# Service difficulty reports: N534JB

A list on [N534JB](https://openairdocs.org/aircraft/N534JB.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 · 62 reports

- [SDR YENA2024111301476](https://openairdocs.org/sdr/YENA2024111301476.md): Girt Bar · abnormal · Nov 11, 2024 · N534JB · Airbus A320232 · Emergency Exits
  > FLT#605, EWR-FLL. 'FOUND GIRT BAR FITTING AT L1 DOOR DAMAGED/ NOT SPRINGING UP PROPERLY; REMOVED AND REPLACED L1 DOOR AFT GIRT BAR FITTING IAW AMM 52-11-31. ALL OPS CHECKS NORMAL.'
- [SDR YENA2023122101620](https://openairdocs.org/sdr/YENA2023122101620.md): Unknown · unknown · Dec 18, 2023 · N534JB · Airbus A320232 · Aircraft Fuel Distribution System
  > FLT#809, JFK-SDQ. (AIR CRAFT PERFORMED AN AIR TURN BACK) 'FUEL OUTTER WING TANK TRNAS MESSAGE INTMT AFTER TAKEOFF. BOTH OUTTER WING TANK GATES CYCLED CLOSED AND OPEN WITH THE RIGHT OUTTER WING TANK GATE SHOWED "XX" ( OUTER TO INNER TANK TRANSFER VALVES (INTER
- [SDR YENA2023101101234](https://openairdocs.org/sdr/YENA2023101101234.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: REPLACE FRAME FOOT 43 LH DUE TO CRACK OUT OF LIMITS IN PASSENGER CABIN; REF AEROMAN NR 2023-483107 WO: 2023 276/1, REMOVED AND REPLACED FITTING FRAME AND FRAME FOOT LOC FRAME 43 LH SIDE BTW STRINGER 18 AND 24 PASSENGER CABIN I.A.W A32
- [SDR YENA2023101101233](https://openairdocs.org/sdr/YENA2023101101233.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 66 LH, DOOR STOP 7, UPPER INB HOLE AT AFT GA LLEY AREA (1 EA) (CRACK DIRECTION AT 1 AND 7 O CLOCK, D= 0.100 IN); (RESOLVED ON W/O: 1242939 TASKCARD: NR-00014) REF. AEROMAN N/R 2023- 482974 WO 2023 276/1, PERF
- [SDR YENA2023101101232](https://openairdocs.org/sdr/YENA2023101101232.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage, Stabilizer Attach Fittings
  > CRACK INDICATION ON FRAME 68 LH, DOOR STOP 4, LOWER INB HOLE AT AFT GA LLEY AREA (1 EA) (CRACK DIRECTION AT 5 O CLOCK.D= 0.130); (RESOLVED ON W/O: 1242939 TASKCARD: NR-00026) FUR-A320-53-00896 REF AEROMAN N/R 2023- 482975, PERFORMED PERMANENT REPAIR ON FRAME 6
- [SDR YENA2023101101231](https://openairdocs.org/sdr/YENA2023101101231.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH, DOOR STOP 6, LOWER INB HOLE AT AFT GA LLEY AREA (1 EA) (CRACK DIRECTION AT 8 O CLOCK,D= 0.120 IN); (RESOLVED ON W/O: 1242939 TASKCARD: NR-00027) FUR-A320-53-00897 REF AEROMAN N/R 2023-482976, PERFORME
- [SDR YENA2023101101230](https://openairdocs.org/sdr/YENA2023101101230.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH, DOOR STOP 6, LOWER INB HOLE AT AFT GA LLEY AREA (1 EA) (CRACK DIRECTION AT 8 O CLOCK, D= 0.120 IN); REF AEROMAN N/R 2023- 482976, PERFORMED PERMANENT REPAIR IAW SRM 53-41-12-300-008, IAW A320 SRM 53-
- [SDR YENA2023101101229](https://openairdocs.org/sdr/YENA2023101101229.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Horizontal Stabilizer Structure
  > DURING HEAVY MAINTENANCE: CPCP CORROSION ON TIP ELEVATOR O/B RIB EXTERNAL SURFACE ON RH HORIZONTAL STAB;(RESOLVED ON W/O: 1242939 TASKCARD: NR-00030) REF; ARM W/O 2023-276/1 N/R 2023-482725 REMOVED AND REPLACED TIP ELEVATOR OUTBOARD RIB 10 LOCATED IN EXTERNAL
