# Service difficulty reports: N526JL

A list on [N526JL](https://openairdocs.org/aircraft/N526JL.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 · 112 reports

- [SDR YENA2025042900449](https://openairdocs.org/sdr/YENA2025042900449.md): Hinge Fitting · not reported · Apr 26, 2025 · N526JL · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: REMOVED AND REPLACED HINGE FITTING VERTICAL STABILIZER IAW A320 SRM 51-72-11 AND IAW A320 SRM 55-36-42-300-008 AND AMM 27-21-41-000-001-A STEP 4A(7) RII AND WORK ACCOMPLISHED ON AEROMAN WO:2025 129/1 NON-ROUTINE 2025-202316.
- [SDR YENA2025042900448](https://openairdocs.org/sdr/YENA2025042900448.md): Fitting · corroded · Apr 26, 2025 · N526JL · Airbus A320232 · Vertical Stabilizer Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: SECONDARY FINDING AFTER REMOVED BEARING CORROSION FOUND ON BORE HINGEARM FITTING N5 VERTICAL STABILIZER; REMOVED AND REPLACED HINGE FITTING #5 VERTICAL STABILIZER IAW A320 SRM 51-72-11 AND SRM A320 55-36-42-300-008. RII AND WORK ACCOM
- [SDR YENA2025042900447](https://openairdocs.org/sdr/YENA2025042900447.md): Fitting · corroded · Apr 26, 2025 · N526JL · Airbus A320232 · Vertical Stabilizer Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: SECONDARY FINDING: AFTER REMOVED BEARING, CORROSION FOUND ON BORE HINGE ARM FITTING #4 VERTICAL STABILIZER; REMOVED AND REPLACED HINGE FITTING #4 VERTICAL STABILIZER IAW A320 SRM 51-72-11 AND SRM A320 55-36-42-300-008. RII AND WORK AC
- [SDR YENA2025042900446](https://openairdocs.org/sdr/YENA2025042900446.md): Frame · cracked · Apr 26, 2025 · N526JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND OPEN HOLE B FR16LH LOC DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOK (VIEW OUTSIDE SKIN) CRACK DEPTH 0.100 INCH; (RESOLVED ON W/O: 1356112 TASKCARD: NR-00040) PERFORMED PERMANENT REPAIR ON HOLE B LOC FR16LH LOC DO
- [SDR YENA2025042900445](https://openairdocs.org/sdr/YENA2025042900445.md): Frame · cracked · Apr 26, 2025 · N526JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND OPEN HOLE B FR16LH LOC DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK (VIEW OUTSIDE SKIN) CRACK DEPTH 0.100 INCH; PERFORMED PERMANENT REPAIR ON HOLE B LOC FR16LH LOC DOUBLE JOGGLE AREA DIRECTION 9 OCLOCK IAW A320
- [SDR YENA2025042900444](https://openairdocs.org/sdr/YENA2025042900444.md): Bottle · damaged · Apr 26, 2025 · N526JL · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE: DIFFICULTY INSTALL SAFETY PIN IN LH OVERWING BOTTLE; REMOVED AND REPLACED LH OVERWING BOTTLE IN AFT CARGO COMPARTMENT IAW AMM 25-62-46-000-001-A AND AMM 25-62-46-400-001. ALL WORK WQS PERFORMED BY AEROMAN WO2025 129/1 NR 2025-202165/
- [SDR YENA2025010700025](https://openairdocs.org/sdr/YENA2025010700025.md): Unknown · odor · Jan 1, 2025 · N526JL · Airbus A320232 · Air Distribution System
  > FLT#405, EWR-FLL. 'F1 REPORTED MOMENTARY PATRID/DIRTY SOCK SMELL ON CLIMBOUT DID NOT RECURR. CABIN ODOR REPORTING FORM COMPLETED; COMPLIED WITH INFO-NOTICE 2017-T015K INSPECTED APU AND FOUND IN CLEAN CONDITION WITH NO LEAKS. INSP AFT FUSELAGE AND FOUND NO EVID
- [SDR YENA2024032600469](https://openairdocs.org/sdr/YENA2024032600469.md): O-Ring · leaking · Mar 25, 2024 · N526JL · Airbus A320232 · Hydraulic System, Main
  > FLT#2592, MIA-JFK. (AIRCRAFT DECLARED AN EMERGENCY INTO JFK) ' Y RSVR LO LVL IN FLIGHT; FOUND HYDRAULIC LEAKS COMING FROM PTU. QUICK DISCONNECT R/R DAMAGED O-RING REF AMM 29-23-00 PERFORMED LEAK CHECK, LEAK CHECK GOOD. REPLENISHED HYD SYSTEM REF AMM 12-12-29.
