# Service difficulty reports: N529JB

A list on [N529JB](https://openairdocs.org/aircraft/N529JB.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 3 · 134 reports

- [SDR YENA2026010200001](https://openairdocs.org/sdr/YENA2026010200001.md): Unknown · odor · Jan 2, 2026 · N529JB · Airbus A320232 · Air Distribution System
  > FLT# 745 JFK- PSE. DURING BASE TO FINAL A STRONG SMELL WAS NOTED BY INFLIGHT IN THE CABIN. SMELL DID NO LAST LONG AFTER LANDING.. C/W INFORMATION NOTICE 2017-T015, STEP 1, ISOLATRED FAULT TO TYPE 10, (AMBIENT AIR) PER TSM 05-50-00-810-085-BTDM 50-50-00-810
- [SDR YENA2024052300780](https://openairdocs.org/sdr/YENA2024052300780.md): Unknown · odor · May 23, 2024 · N529JB · Airbus A320232 · Air Distribution Fan
  > FLT#813, HPN-FLL. 'ODOR IN CABIN REPORTED BASE TO FINAL PHASE OF FLT. LASTED UNTIL ENG SHUTDOWN AT GATE. MX270 COMPLETED.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2024021900280](https://openairdocs.org/sdr/YENA2024021900280.md): Unknown · odor · Feb 16, 2024 · N529JB · Airbus A320232 · Air Distribution System
  > FLT#855, JFK-PLS. 'RECEIVED AN OILY / DIRTY SOCK ODOR DESCENDING THROUGH 10,000 FT LEVEL 2 ( PACKS); COMPLIED WITH INFO NOTICE 2017-T015, SECTION B2. DECONTAMINATION LEVEL 2 WAS ACCOMPLISHED PER TSM 05-50-00-710-080-A. AIRCRAFT OK FOR SVC.'
- [SDR YENA2024012400085](https://openairdocs.org/sdr/YENA2024012400085.md): Unknown · odor · Jan 23, 2024 · N529JB · Airbus A320232 · Air Distribution System
  > FLT#627, JFK-POP. 'DURING DESCENT THROUGH 5,000' F/A CALLED TO INFORM PILOTS OF DIRTY SOCKS ODOR, DESCRIBED AS VERY STRONG. PILOTS DETECTED IT AS WELL ALTHOUGH FAINT. PAX COMPLAINED AND F/A'S WERE NAUSIATED. POWER AT IDLE AND APU NOT RUNNING. (ODOR EVENT DIR
- [SDR YENA2024011100028](https://openairdocs.org/sdr/YENA2024011100028.md): Unknown · unknown · Jan 10, 2024 · N529JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT#133, JFK-BZE. 'DUE TO ODOR EVENT PLACED BOTH PACKS ON MEL ( PACKS);UPON T/B APU IS THE SORCE OF ODOR APU PLACED ON MDDR # 535232 LOG PAGE 3846087-1 COMPLIED WITH INFO NOTICE 2017-T015-J. PERFROMED ECS DEONTAMINATION AND REPLACED RECEP FILTER NO ODOR NOTHE
- [SDR YENA2023041700406](https://openairdocs.org/sdr/YENA2023041700406.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH, IN COC KPIT (1 EA); REF AEROMAN WO 2023-68626 WO 2023 1/1 REMOVED AND REPLACED CONTINUITY FITTING L
- [SDR YENA2023041400398](https://openairdocs.org/sdr/YENA2023041400398.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68753: CORR STRG 43L FR24-FR28 FWD CARGO; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00023) REF AEM NR 2023-68753 FOR ALL WORK ACP RPL STGR 43L FR24-FR28 PER SRM 51-42-11, 51-72-11.
- [SDR YENA2023041300397](https://openairdocs.org/sdr/YENA2023041300397.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68759: CORR INT STRU SPLICE STGR 43L FR30-FR31 FWD CARGO; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00024) REF AEM NR 2023-68759 FOR ALL WORK ACP RPL SPLICE PLATE AT STGR43L PER SRM 51-42-11, 51-72-11.
