASSENGER CABIN (4EA); REF: ARM W/O 2022 175/1 NR 2022-420207 REMOVED AND REPLACED EPSU EMERGENCY POWER SUPPLY UNIT BATTERY 10WL, 11WL, 12WL, 13WL IN PASSENGER CAB
- [SDR YENA2021111200767](https://openairdocs.org/sdr/YENA2021111200767.md): Unknown · odor · Oct 29, 2021 · N521JB · Airbus A320232 · Air Distribution System
  > FLT 401, BOS-MSY. DIRTY SOCK ODOR ON DESCENT FIRST AT 17000 FEW MINUTES STRONGER MODERATE AT ABOUT 10000 ALL THE WAY TO LANDING TWO F/A'S ALSO SMELLED IT IN FWD CABIN TURNED PACK 1 OFF ON FINAL APPCH ODOR REPORTING FORM COMPLETED; COMPILED WITH INFO NOTICE 201
- [SDR YENA2021091500572](https://openairdocs.org/sdr/YENA2021091500572.md): Apu · odor · Sep 11, 2021 · N521JB · Airbus A320232 · APU Bleed Air System
  > FLT 909, BOS-NAS. DURING DECENT STRONG ODOR IN CABIN ( APU SYSTEM); PERFORMED ECS DECONTAMINATION OF PACKS IAW AMM 21-00-00-615-803 AND 36-11-00-615-805-A03. APU DEFERRED REFERENCE MDDR 449451. A/C OK FOR SERVICE. PERFORMED INFO NOTICE 2017-T015I. FOUND TO BE
- [SDR YENA2020050510326](https://openairdocs.org/sdr/YENA2020050510326.md): Frame · cracked · May 1, 2020 · N521JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK ON FRAME 68RH UPPER CORNER WEB JOINT; REF W/O 2020 81/1 N/R 2020-117556. SDR FOR MAJOR REPAIR. PERMANENT REPARED IAW AEROMON EA 53-0354-20 & EC A20-431-01
- [SDR YENA2020050510325](https://openairdocs.org/sdr/YENA2020050510325.md): Skin Panel · damaged · May 1, 2020 · N521JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, ELONGATED HOLES ON WING SKIN PANEL FUEL TANK RIB17 ON RH WING; REF: ARM W/O 2020 81/1 N/R 2020-117580. PERMANENT REPAIR INAW A320 SRM 57-27-11-300-002. THIS REPAIR IS CAT B AND MUST BE INSPECTED AT 28.900FC OR 57,800 FC FROM A/C FIRST
- [SDR YENA2019082319467](https://openairdocs.org/sdr/YENA2019082319467.md): Slide · no test · Aug 19, 2019 · N521JB · Airbus A320232 · Escape Slide
  > FT # 225, EMERGENCY SLIDES L1 AND R1 FAILED EMERGENCY LIGHT TEST (ESCAPE SLIDE LIGHTING); REMOVE AND REPLACED R1 SLIDE IAW AMM 25-62-44. PERFORMED OPS CHECK IAW AMM 25-62-44-400-007-A. OPS CHECK GOOD. PLACARD REMOVED MX-4 UPDATED MCC NOTIFIED. THIS CLEARS MDD
- [SDR YENA201904029169](https://openairdocs.org/sdr/YENA201904029169.md): Lens · missing · Mar 29, 2019 · N521JB · Airbus A320232 · Emergency Lighting
  > FT # 678, EMER EXIT LIGHT COVER MISSING COVER AND HANGING; R & R EMERGENCY LIGHT COVER PER MM 33-50-00 OPS CHK OK.
- [SDR YENA201811080771](https://openairdocs.org/sdr/YENA201811080771.md): Housing · defective · Nov 8, 2018 · N521JB · Airbus A320232 · Emergency Lighting
  > FT 422, NAS-JFK. AFT GALLEY EXIT SIGN OVERHEAD SHORTING OUT. REPEAT INOP FROM PREVIOUS FLIGHT WHEN BANGING ON IS TEMPORARILY FIXED. R&R AFT GALLEY OVERHEAD EMERGENCY EXIT HOUSING ASSY IAW AMM 33-51-00. OPS CHK OK.
- [SDR YENA2018101960694](https://openairdocs.org/sdr/YENA2018101960694.md): Battery · discharged · Oct 16, 2018 · N521JB · Airbus A320232 · Emergency Lighting
  > FLT 2074, TPA-EWR. EMERGENCY LIGHT BATTERY BY FWD L1 DOOR OVERHEAD GALLEY AREA INOP. FIN 10 WL; R & R EMERGENCY LIGHT BATTERY PER AMM 31-51-38, OPS CHECK GOOD.
