# Service difficulty reports: N633JB

A list on [N633JB](https://openairdocs.org/aircraft/N633JB.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 · 88 reports

- [SDR YENA2026100200922](https://openairdocs.org/sdr/YENA2026100200922.md): Unknown · odor · Oct 2, 2026 · N633JB · Airbus A320232 · Air Distribution System
  > FLT 959, BDL-FLL. ODOR EVENT DURING DESCENT, INFLIGHT DESCRIBES AS URINE/DIRTY SOCK/ AMONIA. NOT NOTICEABLE IN FWD AND AFT GALLEYS. AC RIGHT SIDE.
- [SDR YENA2026091100797](https://openairdocs.org/sdr/YENA2026091100797.md): Light · no test · Sep 7, 2026 · N633JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE,EMERGENCY EXIT LIGHT TEST FAILED OPERATIONAL CHECK.; (RESOLVED ON W/O: 1473121 TASKCARD: NR-00030) REF LCQ AAR WO# 440624 N/R# 30809. PERFORMED EPSU TEACH IN PROCEDURE, OPERATION CHECK GOOD IAW A320 AMM 33-51-00-820-801-A, 33-51-00-
- [SDR YENA2026091100796](https://openairdocs.org/sdr/YENA2026091100796.md): Elec Connector · damaged · Sep 7, 2026 · N633JB · Airbus A320232 · Light System Wiring
  > DURING HEAVY MAINTENANCE,REF. AAR-LCQ WO # 440624 N/R 30774 - EMERGENCY LIGHT IN CABIN CEILING PANEL 251JC HAS BROKEN WIRE; (RESOLVED ON W/O: 1473121 TASKCARD: NR-00040) PER AAR-LCQ WO# 440624 N/R 30774 - REPLACED EMERGENCY LIGHT CONNECTOR TERMINAL AND OPS C
- [SDR YENA2026091100795](https://openairdocs.org/sdr/YENA2026091100795.md): Battery · no test · Sep 7, 2026 · N633JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, REF. AAR-LCQ WO# 440624 N/R 30783 - EPSU 13WL FAIL CAPACITY CHECK; (RESOLVED ON W/O: 1473121 TASKCARD: NR-00041) PER AAR-LCQ WO 440624-30783 - REMOVED, REPLACED & OPS CHECK GOOD FOR EPSU BATTERY 13WL IAW A320 AMM 33-51-38-000-002-A,3
- [SDR YENA2026091100794](https://openairdocs.org/sdr/YENA2026091100794.md): Oxygen Box · no test · Sep 7, 2026 · N633JB · Airbus A320232 · Passenger Oxygen System
  > DURING HEAVY MAINTENANCE, AFT CTR 02 BOX FAILED OPS TEST; (RESOLVED ON W/O: 1473121 TASKCARD: NR-00047) REF AAR WO 440624 NR 30769 TROUBLESHOOT AND REPAIRED AFT CENTER O2 BOX IAW AEROSPACE CMM 35-21-74. CRI ACCOMPLISHED ON NR 30823. OPS CHECK GOOD IAW AMM 35
- [SDR YENA2025080600806](https://openairdocs.org/sdr/YENA2025080600806.md): A/C Pack · odor · Aug 6, 2025 · N633JB · Airbus A320232 · Cabin Cooling System
  > FLT#1146, FLL-RIC. "AFTER FL350 FAS CALLED TO REPORT STRONG SOCK SMELL IN ROWS 15 TO AFT A/C ROW CABIN ODOR RECOGNITION AND ISOLATION CHECK LIST. TURNED OFF PACK#2 AFTER 5 MINUTES, THE ODOR HAD DISSIPATED, CROSSBLEED VALVE SHUT AND PACK2 #2 REMAINED OFF FOR