- [SDR YENA2023041300396](https://openairdocs.org/sdr/YENA2023041300396.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68760: CORR INT STR SPLICE STGR 41L FR30-FR31 FWD CARGO; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00025) REF AEM NR2023-68760 FOR ALL WORK ACP RPL SPLICE AT STGR41L FR30-FR31 PER SRM 51-42-11, 51-72-11.
- [SDR YENA2023041300395](https://openairdocs.org/sdr/YENA2023041300395.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68762: CORR SHEAR TIE FR29 STGR 44L FWD CARGO; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00026) REF AEM NR 2023-68762: FOR ALL WORK ACP RPL SHEAR TIE FR29 STGR 44L FWD CARGO PER SRM 51-72-11.
- [SDR YENA2023041300394](https://openairdocs.org/sdr/YENA2023041300394.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR2023-68764 CORR STGR 41R FR31-FR33 FWD CARGO; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00027) REF AEM NR2023-68764 FOR ALL WORK ACP RPL STGR 41R FR31-FR33 FWD CARGO PER SRM 53-21-13-283-004.
- [SDR YENA2023041300393](https://openairdocs.org/sdr/YENA2023041300393.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68766 CORR SHEAR TIE FR34 STGR 42R/41R FWD CARGO; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00028) REF AEM NR 2023-68766 FOR ALL WORK ACP: RPL CLEAT FR34 STGR 42R/41R FWD CARGO PER SRM 51-72-11.
- [SDR YENA2023041300391](https://openairdocs.org/sdr/YENA2023041300391.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION ON EXISTING REPAIR AT AFT LAVATORY VENTILATION OUTLET BTW FR 69 AND FR70 AND BTW STR 30R AND STR 33R AT LOWER FUSELAGE; REF AEROMAN NR 2023-68517 WO 2023 1/1 ACCOMPLISHED REPAIR OF CORROSION ON EXISTING DOUBLER FOUND BETWEEN
- [SDR YENA2023041300392](https://openairdocs.org/sdr/YENA2023041300392.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68749 CORR STGR 40L FR27-FR28 FWD CARGO; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00029) REF AEM NR 2023-68749 FOR ALL WORK ACP RPR STGR 40L GFR27-FR28 FWD CARGO CAT B RPR SRI 53-21-13-205-018 TBL 001.
- [SDR YENA2023041300390](https://openairdocs.org/sdr/YENA2023041300390.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON UPPER INBOARD FASTENER HOLE OF DOOR STOP FI TTING 7 AT FRAME 16 RH, AFFECTED LAYER INTERCOSTAL. CRACK DEPTH 0.110 INCH; REF AEROMAN NR 2023-68779 WO 2023 1/1 REMOVED AND REPLACED INTERCOSTAL FITTING LOCATED F
- [SDR YENA2023041300389](https://openairdocs.org/sdr/YENA2023041300389.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION WAS FOUND ON THE LOWER INBOARD FASTENER HOLE OF DOOR STOP FI TTING 7 AT FRAME 16 RH, AFFECTED LAYER INTERCOSTAL. CRACK DEPTH 0.110 INCH; REF AEROMAN NR 2023-68780 WO 2023 1/1 REMOVED AND REPLACED INTERCOSTAL FITTING L
- [SDR YENA2023041300388](https://openairdocs.org/sdr/YENA2023041300388.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON PASSENGER CREW DOOR FR16 RH UPPER CORNER DOUBLE JO GGLE AREA HOLE Ñ5 IN PASSENGER CABIN (1 EA) (CRACK DIRECTION: 6 O CLO CK, L= 0.080 I APPROX.); REF AEROMAN NR 2023 68834 WO 2023 1/1 ACCOMPLISHED THE REPAIR OF THE
- [SDR YENA2023041300387](https://openairdocs.org/sdr/YENA2023041300387.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON PASSENGER CREW DOOR FR16 RH UPPER CORNER DOUBLE JO GGLE AREA HOLE Ñ6 IN PASSENGER CABIN (1 EA) (CRACK DIRECTION 2 O CLOCK LOOKING FROM OUTSIDE, L= 0.210 IN APPROX.); REF AEROMAN NR 2023-68835 WO 2023 1/1 ACCOMPLISH
- [SDR YENA2023041300386](https://openairdocs.org/sdr/YENA2023041300386.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON PASSENGER CREW DOOR FR16 RH LOWER CORNER DOUBLE JO GGLE AREA HOLE Ñ12 IN PASSENGER CABIN (1 EA) (CRACK DIRECTION 5 O CLO CK LOOKING FROM OUTSIDE, L= 0.090 IN APPROX)); REF AEROMAN NR 2023 68836 WO 2023 1/1 ACCOMPLI