- [SDR YENA2022120901239](https://openairdocs.org/sdr/YENA2022120901239.md): Uplock · missing · Dec 5, 2022 · N526JL · Airbus A320232 · Landing Gear Retraction/Extension System
  > FLT#1422, MSY-FLL. 'FOUND NLG DOOR UPLOCK MISSING SPRING; REMOVED AND REPLACED NLG DOOR UPLOCK ASSY PER AMM 32-31-14. OPS AND FUNCTION CHECK GOOD. LEAK CHECK OK.'
- [SDR YENA2022083000842](https://openairdocs.org/sdr/YENA2022083000842.md): Skin Panel · corroded · Aug 25, 2022 · N526JL · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE BETWEEN RIB1 TO RIB2 ON LH WING (REFER TO THE MPD TASK ZL-500-03); ACCOMPLISHED REPAIR OF THE CORROSION ON THE LH WING TOP SKIN PANEL 2 UPPER SURFACE AT LEVEL OF RIBS 1 AND 2 AND STRINGER 16 IAW
- [SDR YENA2022083000841](https://openairdocs.org/sdr/YENA2022083000841.md): Window Post · cracked · Aug 25, 2022 · N526JL · Airbus A320232 · Flight Compartment Windows
  > DURING HEAVY MAINTENANCE: CRACK: FR2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LH SIDE L=0.160"; REF AEROMAN NR 2022-400154 W/O: 2022 182/1: REMOVED AND REPLACED LH AND RH CONTINUITY FITTINGS FR1-2 IAW SRM 51-72-11-911-001 AND REPAIR
- [SDR YENA2022083000840](https://openairdocs.org/sdr/YENA2022083000840.md): Coupling · damaged · Aug 25, 2022 · N526JL · Airbus A320232 · Fuselage Main, Keel
  > DURING HEAVY MAINTENANCE: PERFORM REPAIR FR43 FOOT COUPLING LH; REF AEROMAN NR 2022-400417 W/O: 2022 182/1: REPAIRED FRAME FOOT COUPLING AND SUPPORT FR43LH IAW JB EC A320-53-1269-02 AND REPAIR INSTRUCTION R53370233.
- [SDR YENA2022083000839](https://openairdocs.org/sdr/YENA2022083000839.md): Coupling · cracked · Aug 25, 2022 · N526JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK: FR43 FOOT COUPLING STR21-22RH; REF AEROMAN NR 2022-400387 W/O: 2022 182/1: REMOVED AND REPLACED FRAME FOOT COUPLING FR43 STR18-24RH IAW SRM 51-42-11, 51-72-11, JB EC A320-53-1269-02, AND REPAIR INSTRUCTION R53370232.