- [SDR YENA2025051300489](https://openairdocs.org/sdr/YENA2025051300489.md): Skin · dented · May 11, 2025 · N633JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / EXTERNAL SKIN AT THE LAP JOINT @ FR 64-65 & STGR 32L-33L / DENT WITH GOUGE – PERMANENT REPAIR (PENDING DTA); REFERENCES: /1/ DAMAGE REPORT MX-283 AND MAPPING /2/ FERRY FLIGHT CONCURRENCE ECA-304 /3/ AIRBUS D
- [SDR YENA2025051300488](https://openairdocs.org/sdr/YENA2025051300488.md): Skin · gouged · May 11, 2025 · N633JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / EXTERNAL SKIN AT THE LAP JOINT @ FR 64-65 & STGR 32L-33L / DENT WITH GOUGE – TEMPORARY REPAIR; REFERENCES: /1/ DAMAGE REPORT MX-283 AND MAPPING /2/ FERRY FLIGHT CONCURRENCE ECA-304 /3/ AIRBUS DOSSIER 8158766
- [SDR YENA2024070100925](https://openairdocs.org/sdr/YENA2024070100925.md): Computer · failed · Jun 29, 2024 · N633JB · Airbus A320232 · Flight Control System
  > FLT#2065, BOS-RSW. (AIRCRAFT DIVERTED TO RIC). 'ELAC 2 FAULT IN FLT ALONG WITH BURNING ODOR. DID NOT RESET AND BURNING ODOR STAYED; REMOVED AND REPLACED ELAC 2 COMPUTER PER AMM 27-93-34. OPS CHECK GOOD AT THIS TIME REF LP 4048103-1 9PER TSM 05-50-00-810-831-A
- [SDR YENA2023122901664](https://openairdocs.org/sdr/YENA2023122901664.md): Servo Control · failed · Dec 26, 2023 · N633JB · Airbus A320232 · Landing Gear Steering System
  > FLT#1280, FLL-DCA. 'WHEEL N/W STRG FAULT LOST STRG ON LANDING; INTERRIGATED PFR AND FOUND FIN 6GC ELECTRO HYD SERVO CONTROL AT FAULT. REMOVED AND REPLACED ELECTRO HYD SERVO CONTROL ELECTRO HYD SERVO CONTROL AND ACCOMPLISHED SATISFACTORY CHECK OUT STEERING CO
- [SDR YENA2023071800828](https://openairdocs.org/sdr/YENA2023071800828.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 L/H SIDE DOOR STOP 7 HOLE H1 AT FWD GALLEY AREA; CRACK INDICATION ON FRAME 16 L/H SIDE DOOR STOP 7 HOLE H1 AT FWD GALLEY AREA IAW SRM 51-41-11, SRM 51-72-11, AND DWG D53114223.
- [SDR YENA2023071800827](https://openairdocs.org/sdr/YENA2023071800827.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 L/H SIDE, DOOR STOP 7, HOLE H3 AT FWD GALLEY AREA (1EA); REF AEROMAN WO 2023 204/1 NR 2023-331325 REMOVED AND REPLACED INTERCOSTAL FITTING LOCATED ON FRAME 16 L/H SIDE DOOR STOP #7 FWD GALLEY AREA IAW SRM
- [SDR YENA2023071800826](https://openairdocs.org/sdr/YENA2023071800826.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 R/H SIDE, DOOR STOP 7, HOLE H1 AT FWD GALLEY AREA (1EA); REF AEROMAN WO 2023 204/1 NR 2023-331326 REMOVED AND REPLACED INTERCOSTAL FITTING IAW A320 SRM 53-11-12-300-010, FIG. 006 (SHT 2), ITEM 20.
- [SDR YENA2023071800825](https://openairdocs.org/sdr/YENA2023071800825.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 R/H SIDE, DOOR STOP 7, HOLE H3 AT FWD GALLEY AREA (1EA); REF AEROMAN WO 2023 204/1 NR 2023-331327 REMOVED AND REPLACED INTERCOSTAL FITTING IAW A320 SRM 53-11-12-300-010, FIG. 004 (SHT 1), ITEM 8.