- [SDR YENA2018101960693](https://openairdocs.org/sdr/YENA2018101960693.md): Light · inoperative · Oct 16, 2018 · N521JB · Airbus A320232 · Emergency Lighting
  > FLT 2074, TPA-EWR. 41WL EXIT MARKING SIGN AND 100 WL 1 BLOWN DURING TROUBLESHOOTING; FIN: 41 WL ( EXIT MARKING SIGN) + FIN 100 WL (LIGHT) RELAMPED PER AMM 33-51-00. FUNCTIONS NORMALLY AFTER TESTING.
- [SDR YENA2018101960692](https://openairdocs.org/sdr/YENA2018101960692.md): Battery · failed · Oct 16, 2018 · N521JB · Airbus A320232 · Emergency Lighting
  > FLT 2074, TPA-EWR. AFT EPSU FAULT (13WL); REMOVED AND REPLACED RELAY 8WL AND DIODE 1158VD. ALSO REPLACED AFT EPSU (13WL) AND EPSU BATTERY AS REQUIRED. AFT EMERGENCY EXIT LIGHTS CHECK OK IAW 33-51-00.
- [SDR YENA2018101960691](https://openairdocs.org/sdr/YENA2018101960691.md): Epsu · failed · Oct 16, 2018 · N521JB · Airbus A320232 · Emergency Lighting
  > FLT 2074, TPA-EWR. AFT EPSU FAULT (13WL); REMOVED AND REPLACED RELAY 8WL AND DIODE 1158VD. ALSO REPLACED AFT EPSU (13WL) AND EPSU BATTERY AS REQUIRED. AFT EMERGENCY EXIT LIGHTS CHECK OK IAW 33-51-00.
- [SDR YENA201810160690](https://openairdocs.org/sdr/YENA201810160690.md): Epsu · failed · Oct 16, 2018 · N521JB · Airbus A320232 · Emergency Lighting
  > FT 2074, TPA-EWR. FWD EMERGENCY LIGHTS INOP. R&R CONNECTOR AT 10WL IAW ESPM 20-44-19, OPS CHECK FAIL. FOUND 5409VB SHORTED, REMOVED HARNESS, R&R EPSU IAW AMM 33-51-38. OPS CHECK REQUIRED ON INSTALLATION OF 5409VB.
- [SDR YENA2018101960689](https://openairdocs.org/sdr/YENA2018101960689.md): Wire · shorted · Oct 16, 2018 · N521JB · Airbus A320232 · Light System Wiring
  > FLT 2074, TPA-EWR. FWD EMERGENCY EXIT LIGHTS INOP; FOUND WIRE SHORTED OUT FIN 5409VB, HARNESS REF. IAW AWM 33-51-01, R&R IAW ESPM 20-33-00, OPS TEST 33-51-11-710-050-A, PERFORMED OPS CHECK GOOD.
- [SDR YENA2018100160394](https://openairdocs.org/sdr/YENA2018100160394.md): Battery Pack · discharged · Sep 26, 2018 · N521JB · Airbus A320232 · Emergency Lighting
  > FLT 1558, BOG-FLL. FOUND MULTIPLE EMERGENCY LIGHTS FWD GALLEY INOP; REPLACED BATTERY PACK ON CHARGER IN FWD LT OVERHEAD PER AMM 33-51-00.
- [SDR YENA2018100160393](https://openairdocs.org/sdr/YENA2018100160393.md): Charger · failed · Sep 26, 2018 · N521JB · Airbus A320232 · Emergency Lighting
  > FLT 1558, BOG-FLL. FOUND FWD GALLEY EMERG EXIT LIGHT AS WELL AS ROW 1 AND 3 LIGHTS OUT; FOUND GALLEY BATTERY CHARGER, FWD LT SIDE, BAD. REPLACED BATTERY CHARGER PER AMM 33-51-00. GROUND CHECK GOOD.
- [SDR YENA2018091740344](https://openairdocs.org/sdr/YENA2018091740344.md): Slide · faulted · Sep 14, 2018 · N521JB · Airbus A320232 · Escape Slide
  > FLT 894, STI-EWR. DURING EMERGENCY LIGHTS TEST, FWD LT SLIDE FAULTED. REMOVED AND REPLACED FWD LT SLIDE PACK IAW AMM 25-62-44. OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N521JB/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 = 'N521JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N521JB/reports

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