# Service difficulty reports: N527JL

A list on [N527JL](https://openairdocs.org/aircraft/N527JL.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 · 75 reports

- [SDR YENA2026042700430](https://openairdocs.org/sdr/YENA2026042700430.md): Unknown · odor · Apr 25, 2026 · N527JL · Airbus A320232 · Air Distribution System
  > FLT# 635, BUF-SJU. FLIGHT ATTENDANTS REPORT FUMES ON FINAL DESCENT FROM ROW 20 TO THE BACK; COMPLIED WITH INFORMATION NOTICE 2017-T015M, STEP 1 ISOLATED FAULT TO TYPE 10. APU & ENGINES RUNNED NO ODOR PRESENT. APU AREA INSPECTED NO CONTAMINATION FOUND PER TSM 0
- [SDR YENA2025102101044](https://openairdocs.org/sdr/YENA2025102101044.md): Ecs · contaminated · Oct 17, 2025 · N527JL · Airbus A320232 · Cabin Cooling System
  > FLT#48, TPA-LGA. "ODOR EVENT-DIRTY SOCKS SMELL AFT GALLEY AND BACK FEW ROWS I WAS TOLD SLIGHTY BETTER WITH PACK 1 OFF THAN IT CAME BACK; C/W INFO NOTICE 2017-T015L. PERFORMED T/S IAW TSM 05-50-00-810-831-A. DETERMINED TO BE A TYPE 1 (APU). APU HAS BEEN PLACED
- [SDR YENA2025093000972](https://openairdocs.org/sdr/YENA2025093000972.md): Unknown · odor · Sep 26, 2025 · N527JL · Airbus A320232 · Air Distribution System
  > FLT#1229, EWR-CUN. TRANSIENT ODOR EVENT DURING TAKEOFF, MODORATE NURNING SMELL THROUOUT CABIN. BEGAN TO DISIPATE DURING CLIMBOUT. ( THALES-AVANT IFE (ENTIRE SYSTEM)); REACTIVATED AVANT IFE SYSTEM IAW AVANT AMMS 44-21-00. NO HAZARDOUS CONDITION NOTED. PERFORME
- [SDR YENA2025080600805](https://openairdocs.org/sdr/YENA2025080600805.md): Fitting · not reported · Aug 2, 2025 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: REPLACE THE CONTINUITY FITTINGS IAW EAN 53-0036-25 PART N3; ACCOMPLISHED THE SECOND REPLACEMENT OF LH/RH CONTINUITY FITTINGS IAW AEM EA 53-0036-25 REV. 0 (COVER PLUS PARTS 2 AND 3), AIRBUS RDAF 81073709/033/2025#A AND EC A22-539-03. T
- [SDR YENA2025080600804](https://openairdocs.org/sdr/YENA2025080600804.md): Window Frame · cracked · Aug 2, 2025 · N527JL · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE/WINDSHIELD FRAME/CENTER POST LH & RH CONTINUITY FITTING LH/RH CRACK; ACCOMPLISHED REPAR OF THE PREVIOUSLY ACCOMPLISHED TEMP REPAIR (ORIGINAL DEFECT WAS A CRACK) ON LH CENTER POST LWR ATTACHMENT CORNER RADIUS IAW AEM EA 53-003
- [SDR YENA2025080600803](https://openairdocs.org/sdr/YENA2025080600803.md): Light · no test · Aug 2, 2025 · N527JL · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: DONT PASS EMERGENCY LIGHT TEST SLIDE RAFT ON DOOR 831; REMOVED AND REPLACED EMERGENCY ESCAPE SLIDE RAFT PASSENGER CREW DOOR 831 IAW AMM 25-62-44-000-012-A AND AMM 25-62-44-400-007-A. REF AEROMAN NR 2025-369072.