- [SDR YENA2022083000838](https://openairdocs.org/sdr/YENA2022083000838.md): Stop Fitting · cracked · Aug 25, 2022 · N526JL · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK HOLE 5 DOUBLE JOGGLE AREA FR20RH AND #7 DOOR STOP FITTING LEVEL AT FWD GALLEY (D=0.061" 2 O'CLOCK DIRECTION); REF AEROMAN NR 2022-400196 W/O: 2022 182/1: REPAIRED HOLE #5 DOUBLE JOGGLE AREA FR20RH AND #7 DOOR STOP FITTING IAW RE
- [SDR YENA2022083000837](https://openairdocs.org/sdr/YENA2022083000837.md): Stop Fitting · cracked · Aug 25, 2022 · N526JL · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK (2EA): FR16RH DOOR STOP FITTING #7 UPPER INBD HOLE (D=0.080 6 O'CLOCK DIRECTION) AND LOWER INBD HOLE (D=0.124" 8 & 10 O'CLOCK DIRECTION); REF AEROMAN NR 2022-400210 & 400211 W/O: 2022 182/1: REMOVED AND REPLACED INTERCOSTAL FR16
- [SDR YENA2022083000836](https://openairdocs.org/sdr/YENA2022083000836.md): Stop Fitting · cracked · Aug 25, 2022 · N526JL · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK (2EA): FR16LH DOOR STOP FITTING #7 UPPER INBD HOLE (D=0.094" AT 5 O'CLOCK DIRECTION) AND LOWER INBD HOLE (D=0.123" AT 4 & 12 O'CLOCK DIRECTION); REF AEROMAN NR 2022-400205 & 400207 W/O: 2022 182/1: REMOVED AND REPLACED INTERCOST
- [SDR YENA2022083000835](https://openairdocs.org/sdr/YENA2022083000835.md): Stringer · corroded · Aug 25, 2022 · N526JL · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOCATED BTW FRAME 56 AND FRAME 57 IN AFT CARGO COMPARTMENT (CPCP RELATED MPD TASK 534107-01); REMOVED AND REPLACEDSTRINGER 43L AND FASTENERS LOCATED BTW FRAME 54AND FRAME 60 IN AFT CARGO COMPARTMENT AS PER A320
- [SDR YENA2022062900640](https://openairdocs.org/sdr/YENA2022062900640.md): None · none · Jun 28, 2022 · N526JL · Airbus A320232 · Emergency Lighting
  > FLT#38, SJO-FLL. 'OVERHEAD EMERGENCY EXIT LIGHT; REPLACED AFT O/H EMERGENCY LT ASSY PER AMM: 33-51-17, OPS CHECK OK. MX-4 UPDATED. PLACARD REMOVED AND DISPATCH NOTIFIED. E49679 AND MCC NOTIFIED.'
- [SDR YENA2021111000745](https://openairdocs.org/sdr/YENA2021111000745.md): Unknown · odor · Nov 3, 2021 · N526JL · Airbus A320232 · Air Distribution System
  > FLT 2855, CHS-LGA. DIRTY SOCK SMELL BY ALL 4 FLIGHT ATTENDANTS FROM 10,000 FT THROUGHOUT DESCENT AND TAXI INTO GATE; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10,A,1,C PER TSM 05-50-00-810-085B. AIRCRAFT IS OK FOR SERVICE.
- [SDR YENA2020040610270](https://openairdocs.org/sdr/YENA2020040610270.md): Door Sill · corroded · Apr 1, 2020 · N526JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION LOWER SILL UPPER SURFACE FR 66-68 LH SIDE; (REF AEM NR 2020-28/1-2020-90695) R & R LOWER SILL BETWEEN FR 66-68 LH SIDE IAW A320 SRM 51-72-11, DWG D53480009, D53474250
- [SDR YENA2020040610269](https://openairdocs.org/sdr/YENA2020040610269.md): Floorbeam · corroded · Apr 1, 2020 · N526JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION ON FLOOR BEAM +Y1292 FR 66-68; (REF AEM NR 2020-28/1-2020-90687) R & R FLOOR BEAM +Y1292 BETWEEN FR66-68 IAW A320 SRM 51-72-11 DWG 53472815
- [SDR YENA2020040610268](https://openairdocs.org/sdr/YENA2020040610268.md): Skin · dented · Apr 1, 2020 · N526JL · Airbus A320232 · Leading Edge Devices
  > DURING HEAVY MAINTENANCE, DENT UPPER SKIN SLAT 1 11 INCHECS FROM OUTBOARD EDGE LH WING; REF AEROMAN N/R W/O# 2020-28/1 WCC#2020-90658 PERFORMED PERMANENT REPAIR ON UPPER SKIN SLAT 1 OUTBOARD EDGE ON LH WING IAW SRM A320-57-42-21-300-006 PARA 2.A. FIG 001 (SHEE
- [SDR YENA2020040610267](https://openairdocs.org/sdr/YENA2020040610267.md): Crossbeam · cracked · Apr 1, 2020 · N526JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CRACK INDICATION AT FR 16 CROSSBEAM HOLE 8 AND HOLE 18, FR 20 CROSSBEAM HOLE 17 AND HOLE 26; REF AEM NR'S 2020-28/1-2020-90691/90692/90693/90694 - PERFORMED PERMANENT CAT A REPAIR IAW A320 SB A320-53-1286 AND JB EC A320-53-1286-01
- [SDR YENA201904290251](https://openairdocs.org/sdr/YENA201904290251.md): Battery · failed · Apr 29, 2019 · N526JL · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED EPSU BATTERIES FIN 10WL AND 13WL; REMOVED & REPLACED EMERGENCY LIGHT BATTERIES AT FIN 10WL AND 13WL PER AMM 33-51-38.