- [SDR YENA2023101101228](https://openairdocs.org/sdr/YENA2023101101228.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Elevator Structure
  > DURING HEAVY MAINTENANCE: BROKEN PLATE ATTACH FITTING 6 ON ELEVATOR L/H; PERFORMED PERMANENT REPAIR ON HINGE ATTACH FITTING 6 ON ELEVATOR LH THIS REPAIR IS CATEGORY A, REPETITIVE INSPECTION IS NOT REQUIRED IAW A320 SRM 55-26-41-300-003 ACCOMPLISHED ON AEROMAN
- [SDR YENA2023101101227](https://openairdocs.org/sdr/YENA2023101101227.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Wing Structure
  > DURING HEAVY MAINTENANCE: CORROSION RETRACTION ACTUATOR ATTACHMENT BRACKET ON LH MAIN LANDING GEAR; (RESOLVED ON W/O: 1242939 TASKCARD: NR-00031) WORK ACP ON AEROMAN W/0: 2023 276/1 NRC 2023-483129 REPAIRED JACK RETRACTION ACTUATOR ANCHORAGE FITTING RH MLG. FI
- [SDR YENA2023101101226](https://openairdocs.org/sdr/YENA2023101101226.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (CRCK INDICATION FOUND ON WINDSHIELD RH CENTER POST, DIRECTION OF CRACK IS 11 O CLOCK AROUND OF UPPER BOLT, LENGTH OF CRACK IS 0.100 INCHES APPROX); REF AEROMAN WO 2023 276/1 NR 2023-482826 AC
- [SDR YENA2023101101225](https://openairdocs.org/sdr/YENA2023101101225.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (CRACK INDICATION FOUND ON WINDSHIELD RH CONTINUITY FITTING, CRACK IS IN VERTICL DIRECTION, LENGTH OF CRACK IS 0.230 INCHES APPROX; REF AEROMAN WO 2023 276/1 NR 2023-482830 ACCOMPLISHED REPAIR
- [SDR YENA2023101101224](https://openairdocs.org/sdr/YENA2023101101224.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Wing Structure
  > DURING HEAVY MAINTENANCE: CORROSION SKIN PANEL LOWER SURFACE TOP SKIN (AREA OVERHANG) REAR SPAR RIB 13 PLUS 20 INCHES RH WING; REF AEROMAN WO 2023 276/1 NR 2023-483032 ACCOMPLISH REPAIR OF 3 CORROSION SPOTS WERE FOUND ON RH WING TOP SKIN PANEL 2 TRAILING EDGE
- [SDR YENA2023101101223](https://openairdocs.org/sdr/YENA2023101101223.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION SKIN PANEL LOWER SURFACE TOP SKIN (AREA OVERHANG) REAR SPAR AT RIB 14 PLUS 17 INCHES ON RH WING; REF AEROMAN WO 2023 276/1 NR 2023-483033 ACCOMPLISH REPAIR OF 3 CORROSION SPOTS WERE FOUND ON RH WING TOP SKIN PANEL 2 TRAILING
- [SDR YENA2023101101222](https://openairdocs.org/sdr/YENA2023101101222.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION SKIN PANEL LOWER SURFACE TOP SKIN (AREA OVERHANG) REAR SPAR AT RIB 15 PLUS 18 INCHES ON RH WING; REF AEROMAN WO 2023 276/1 NR 2023-483034 ACCOMPLISH REPAIR OF 3 CORROSION SPOTS WERE FOUND ON RH WING TOP SKIN PANEL 2 TRAILING
- [SDR YENA2023101101221](https://openairdocs.org/sdr/YENA2023101101221.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME IN PASSENGER CABIN (1 EA) (CRACK INDICATION FOUND OPEN HOLE 6 LOC FRAME 16 RH DOUBLE JOGGLE AREA. CRACK DIRECTION 10 OCLOCK.); REF AEROMAN WO 2023 276/1 NR 482849 ACCOMPLISHED REPAIR OF CRACK AT HOLE #6,B AND
- [SDR YENA2023101101220](https://openairdocs.org/sdr/YENA2023101101220.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: REMOVE AND REPLACE FRAME 16 RH ON UPPER FUSELAGE; REF AEROMAN WO 2023 276/1 NR 2023-483177 ACCOMPLISHED REPAIR OF CRACK AT HOLE #6,B AND E AT FR16 RH DOUBLE JOGGLE AREA IN ACCORDANCE WITH EA# 53-0306-23 COVER, P1 THRU P6, RDAF 8127240