- [SDR YENA2025080600802](https://openairdocs.org/sdr/YENA2025080600802.md): Window Frame · cracked · Aug 2, 2025 · N527JL · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / WINDSHIELD FRAME / CENTER POST LH & CONTINUITY FITTING LH/RH / CRACK – PERMANENT REPAIR; REFERENCES: /1/ TEMPORARY REPAIR IAW A22-539-01 /2/ AEM EA 53-0036-25 REV 0 (COVER AND PARTS 1 - 4) /3/ AIRBUS RDAF 81073709/033/2025#
- [SDR YENA2024093001315](https://openairdocs.org/sdr/YENA2024093001315.md): Unknown · odor · Sep 27, 2024 · N527JL · Airbus A320232 · Air Distribution System
  > FLT#1447, HPN-TPA. 'FA#4 REPORTED THAT THERE WAS A DIRTY SOCK SMELL THAT WAS APPARENT FROM DESCENT & LANDING UNTIL THE L1 DOOR WAS OPENED AT WHICH TIME ALREADY SHUTDOWN; COMPLIED WITH INFORMATION 2017-T015, SECTION B2. IDENTIFIED O. SEE L/P 4046711 ITEM 2 FORT
- [SDR YENA2024081201112](https://openairdocs.org/sdr/YENA2024081201112.md): Actuator · failed · Aug 11, 2024 · N527JL · Airbus A320232 · Compressor Bleed Control
  > FLT#2066, RSW-JFK.' (AIRCRAFT DIVERTED TO JFK) 'ENG 2 STALL ECAM AT FL350, AFTER REDUCING THURST AND FOLLOWING QRH PROCEDURE STALL INDICATIONS STOPPED; REMOVED AND REPLACED #2 ENG VSV ACTUATOR IAW AMM 75-32-41. REF L.O 4046951 ITEM 2 (ACCOMPLISHED REMOVED AND
- [SDR YENA2024010200003](https://openairdocs.org/sdr/YENA2024010200003.md): Adiru · failed · Dec 29, 2023 · N527JL · Airbus A320232 · Navigation System
  > FLT#479, JFK-MBJ. (AIRCRAFT PERFORMED AN AIR TURN BACK AND DECLARED AN EMERGENCY) ' NAV 1 ADR FAULT 1 DURING FLIGHT. MADE AN EMERGENCY RETURN AND ACCOMPLISHED AN OVERWEIGHT LANDING. LANDING WEIGHT 157,000 TOUCH DOWN 250-300 FEET PER MIN. NO OVERSPEED. SMOOTH T
- [SDR YENA2023050900503](https://openairdocs.org/sdr/YENA2023050900503.md): Unknown · unknown · May 6, 2023 · N527JL · Airbus A320232 · Emergency Lighting
  > FLT#943, RNO-LAX. 'LIGHTED EXIT SIGN IN CABIN OVER OVER WING EXILT ON R APPEARS TO HAVE BURNED OUT BULBS; RELAMPED LIGHTS BULBS ON OVERWING "R" SIDE EXIT PER AMM 33-51-15. OPS CHECK NORMAL.'
- [SDR YENA2023031700255](https://openairdocs.org/sdr/YENA2023031700255.md): Unknown · unknown · Mar 16, 2023 · N527JL · Airbus A320232 · Nose/Tail Landing Gear
  > FLT#8151, LGA-JFK. 'NOSE GEAR DOOR SLOW TO CLOSE AFTER TAKE OFF CLOSED AFTER PASSING 20000 FEET WITH ECAM L/G NOSE UPLOCK ALONG WITH RED NOSE UNLOCK INDICATOR WHEN DOORS FULLY CLOSED PASSING 2030 REPEAT WRITE UP REF 3497129 ( LANDING GEAR RETRACTION SYSTEM).'
- [SDR YENA2023021300153](https://openairdocs.org/sdr/YENA2023021300153.md): None · none · Feb 9, 2023 · N527JL · Airbus A320232 · Landing Gear Retraction/Extension System
  > FLT#1463, LAX-SJD. (AIRCRAFT PERFORMED AN AIR TURN BACK TO LAX) ' AFTER ROTATION & CALL FOR GEAR UP. THE NOSE DOOR OR GEAR DID NOT CLOSE OR RETRACT. ECAM ALERT CLIMBED TO 1000' & DOOR OR GEAR RETRACTED. NO FURTHER INDICATION. CONTACT MX TOLD T TO RETURN TO LAX
- [SDR YENA2022072200672](https://openairdocs.org/sdr/YENA2022072200672.md): None · failed · Jul 21, 2022 · N527JL · Airbus A320232 · Magnetic Compass
  > FLT#2283, BOS-RDU. (AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS) ' STBY AIRSPEED UNRELIABLE; REMOVED AND REPLACED STBY AIRSPEED INDICATOR IAW AMM 34-21-26.'
- [SDR YENA2022072200702](https://openairdocs.org/sdr/YENA2022072200702.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: CROSSBEAM FOM HOLE H25 FR20 RH AFT AVIONICS COMPARTMENT L= 0.042" 1 O'CLOCK DIRECTION LOOKING AFT; REF AEROMAN NR 2022-317690 W/O: 2022 68/1: ACCOMPLISHED AD 2018-14-09-FAA-01 AND SB A320-53-1286.