- [SDR YENA201904290250](https://openairdocs.org/sdr/YENA201904290250.md): Battery · failed · Apr 29, 2019 · N526JL · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED EPSU BATTERIES FIN 10WL AND 13WL; REMOVED & REPLACED EMERGENCY LIGHT BATTERIES AT FIN 10WL AND 13WL PER AMM 33-51-38.
- [SDR YENA2019040850181](https://openairdocs.org/sdr/YENA2019040850181.md): Battery Pack · no test · Apr 5, 2019 · N526JL · Airbus A320232 · Emergency Lighting
  > FT # 391, EMERGENCY LIGHT TEST FAILS BATTERIES 11WL AND 12WL; R & R 11WL AND 12WL BATTERIES IAW AMM 33-51-38. OPS CHECK OK.
- [SDR YENA2019040850180](https://openairdocs.org/sdr/YENA2019040850180.md): Battery Pack · no test · Apr 5, 2019 · N526JL · Airbus A320232 · Emergency Lighting
  > FT # 391, EMERGENCY LIGHT TEST FAILS BATTERIES 11WL AND 12WL; R & R 11WL AND 12WL BATTERIES IAW AMM 33-51-38. OPS CHECK OK.
- [SDR YENA2018112070781](https://openairdocs.org/sdr/YENA2018112070781.md): Bulb · inoperative · Nov 17, 2018 · N526JL · Airbus A320232 · Emergency Lighting
  > FT # 1654,SJU-FLL. MID CABIN OVERHEAD EMERGENCY EXIT LIGHT ONLY HAS ONE LIGHT BULB WORKING; RELAMPED PER AMM 33-51-17 ALL BULBS CKS OK.
- [SDR YENA201805040199](https://openairdocs.org/sdr/YENA201805040199.md): Battery · discharged · May 4, 2018 · N526JL · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EMER LIGHT FAILS TEST. R&R EMER LIGHT BATTERY AT 10WL AND 13WL IAW AMM 33-51-38 (FILED BY EMAIL ON 5/8/2018).
- [SDR YENA201805040198](https://openairdocs.org/sdr/YENA201805040198.md): Battery · discharged · May 4, 2018 · N526JL · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EMER LIGHT FAILS TEST. R&R EMER LIGHT BATTERY AT 10WL AND 13WL IAW AMM 33-51-38 (FILED BY EMAIL ON 5/8/2018).
- [SDR YENA201801100019](https://openairdocs.org/sdr/YENA201801100019.md): Girt Bar · unserviceable · Jan 10, 2018 · N526JL · Airbus A320232 · Emergency Equipment
  > THE R2 DOOR GIRT BAR UNSERVICEABLE. REPLACED IAW AMM 25-62-44.
- [SDR YENA201801100018](https://openairdocs.org/sdr/YENA201801100018.md): Girt Bar · binding · Jan 10, 2018 · N526JL · Airbus A320232 · Emergency Equipment
  > FOUND DAMAGED GIRT BAR INSTALLED AT L2 DOOR. TRIGGER IS BOUND UP. REMOVED, CLEANED AND INSPECTED THE GIRT BAR AND FOUND IN SERVICEABLE CONDITION IAW AMM 25-62-44.
- [SDR YENA201708300719](https://openairdocs.org/sdr/YENA201708300719.md): Light · damaged · Aug 30, 2017 · N526JL · Airbus A320232 · Emergency Lighting
  > CABIN SEAT MOUNTED EMERGENCY LIGHT AT 1C FOUND TO BE DAMAGED. BENT PIN. R & R THE EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-19. OPS CHECKED NORMAL.