- [SDR YENA2023101101219](https://openairdocs.org/sdr/YENA2023101101219.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: DURING EMERGENCY LIGHT TEST FWD EPSU SHOWS UNIT FAULT WHEN PRESSING P/B TEST AT FWD GALLEY AREA; REF AEROMAN WO 2023 276/1 NR 483190 REMOVED AND REPLACED POWER SUPPLY UNIT (EPSU) AND SLIDE RAFT DOOR 831 AT FWD GALLEY ARE IAW AMM 33-51
- [SDR YENA2023101101218](https://openairdocs.org/sdr/YENA2023101101218.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH, DOOR STOP 6, LOWER INB HOLE AT AFT GA LLEY AREA (1 EA) (CRACK DIRECTION AT 8 O CLOCK, D= 0.120 IN); REF AREOMAN NR 2023-482975 PERFORMED PERMANENT REPAIR ON FRAME 68 RH, DOOR STOP 6, LOWER AFT GALLEY A
- [SDR YENA2023101101217](https://openairdocs.org/sdr/YENA2023101101217.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH, DOOR STOP 4, LOWER INB HOLE AT AFT GA LLEY AREA (1 EA) (CRACK DIRECTION AT 5 O CLOCK. D= 0.130); REF AEROMAN WO 2023 276/1 NR 2023-482975 ACCOMPLISHED REPAIR OF CRACK AFFECTING FR68 LHS, AT LEVEL OF DO
- [SDR YENA2023101001216](https://openairdocs.org/sdr/YENA2023101001216.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / FR16 RH DOUBLE JOGGLE AREA / HOLE#6, B, C AND E / CRACK. PERMANENT REPAIR.(CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023101001215](https://openairdocs.org/sdr/YENA2023101001215.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / LOWER ATTACHMENT AREA / UPPER POTFACE FASTENER RH AND CONTINUIRT FITTING RH / CRACK. PERMANENT REPAIR.(CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023101001214](https://openairdocs.org/sdr/YENA2023101001214.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: WINGS / RH WING / TOP SKIN PANEL 2 TEOH RIBS 13-16 / CORROSION. TEMPORARY REPAIR.(CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023101001213](https://openairdocs.org/sdr/YENA2023101001213.md): Unknown · unknown · Oct 9, 2023 · N534JB · Airbus A320232 · Horizontal Stabilizer Structure
  > DURING HEAVY MAINTENANCE: CPCP CORROSION ON TIP ELEVATOR O/B RIB EXTERNAL SURFACE ON RH HORIZONTAL STAB; REF; ARM W/O 2023-276/1 N/R 2023-482725 REMOVED AND REPLACED TIP ELEVATOR OUTBOARD RIB 10 LOCATED IN EXTERNAL SURFACE ON RH HORIZONTAL STABILIZER IAW A320
- [SDR YENA2023052500551](https://openairdocs.org/sdr/YENA2023052500551.md): Unknown · unknown · May 22, 2023 · N534JB · Airbus A320232 · Cabin Pressure Control System
  > FLT#137, JFK-STI. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK AND DECLARED AN EMERGENCY) ' CAB PR EXCESS CAB PR ALT'. (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2023020900145](https://openairdocs.org/sdr/YENA2023020900145.md): None · failed · Feb 7, 2023 · N534JB · Airbus A320232 · Drag Control System
  > FLT#954, SJU-FLL. 'SEC #3 FAULT DURING FINAL DESCENT WITH STRONG ELECTRICAL ODOR; PERFORMED TSM 24-00-00-810-823-A. IDENTIFIED SOURCE OF BURNT ELECTRICAL ODOR TO THE SEC3. REPLACED SEC 3 IAW AMM TASK 27-94-34. OPS CHECK NORMAL.'