- [SDR YENA2023071800824](https://openairdocs.org/sdr/YENA2023071800824.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND ON FRAME SEGMENTS AT OVERWING EMERGENCY EXIT DOOR (FWD LH EEH DOOR 833) CRACK L= 0.130 INCH APPROX; REF AEROMAN WO 2023 204/1 NR 2023-331067 REMOVED AND REPLACED FRAME SEGMENT 1 AND PERFORMED FRAME 1 REINFO
- [SDR YENA2023071800823](https://openairdocs.org/sdr/YENA2023071800823.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (AFT L/H EEH DOOR 834) CRACK L= 0.133 INCH APPROX; REMOVED AND REPLACED FRAME SEGMENT 1 AND PERFORMED FRAME / REINFORCE DOOR STRUCTURE MODIFICATION ON EME
- [SDR YENA2023071800822](https://openairdocs.org/sdr/YENA2023071800822.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENT 1 AT OVERWING EMERGENCY EXIT DOOR (AFT R/H EEH DOOR 844) CRACK L= 0.120 INCH APPROX; REF AEROMAN WO 2023 204/1 NR 2023-331069 REMOVED AND REPLACED FRAME SEGMENT 1 AND PERFORMED FRAME / REIN
- [SDR YENA2023071800821](https://openairdocs.org/sdr/YENA2023071800821.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 AT THE OVERWING EMERGENCY EXIT DOOR (FWD RH EEH DOOR 843) CRACK L=0.127 INCH APPROX; REF: ARM W/O 2023 204/1 N/R 2023-331070. REMOVED AND REPLACED FRAME SEGMENT 1 AND PERFORMED FRAME/REI
- [SDR YENA2023071800820](https://openairdocs.org/sdr/YENA2023071800820.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SIL LOC. BTW FR66-FR68 STR 23L AT AFT GALLEY AREA (CPCP MPD 534195-01); (RESOLVED ON W/O: 1222084 TASKCARD: NR-00021) REMOVED & REPLACED LOWER SIL LOC. BTW FR66- FR68 AT STR 23L AT AFT GALLEY AREA IAW A320 SRM 5-42-11
- [SDR YENA2023071800819](https://openairdocs.org/sdr/YENA2023071800819.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SIL LOC. BTW FR 66- FR68 AT STR 23R AT AFT GALLEY AREA. (CPCP MPD 534195-01); (RESOLVED ON W/O: 1222084 TASKCARD: NR-00022) PERFORMED PERMANENT REPAIR ON LOWER SIL BTW FR 37 PLUS 12.5 INCHES THRU FR 68 AT LEVEL OF STR
- [SDR YENA2023071800818](https://openairdocs.org/sdr/YENA2023071800818.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 32L BTW FR.61 TO FR.63 IN AFT CARGO COMPARTMENT; REF AEROMAN WO 2023 204/1 NR 2023-331406 REMOVED AND REPLACED STRINGER 32L LOCATED BTW FR 53 TO FR 63 IN AFT CARGO COMPARTMENT I.A.W A320 SRM 51-42-11, A320 SRM 51-7
- [SDR YENA2023071800817](https://openairdocs.org/sdr/YENA2023071800817.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE WEB LOCATED BTW FR 69 AND FR70 AT LEVEL STR 23R AT AFT GALLEY AREA (CPCP RELATED MPD TASK 534195-01; (RESOLVED ON W/O: 1222084 TASKCARD: NR-00025) REF AEROMAN WO 2023 204/1 NR 2023-331339, JB W/O 1222084,
- [SDR YENA2023071800816](https://openairdocs.org/sdr/YENA2023071800816.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STRINGER 40R AND 41R AT LEVEL OF FRAME 31 IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE LOC. BTW STRINGER 40R AND 41R AT LEVEL OF FRAME 31 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11, SRM 51-
- [SDR YENA2023071800815](https://openairdocs.org/sdr/YENA2023071800815.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE WEB LOC. BTW FR 69 AND FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA (CPCP-RELATED MPD TASK 534195-01); REMOVED AND REPLACED STRUCTURE WEB LOC. BTW FR69 AND FR70 AT LEVEL OF STR 23L AT AFT GALLEY AREA IAW A320