- [SDR YENA2023041300385](https://openairdocs.org/sdr/YENA2023041300385.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE UPPER SKIN LOWER SURFACE OVERHANG AREA BTW RIB 15 AND RIB 16 ON RH WING; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00037) REF AEM NR 2023-68586 FOR ALL WORK ACCOMPLISHED, REPAIR MULTI-SITE CORROSION SPOTS FOUND O
- [SDR YENA2023041300384](https://openairdocs.org/sdr/YENA2023041300384.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION WEB FLOOR STRUCTURES BTW FR 69 TO FR 70 AT LEVEL STR 23R AFT GALLEY AREA;(RESOLVED ON W/O: 1200126 TASKCARD: NR-00038) REF AEM NR # 2023-68851 FOR ALL WORK ACCOMPLISHED, REMOVED AND REPLACED WEB LOCATED BTW FR 69 TO FR 70
- [SDR YENA2023041300383](https://openairdocs.org/sdr/YENA2023041300383.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE LOC. BTW FR 41 TO FR 42 AND BTW -Y1292 TO -Y1732 EXTERNAL SKIN UPPER SURFACE CENTER WING BOX IN PASSENGER CABIN; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00039) REF AEM NR# 2023-68843 FOR ALL WORK ACCOMPLISHED
- [SDR YENA2023041300382](https://openairdocs.org/sdr/YENA2023041300382.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE BTW FR41 TO FR42 BTW Y1292 TO Y1732 EXTERNAL SKIN UPPER SURFACE CENTER WING BOX IN PASSENGER CABIN; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00040) REF AEM NR2023-68841 FOR ALL WORK ACCOMPLISHED THE REPAIR OF
- [SDR YENA2023041300381](https://openairdocs.org/sdr/YENA2023041300381.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION TOP SKIN PANEL UPPER SURFACE AFT AT FR42 Y1292 PLUS IN CENTER FUEL TANK; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00041) REF AEM NR 2023-68924 FOR ALL WORK ACCOMPLISHED THE REPAIR OF THE CORROSION DAMAGE ON THE CENTER WING BO
- [SDR YENA2023041300380](https://openairdocs.org/sdr/YENA2023041300380.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE UPPER SKIN LOWER SURFACE OVERHANG AREA BTW RIB 17 AND RIB 18 ON RH WING; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00042) REF AEM NR 2023-68589 FOR ALL WORK ACCOMPLISHED, REMOVED CORROSION LOC T/E RIB 18 LOWER S
- [SDR YENA2023041300379](https://openairdocs.org/sdr/YENA2023041300379.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE UPPER SKIN LOWER SURFACE OVERHANG AREA BTW RIB 16 AND RIB 17 ON RH WING; (RESOLVED ON W/O: 1200126 TASKCARD: NR-00043) REF AEM NR# 2023-68587 FOR ALL WORK ACCOMPLISHED REPAIR MULTI-SITE CORROSION SPOTS FOUND O
- [SDR YENA2023041300378](https://openairdocs.org/sdr/YENA2023041300378.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH, IN COC KPIT (1 EA); REF AEROMAN WO 2023-68626 WO 2023 1/1 REMOVED AND REPLACED CONTINUITY FITTING L
- [SDR YENA2023041300377](https://openairdocs.org/sdr/YENA2023041300377.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH, IN COC KPIT (1 EA); REF AEROMAN NR 2023-68628 WO 2023 1/1 REMOVED AND REPLACED CONTINUITY FITTING R
- [SDR YENA2023041300376](https://openairdocs.org/sdr/YENA2023041300376.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INBOARD FASTENER HOLE OF DOOR STOP FI TTING 1 AT FRAME 16 LH, AFFECTED LAYER FRAME. CRACK DEPTH 0.110 INCH; REF AEROMAN NR 2023-68784 WO 2023 1/1 PERFORMED REPAIR ON LOWER INBOARD FASTENER HOLE OF DOOR
- [SDR YENA2023041300375](https://openairdocs.org/sdr/YENA2023041300375.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INBOARD FASTENER HOLE OF DOOR STOP FI TTING 1 AT FRAME 20 LH, AFFECTED LAYER FRAME. CRACK DEPTH 0.100 INCH; REF AEROMAN NR 2023-68785 WO 2023 1/1 PERFORMED REPAIR ON LOWER INBOARD FASTENER HOLE OF DOOR
- [SDR YENA2023041300374](https://openairdocs.org/sdr/YENA2023041300374.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: 12WL EPSU FAULT RH SIDE; REF AEROMAN NR 2023-69144 WO 2023 1/1 R & R EPSU 12WL RH SIDE IAW AMM 35-51-38-000-001A.