- [SDR YENA2022041200357](https://openairdocs.org/sdr/YENA2022041200357.md): Epsu · failed · Apr 8, 2022 · N534JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, UNIT FAUL EPSU 10WL FWD GALLEY AREA; REF AEROMAN NR 2022-145724 WO 2000 70/1 PERFORMED TSM UNIT FAULT ON EPSU 10WL FWD GALLEY AREA IAW TSM 33-51-00-810-801-A REMOVED AND REPLACED SERVICEABLE EPSU 10WL IAW 33-51-38-400-001-A AND PERFOR
- [SDR YENA2022041200356](https://openairdocs.org/sdr/YENA2022041200356.md): None · none · Apr 8, 2022 · N534JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE, CORROSION LOCATED ON RIB 10 PLUS 5 INCH UPPER SKIN LOWER SURFACE TRAILING EDGE LH WING; ACCOMPLISHED PER JB EA 57-0091-22
- [SDR YENA2022041200355](https://openairdocs.org/sdr/YENA2022041200355.md): None · none · Apr 8, 2022 · N534JB · Airbus A320232 · Wing, Control Surfaces
  > DURING HEAVY MAINTENANCE, CORROSION TE RIB 10-11 OVERHANG LH WING; ACCOMPLISHED PER JETBLUE EA 57-0091-22
- [SDR YENA2022041200354](https://openairdocs.org/sdr/YENA2022041200354.md): Skin Panel · corroded · Apr 8, 2022 · N534JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, WINGS / LH WING / TOP SKIN PANEL / TE OVERHANG / LOWER SURFACE / RIBS 10-11 / CORROSION – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2021122700868](https://openairdocs.org/sdr/YENA2021122700868.md): Computer · failed · Dec 21, 2021 · N534JB · Airbus A320232 · Trailing Edge Flap Control System
  > FLT 765, JFK-GCM (AIR TURN BACK TO JFK).F/CTL FLAP SYS 1 FAULT UPON RETRACTION AFTER T/O; TROUBLESHOT TO SFCC1. R/R SFCC1. REF TO AMM 27-51-34. OPS CHECK GOOD. OK FOR SVC. REF TO TSM 27-51-00-810-808A
- [SDR YENA2021031000159](https://openairdocs.org/sdr/YENA2021031000159.md): Battery · failed · Mar 5, 2021 · N534JB · Airbus A320232 · Emergency Lighting
  > FLT 291, BOS-TPA. EMERGENCY LIGHT TEST FAILED BATERY FIN# 13WL; R & R EMERGENCY LIGHT BATTERY FIN# 13WL PER AMM 33-51-38
- [SDR YENA2021030500147](https://openairdocs.org/sdr/YENA2021030500147.md): Battery · failed insp · Mar 5, 2021 · N534JB · Airbus A320232 · Emergency Lighting
  > FLT # 291, BOS-TPA. EMERCENCY LIGHT TEST FAILED BATTERY FIN#10WL; EMERCENCY LIGHT TEST FAILED BATTERY FIN#10WL
- [SDR YENA2020022400194](https://openairdocs.org/sdr/YENA2020022400194.md): Battery · no test · Feb 20, 2020 · N534JB · Airbus A320232 · Emergency Lighting
  > FT # 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED; R & R EMERGENCY LIGHT BATTERY AT FIN# 11WL PER AMM 33-51-38
- [SDR YENA2019062620343](https://openairdocs.org/sdr/YENA2019062620343.md): Battery Pack · failed · Jun 22, 2019 · N534JB · Airbus A320232 · Emergency Lighting
  > FT # 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED EPSU BATTERY AT 12WL; REMOVED & REPLACED EMERGENCY LIGHT BATTERY AT EPSU FIN 12WL PER AMM 33-51-38.