- [SDR YENA2023071800814](https://openairdocs.org/sdr/YENA2023071800814.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE LOCATED AT LEVEL RIB 14 REAR SPAR AREA ON RH WING; ACCOMPLISHED REPAIR OF 8 CORROSION SPOTS AT RH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 UPPER AND LOWER SURFACE IN ACCORDANCE WITH AEROMAN EA 57-0235-23 (
- [SDR YENA2023071800813](https://openairdocs.org/sdr/YENA2023071800813.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION LOCATED ON TOP SKIN PANEL LOWER SURFACE TRAILING EDGE AREA FALSE REAR SPAR AT LEVEL RIB 7A RH WING; ACCOMPLISHED REPAIR OF 8 CORROSION SPOTS AT RH WING TRAILING EDGE OVERHANG,TOP SKIN PANEL 2 UPPER AND LOWER SURFACE IN ACCOR
- [SDR YENA2023071800812](https://openairdocs.org/sdr/YENA2023071800812.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION LOCATED ON TOP SKIN PANEL LOWER SURFACE TRAILING EDGE AREA R EAR SPAR BTW RIB 10 TO RIB 11 RH WING; ACCOMPLISHED REPAIR OF 8 CORROSION SPOTS AT RH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 UPPER AND LOWER SURFACE IN ACCO
- [SDR YENA2023071800811](https://openairdocs.org/sdr/YENA2023071800811.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION LOCATED ON TOP SKIN PANEL LOWER SURFACE TRAILING EDGE AREA R EAR SPAR BTW RIB 12 TO RIB 13 RH WING; ACCOMPLISHED REPAIR OF 8 CORROSION SPOTS AT RH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 UPPER AND LOWER SURFACE IN ACCO
- [SDR YENA2023071800810](https://openairdocs.org/sdr/YENA2023071800810.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION LOCATED ON TOP SKIN PANEL LOWER SURFACE TRAILING EDGE AREA R EAR SPAR BTW RIB 15 TO RIB 16 RH WING; ACCOMPLISHED REPAIR OF 8 CORROSION SPOTS AT RH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 UPPER AND LOWER SURFACE IN ACCO
- [SDR YENA2023071800809](https://openairdocs.org/sdr/YENA2023071800809.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION LOCATED ON TOP SKIN PANEL LOWER SURFACE TRAILING EDGE AREA R EAR SPAR BTW RIB 21 TO RIB 22 RH WING; ACCOMPLISHED REPAIR OF 8 CORROSION SPOTS AT RH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 UPPER AND LOWER SURFACE IN ACCO
- [SDR YENA2023071800808](https://openairdocs.org/sdr/YENA2023071800808.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION LOCATED ON TOP SKIN PANEL LOWER SURFACE TRAILING EDGE AREA R EAR SPAR BTW RIB 16 TO RIB 17 RH WING; ACCOMPLISHED REPAIR OF 8 CORROSION SPOTS AT RH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 UPPER AND LOWER SURFACE IN ACCO
- [SDR YENA2023071800807](https://openairdocs.org/sdr/YENA2023071800807.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION LOC. ON TOP SKIN PANEL LOWER SURFACE TRAILING EDGE AREA REAR SPAR BTW RIB 10 PLUS 5 INCHES LH WING; ACCOMPLISHED REPAIR LOCATED LH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 LOWER SURFACE IN ACCORDANCE WITH AEROMAN EA # 5
- [SDR YENA2023071800806](https://openairdocs.org/sdr/YENA2023071800806.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION LOC. ON TOP SKIN PANEL LOWER SURFACE TRAILING EDGE AREA REAR SPAR BTW RIB 11 PLUS 20 INCHES LH WING; ACCOMPLISHED REPAIR LOCATED LH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 LOWER SURFACE IN ACCORDANCE WITH AEROMAN EA #