- [SDR YENA201701030013](https://openairdocs.org/sdr/YENA201701030013.md): Lamp · inoperative · Jan 3, 2017 · N526JL · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT 1C INOPERATIVE. REPLACED THE LAMPS AND OPS CHECK GOOD IAW AMM 33-50-00.
- [SDR YENA20160925868](https://openairdocs.org/sdr/YENA20160925868.md): Floor Support · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAMES 67-68, -Y1162. R & R THE FLOOR SUPPORT.
- [SDR YENA20160925867](https://openairdocs.org/sdr/YENA20160925867.md): Seat Track · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON SEAT TRACK FRAMES 64-66, -Y1292. R & R THE SEAT TRACK.
- [SDR YENA20160925866](https://openairdocs.org/sdr/YENA20160925866.md): Floor Support · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAMES 68- 70, Y160. R & R FLOOR SUPPORT.
- [SDR YENA20160925865](https://openairdocs.org/sdr/YENA20160925865.md): Floor Support · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAMES 64-67, -Y765. R & R THE FLOOR SUPPORT.
- [SDR YENA20160925864](https://openairdocs.org/sdr/YENA20160925864.md): Floor Support · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAMES 68-70, -Y46. R & R THE FLOOR SUPPORT.
- [SDR YENA20160925863](https://openairdocs.org/sdr/YENA20160925863.md): Floor Support · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAMES 64-67, -Y465. R & R THE FLOOR SUPPORT.
- [SDR YENA20160925862](https://openairdocs.org/sdr/YENA20160925862.md): Floor Support · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAME 68-69, -Y1162. R & R FLOOR SUPPORT.
- [SDR YENA20160925861](https://openairdocs.org/sdr/YENA20160925861.md): Floor Support · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAMES 67 -70, -Y765. R & R THE FLOOR SUPPORT.
- [SDR YENA20160925860](https://openairdocs.org/sdr/YENA20160925860.md): Floor Support · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAME 67-70, Y765. R & R THE FLOOR SUPPORT.
- [SDR YENA20160925859](https://openairdocs.org/sdr/YENA20160925859.md): Floorbeam · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON FLOORBEAM FRAME 68 -69, Y1162 LT. R & R FLOORBEAM.
- [SDR YENA20160925858](https://openairdocs.org/sdr/YENA20160925858.md): Floorbeam · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON FLOORBEAM FRAME 67-68, Y1292. R & R FLOORBEAM.
- [SDR YENA20160925857](https://openairdocs.org/sdr/YENA20160925857.md): Floorbeam · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY CHECK, CORROSION WAS FOUND ON FLOORBEAM FRAME 64-67, Y512 LT. R & R FLOORBEAM.
- [SDR YENA20160925856](https://openairdocs.org/sdr/YENA20160925856.md): Seat Track · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS FOUND ON SEAT TRACK FRAME 64-FRAME 66, Y765 LT. R & R SEAT TRACK IAW SRM 51-72-11 & 51-42-11.
- [SDR YENA20160925855](https://openairdocs.org/sdr/YENA20160925855.md): Seat Track · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON SEAT TRACK FRAME 12-16 -Y81 RT. R & R SEAT TRACK IAW SRM 51-72-11 AND SRM 51-42-11.
- [SDR YENA20160925854](https://openairdocs.org/sdr/YENA20160925854.md): Floorbeam · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM FRAME 12-16, -Y81 RT. R & R FLOORBEAM IAW SRM 51-72-11 & SRM 51-42-11.
- [SDR YENA20160925853](https://openairdocs.org/sdr/YENA20160925853.md): Floorbeam · corroded · Sep 25, 2016 · N526JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM FRAME 12-24, -Y254 RT. R & R FLOORBEAM, FRAME 12-24, -Y254 RT IAW SRM 51-72-11, REV 115 AND SRM 51-42-11, REV 115.

Next page: https://openairdocs.org/aircraft/N526JL/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 = 'N526JL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N526JL/reports

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