- [SDR YENA201710180845](https://openairdocs.org/sdr/YENA201710180845.md): Wire · broken · Oct 18, 2017 · N534JB · Airbus A320232 · Light System Wiring
  > EMERGENCY LIGHT ROW 1ABC INOPERATIVE. FOUND A BROKEN WIRE AT CONNECTOR VC5751A. REMOVED & REPLACED WIRE HARNESS. OPS NORMAL IAW AMM 33-51-00-710--001-A.
- [SDR YENA201709210776](https://openairdocs.org/sdr/YENA201709210776.md): Power Supply · inoperative · Sep 21, 2017 · N534JB · Airbus A320232 · Emergency Lighting
  > ROW 1 EMERGENCY LIGHTS FOUND INOPERATIVE. THE FWD POWER SUPPLY WAS FOUND TO BE FAULTY. R & R THE FWD POWER SUPPLY IAW AMM 33-51-00. NO FURTHER PROBLEMS NOTED.
- [SDR YENA201708160668](https://openairdocs.org/sdr/YENA201708160668.md): Floor Support · corroded · Aug 16, 2017 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y254 BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53110900.
- [SDR YENA201708160667](https://openairdocs.org/sdr/YENA201708160667.md): Floor Support · corroded · Aug 16, 2017 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT -Y254 BETWEEN FRAMES 12 TO 24 FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53110900.
- [SDR YENA201705260403](https://openairdocs.org/sdr/YENA201705260403.md): Battery · failed · May 26, 2017 · N534JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY FAULT AT 11WL. R & R EMERGENCY LIGHT BATTERY UNIT IAW AMM 33-51-38.
- [SDR YENA20160117048](https://openairdocs.org/sdr/YENA20160117048.md): Dummy Rail · corroded · Jan 17, 2016 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > THE DUMMY RAIL AT LT SIDE FROM FRAMES 65 TO 67 HAS CORROSION AT FRAME 66. R & R DUMMY RAIL IAW SRM 51-72-11.
- [SDR YENA20160117047](https://openairdocs.org/sdr/YENA20160117047.md): Support · corroded · Jan 17, 2016 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > SUPPORT FITTING FOR THE RT AFT SHEAR WEB HAS CORROSION AT FRAME 69 TO 70. R & R THE SUPPORT FITTING IAW SRM 51-72-11.
- [SDR YENA20160117046](https://openairdocs.org/sdr/YENA20160117046.md): Support · corroded · Jan 17, 2016 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > THE LT AFT SHEAR WEB SUPPORT HAS CORROSION AT FRAMES 69 TO 70. R & R THE SUPPORT IAW SRM 51-73-11.
- [SDR YENA20160117045](https://openairdocs.org/sdr/YENA20160117045.md): Floor Support · corroded · Jan 17, 2016 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT Y-1292 HAS CORROSION AT FRAME 68. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA20160117044](https://openairdocs.org/sdr/YENA20160117044.md): Floor Support · corroded · Jan 17, 2016 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT Y-1292 HAS CORROSION AT FRAME 66. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA20160117043](https://openairdocs.org/sdr/YENA20160117043.md): Floor Support · corroded · Jan 17, 2016 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAS CORROSION JUST FWD OF FRAME 66 SPLICE. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA20160117042](https://openairdocs.org/sdr/YENA20160117042.md): Floor Support · corroded · Jan 17, 2016 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT Y-1292 HAS CORROSION AT FRAME 68. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA20160117041](https://openairdocs.org/sdr/YENA20160117041.md): Dummy Rail · corroded · Jan 17, 2016 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > THE DUMMY RAIL J939 HAS CORROSION AT FRAME 66. R & R DUMMY RAIL IAW 51-42-11, P1-9,51-44-11, P 1-9, 51-21-11, P1-30.
- [SDR YENA20160117040](https://openairdocs.org/sdr/YENA20160117040.md): Floor Support · corroded · Jan 17, 2016 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAS CORROSION FRAMES 66 & 68. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA20160117039](https://openairdocs.org/sdr/YENA20160117039.md): Floor Support · corroded · Jan 17, 2016 · N534JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOORBEAM Y-1292 HAS CORROSION AT FRAMES 66 & 68. R & R THE FLOOR SUPPORT IAW 51-72-11.

Next page: https://openairdocs.org/aircraft/N534JB/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 = 'N534JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N534JB/reports

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