- [SDR YENA2023071800805](https://openairdocs.org/sdr/YENA2023071800805.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION LOC. ON TOP SKIN PANEL LOWER SURFACE TRAILING EDGE AREA REAR SPAR BTW RIB 13 PLUS 18 INCHES LH WING; ACCOMPLISHED REPAIR LOCATED LH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 LOWER SURFACE IN ACCORDANCE WITH AEROMAN EA# 5
- [SDR YENA2023071800804](https://openairdocs.org/sdr/YENA2023071800804.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing Structure
  > DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE LOCATED BTW RIB 10 TO RIB 11 FRONT SPAR AREA ON RH WING; ACCOMPLISHED REPAIR OF 8 CORROSION SPOTS AT RH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 UPPER AND LOWER SURFACE IN ACCORDANCE WITH AEROMAN EA# 57-02
- [SDR YENA2023071800803](https://openairdocs.org/sdr/YENA2023071800803.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE WEB LOC. BTW FR 69 AND FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA (CPCP-RELATED MPD TASK 534195-01); REMOVED AND REPLACED STRUCTURE WEB LOC. BTW FR69 AND FR70 AT LEVEL OF STR 23L AT AFT GALLEY AREA IAW A320
- [SDR YENA2023071800802](https://openairdocs.org/sdr/YENA2023071800802.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STRINGER 40R AND 41R AT LEVEL OF FRAME 31 IN THE FWD CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE LOC. BTW STRINGER 40R AND 41R AT LEVEL OF FRAME 31 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11, SRM
- [SDR YENA2023071800801](https://openairdocs.org/sdr/YENA2023071800801.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SIL LOC. BTW FR 66- FR68 AT STR 23R AT AFT GALLEY AREA. (CPCP MPD 534195-01); PERFORMED PERMANENT REPAIR ON LOWER SIL BTW FR 37 PLUS 12.5 INCHES THRU FR 68 AT LEVEL OF STR 23R SIDE. IAW A320 SRM 53-41-14-300-001 PAR 2A
- [SDR YENA2023071800800](https://openairdocs.org/sdr/YENA2023071800800.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SIL LOC. BTW FR66-FR68 STR23L AT AFT GALLEY AREA (CPCP MPD 534195-01); REMOVED & REPLACED LOWER SIL LOC. BTW FR66- FR68 AT STR 23L AT AFT GALLEY AREA IAW A320 SRM 5-42-11 & SRM 51-72-11 & DWG D53480505 REF AEM WO 2023-
- [SDR YENA2023071800799](https://openairdocs.org/sdr/YENA2023071800799.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE WEB LOCATED BTW FR 69 AND FR70 AT LEVEL STR 23R AT AFT GALLEY AREA (CPCP RELATED MPD TASK 534195-01.); REF AEROMAN WO 2023 204/1 NR 2023-331339, JB W/O 1222084, NR-00025. REMOVED AND REPLACED STRUCTURE WEB
- [SDR YENA2023071800798](https://openairdocs.org/sdr/YENA2023071800798.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: WINGS / RH WING / TOP SKIN PANEL 2 / UPPER AND LOWER SURFACE / MULTIPLE CORROSION DAMAGES - TIME LIMITED REPAIR (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023071800797](https://openairdocs.org/sdr/YENA2023071800797.md): Unknown · unknown · Jul 14, 2023 · N633JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL 2 / LOWER SURFACE, REAR SPAR AND TRAILING EDGE OVERHANG / MULTIPLE CORROSION DAMAGES. PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023023100182](https://openairdocs.org/sdr/YENA2023023100182.md): Slide Raft · failed · Feb 17, 2023 · N633JB · Airbus A320232 · Emergency Equipment