- [SDR YENA2023041300373](https://openairdocs.org/sdr/YENA2023041300373.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE REAR FALSE SPAR AT LEVEL OF RIB 8 OVERHAND ARE A ON RH WING; REF AEROMAN NR 2023-68541 WO 2023 1/1 REPAIRED MULTI-SITE CORROSION SPOTS FOUND ON THE TRAILING EDGE OVERHANG TOP SKIN PANEL 2 ON THE RH WING BETWEEN
- [SDR YENA2023041300372](https://openairdocs.org/sdr/YENA2023041300372.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE: CORROSION LOCATED ON TOP SKIN TRAILING EDGE OVERHANG AREA LOWER SURFACE E AT LEVEL RIB 16 PLUS 12.800 IN RH WING; REF AEROMAN NR 2023-69019 WO 2023 1/1 REPAIRED MULTI-SITE CORROSION SPOTS FOUND ON THE TRAILING EDGE OVERHANG TOP SKIN P
- [SDR YENA2023041300371](https://openairdocs.org/sdr/YENA2023041300371.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE: SECONDARY FINDING: WEAR LOCATED TOP SKIN PANEL TRAILING EDGE OVERHANG AREA AT LEVEL RIB 4 RH WING; REF AEROMAN NR 2023-69030 WO 2023 1/1 REPAIRED MULTI-SITE CORROSION SPOTS FOUND ON THE TRAILING EDGE OVERHANG TOP SKIN PANEL 2 ON THE R
- [SDR YENA2023041300370](https://openairdocs.org/sdr/YENA2023041300370.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE: CORROSION LOCATED AT LEVEL RIB 7A TOP SKIN TRAILING EDGE OVERHANG LOWE R SURFACE AREA RH WING; REF AEROMAN NR 2023-69065 WO 2023 1/1 REPAIRED MULTI-SITE CORROSION SPOTS FOUND ON THE TRAILING EDGE OVERHANG TOP SKIN PANEL 2 ON THE RH WI
- [SDR YENA2023041300369](https://openairdocs.org/sdr/YENA2023041300369.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE: CORROSION LOCATED ON TOP SKIN TRAILING EDGE OVERHANG AREA LOWER SURFACE E AT LEVEL RIB 16 PLUS 12.800 IN RH WING; REF AEROMAN NR 2023-69019 WO 2023 WO 1/1 REPAIRED MULTI-SITE CORROSION SPOTS FOUND ON THE TRAILING EDGE OVERHANG TOP SKI
- [SDR YENA2023041300368](https://openairdocs.org/sdr/YENA2023041300368.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE: CORROSION TOP SKIN TE OVERHANG RIB 13 PLUS 17" LH WING; REF AEROMAN NR 2023-69037 WO 2023 1/1 REPAIRED PER EC A23-242-01.