  > FLT#1134, SJU-MCO. ' EMERGENCY LIGHTS TEST FAILED INT AND EXT LOAD FAULT FWD LEFT, R1 DOOR SLIDE REQUIRES REPLACEMENT; REMOVED AND REPLACED R1 DOOR SLIDE PACK ASSY PER AMM 25-62-44. PERFORMED OPS TEST OF EMERG LIGHT SYS PER AMM 33-51-00. TEST OK. A/C OK FOR CO
- [SDR YENA2022070800660](https://openairdocs.org/sdr/YENA2022070800660.md): None · failed · Jul 6, 2022 · N633JB · Airbus A320232 · Cabin Pressure Controller
  > FLT#404, SJU-JFK. (AIRCRAFT PERFORMED AN AIR TURN BACK TO SJU) 'ON CLIMB OUT AIR STOPPED FLOWING FROM VENTS, CABIN CREW REPORTED HISSING SOUNDS THEN WE EXPERIENCED LARGE PRESSURE SPIKES AND THEN NO AIRFLOW FOLLOWED BY MORE HIGH PRESSURE FROM VENTS. PACKS TURNE
- [SDR YENA2022022500096](https://openairdocs.org/sdr/YENA2022022500096.md): Connector · corroded · Jan 10, 2022 · N633JB · Airbus A320232 · Emergency Equipment
  > DURING HEAVY MAINTENANCE, SECONDARY FINDING CORROSIONON ELECTRICAL CONNECTOR ESCAPE SLIDE RAFT DOOR831 FWD GALLEY AREA; REF AEROMAN NR 2021-519313 WO 2021-343/1 REMOVED AND REPLACED ESCAPE SLIDE RAFT DOOR 831 FWD GALLEY AREA I.A.W AMM 25-62-44-000-012-A AND AM
- [SDR YENA2022022500095](https://openairdocs.org/sdr/YENA2022022500095.md): Light · failed · Jan 10, 2022 · N633JB · Airbus A320232 · Emergency Equipment
  > DURING HEAVY MAINTENANCE, THE PTP SHOWN MAINTENANCE MESSAGE EPSU BATTERY EMER L ATA 33-51-38; REF AEROMAN NT 2021-519352 WO 2021 343/1 REMOVED AND REPLACED EPSU BATTERY EMERGENCY P/N 3214-31 S/N 893374 IAW AMM 33-51-38-400-002-A AMM-33-51-38-000-002-
- [SDR YENA2022022500094](https://openairdocs.org/sdr/YENA2022022500094.md): Light · failed · Jan 10, 2022 · N633JB · Airbus A320232 · Emergency Equipment
  > DURING HEAVY MAINTENANCE, DONT PASS OPERATIONAL CHECK EPSU EMERGENCY POWER SUPPLY UNIT 10WL; REF AEROMAN NR 2021-519331 WO 2021 343/1 BR & R EPSU FIN 10WL IAW AMM 33-51-38-00-001-A & AMM 33-51-34-400-001-A
- [SDR YENA2022022500093](https://openairdocs.org/sdr/YENA2022022500093.md): Doubler · out of limits · Jan 10, 2022 · N633JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, (E/A A21-1381-01) FUSELAGE/ XM ANTENNA STRUCTURAL DEMOD/ OVERSIZED DOUBLER HOLES FR 54-55 @ STGR 1L-1R - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2021100700663](https://openairdocs.org/sdr/YENA2021100700663.md): Brake Sys · reads low · Oct 5, 2021 · N633JB · Airbus A320232 · Brake
  > FLT # 394, DEN-BOS. LEFT SIDE ALT BRAKE ONLY SHOWS 1000 PSI; RIGHT BRAKE PEDAL BOTH SIDES HAS NO FEEL AND WHEN DEPRESSED ONLY INDICATES 100PSI ON TRIPLE INDICATOR (ALTINATE SYS), REF ABOVE ITEM. SVCD ALTERNATE BRAKE RESERVOIR PER AMM 12-12-32 & BOTH BRAKE PED
- [SDR YENA2020060490361](https://openairdocs.org/sdr/YENA2020060490361.md): Battery · failed · May 29, 2020 · N633JB · Airbus A320232 · Emergency Lighting
  > FLT 737, BDL-MCO. AFT GALLEY EPSU BATT FAILED RTS T/C BATT CAPACITY TEST. R & R AFT GALLEY EPSU BATT AS PER AMM 33-51-00, OPS CK GOOD.

Next page: https://openairdocs.org/aircraft/N633JB/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 = 'N633JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N633JB/reports

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