- [SDR YENA2023041300367](https://openairdocs.org/sdr/YENA2023041300367.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE: CORROSION TOP SKIN TE OVERHANG RIB 15 LH WING; REF AEROMAN NR 2023-69039 CORRECTIVE ACTION: REPAIR CORROSION STOPS AFFECTING THE TOP SKIN PANEL #2 TRAILING EDGE OVERHANG BETWEEN RIB 13-16, RIB 18-20 AND WX3494-WX-4010 ON THE LH WING I
- [SDR YENA2023041300366](https://openairdocs.org/sdr/YENA2023041300366.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE: CORROSION EXTERNAL SKIN TOP SKIN TE OVERHANG RIB 18 + 6.5" LH WING; REF AEROMAN NR 2023-69044 WO 2023 1/1 CORRECTIVE ACTION: REPAIR CORROSION STOPS AFFECTING THE TOP SKIN PANEL #2 TRAILING EDGE OVERHANG BETWEEN RIB 13-16, RIB 18-20 A
- [SDR YENA2023041300365](https://openairdocs.org/sdr/YENA2023041300365.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE: CORROSION EXTERNAL SKIN TE OVERHANG RIB 19 + 8.5" LH WING; REF AEROMAN NR 2023-69045 WO 2023 1/1 CORRECTIVE ACTION: REPAIR CORROSION STOPS AFFECTING THE TOP SKIN PANEL #2 TRAILING EDGE OVERHANG BETWEEN RIB 13-16, RIB 18-20 AND WX3494-
- [SDR YENA2023041300364](https://openairdocs.org/sdr/YENA2023041300364.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68749 CORR STGR 40L FR27-FR28 FWD CARGO; REF AEM NR 2023-68749 FOR ALL WORK ACP RPR STGR 40L GFR27-FR28 FWD CARGO CAT B RPR SRI 53-21-13-205-018 TBL 001. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023041300363](https://openairdocs.org/sdr/YENA2023041300363.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68766 CORR SHEAR TIE FR34 STGR 42R/41R FWD CARGO; REF AEM NR 2023-68766 FOR ALL WORK ACP: RPL CLEAT FR34 STGR 42R/41R FWD CARGO PER SRM 51-72-11. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023041300362](https://openairdocs.org/sdr/YENA2023041300362.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR2023-68764 CORR STGR 41R FR31-FR33 FWD CARGO; REF AEM NR2023-68764 FOR ALL WORK ACP RPL STGR 41R FR31-FR33 FWD CARGO PER SRM 53-21-13-283-004. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023041300361](https://openairdocs.org/sdr/YENA2023041300361.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68762: CORR SHEAR TIE FR29 STGR 44L FWD CARGO; REF AEM NR 2023-68762: FOR ALL WORK ACP RPL SHEAR TIE FR29 STGR 44L FWD CARGO PER SRM 51-72-11. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023041300360](https://openairdocs.org/sdr/YENA2023041300360.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68760: CORR INT STR SPLICE STGR 41L FR30-FR31 FWD CARGO; REF AEM NR2023-68760 FOR ALL WORK ACP RPL SPLICE AT STGR41L FR30-FR31 PER SRM 51-42-11, 51-72-11. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023041300359](https://openairdocs.org/sdr/YENA2023041300359.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68759: CORR INT STRU SPLICE STGR 43L FR30-FR31 FWD CARGO; REF AEM NR 2023-68759 FOR ALL WORK ACP RPL SPLICE PLATE AT STGR43L PER SRM 51-42-11, 51-72-11. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023041300358](https://openairdocs.org/sdr/YENA2023041300358.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: REF AEM NR 2023-68753: CORR STRG 43L FR24-FR28 FWD CARGO; REF AEM NR 2023-68753 FOR ALL WORK ACP RPL STGR 43L FR24-FR28 PER SRM 51-42-11, 51-72-11. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023041300357](https://openairdocs.org/sdr/YENA2023041300357.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing Spar
  > DURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / UPPER SKIN PANEL / UPPER SURFACE / FRAME 41-42 / STIFF 16-17 / CORROSION DAMAGE - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023041300356](https://openairdocs.org/sdr/YENA2023041300356.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing Structure
  > DURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL 2 / TRAILING EDGE OVERHANG / RIBS 13-16 & 18-20 AND WX3493 & WX4010 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023041300355](https://openairdocs.org/sdr/YENA2023041300355.md): Unknown · unknown · Apr 12, 2023 · N529JB · Airbus A320232 · Wing Structure
  > DURING HEAVY MAINTENANCE: WINGS / RH WING / TOP SKIN PANEL 2 / TRAILING EDGE OVERHANG / BETWEEN GEAR RIB 5 AND RIB 18 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)

Next page: https://openairdocs.org/aircraft/N529JB/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 = 'N529JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N529JB/reports

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