- [SDR YENA2022072200701](https://openairdocs.org/sdr/YENA2022072200701.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: CROSSBEAM FROM HOLE H26 AT FR20 RH AFT AVIONICS COMPARTMENT L= 0.063" 12 O'CLOCK DIRECTION LOOKING AFT; REF AEROMAN NR 2022-317692 W/O: 2022 68/1: ACCOMPLISHED FAA AD 2018-14-09 AND SB A320-53-1286.
- [SDR YENA2022072200700](https://openairdocs.org/sdr/YENA2022072200700.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: FR20LH HOLE 26 AFT AVIONICS COMPARTMENT L=0.048" 6 O'CLOCK DIRECTION LOOKING FORWARD; REF AEROMAN NR 2022-317693 W/O: 2022 68/1: ACCOMPLISHED FAA AD 2018-14-09 AND SB A320-53-1286.
- [SDR YENA2022072200699](https://openairdocs.org/sdr/YENA2022072200699.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: FR 16LH HOLE 1 LATERAL AVIONICS COMPARTMENT LH L=0.035" 1 O'CLOCK DIRECTION LOOKING FORWARD; REF AEROMAN NR 2022-317694 W/O: 2022 68/1: ACCOMPLISHED FAA AD 2018-14-09 AND SB A320-53-1286.
- [SDR YENA2022072200698](https://openairdocs.org/sdr/YENA2022072200698.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: CROSSBEAM FROM HOLE H6 FR16LH AT LATERAL AVIONICS COMPARTMENT LH L=0.039" 1 O'CLOCK DIRECTION LOOKING FWD; REF AEROMAN NR 2022-317695 W/O: 2022 68/1: ACCOMPLISHED FAA AD 2018-14-09 AND SB A320-53-1286.
- [SDR YENA2022072200697](https://openairdocs.org/sdr/YENA2022072200697.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK 3 EA: OVERWING EMERGENCY EXIT HATCH 834. CRACK 1: 14TH FASTENER (L=0.404"), 2: 15TH FASTENER (L=0.880") AND 3: 16TH FASTENER (L=0.856") ALL FROM UPPER SIDE FWD INNER SEGMENT; REF AEROMAN NR 2022-317576 W/O: 2022 68/1: ACCOMPLIS
- [SDR YENA2022072200696](https://openairdocs.org/sdr/YENA2022072200696.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACKS 3EA: OVERWING EMERGENCY EXIT HATCH 843. CRACK 1: 6TH FASTENER (L=0.564"), CRACK 2: 8TH FASTENER (L=0.180"), CRACK 3: 9TH FASTENER (L=0.144") ALL FROM UPPER SIDE AFT INNER SEGMENT; REF AEROMAN NR 2022-317567 W/O: 2022 68/1: ACC
- [SDR YENA2022072200695](https://openairdocs.org/sdr/YENA2022072200695.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACKS 6EA: OVERWING EMERGENCY EXIT HATCH 843 FWD INNER SEGMENT UPPER SIDE. CRACK 1: 13TH FASTENER (L=0.241"), CRACK 2: 14TH FASTENER (L=0.553"), CRACK 3: 15TH FASTENER (L=0.110"), CRACK 4: 16TH FASTENER (L=0.155"), CRACK 5: 17TH FAST
- [SDR YENA2022072200694](https://openairdocs.org/sdr/YENA2022072200694.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACKS 3EA: OVERWING EMERGENCY EXIT HATCH 833 FWD INNER SEGMENT UPPER SIDE. CRACK 1: 8TH FASTENER (L=0.122"), CRACK 2: 15TH FASTENER (L=0.154"), CRACK 3: 16TH FASTENER (L=0.167"); REF AEROMAN NR 2022-317559 W/O: 2022 68/1: ACCOMPLISH
- [SDR YENA2022072200693](https://openairdocs.org/sdr/YENA2022072200693.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACKS 2EA: OVERWING EMERGENCY EXIT HATCH 844 FWD INNER SEGMENT UPPER SIDE. CRACK 1: 15TH FASTENER (L=0.187"), CRACK 2: 16TH FASTENER (L=0.342"); REF AEROMAN NR 2022-317574 W/O:2022 68/1: ACCOMPLISHED SB A320-52-1144.
- [SDR YENA2022072200692](https://openairdocs.org/sdr/YENA2022072200692.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACKS 5EA: OVERWING EMERGENCY EXIT HATCH 844 FWD INNER SEGMENT UPPER SIDE. CRACK 1: 13TH FASTENER (L=0.183"), CRACK 2: 14TH FASTENER (L=0.592"), CRACK 3: 15TH FASTENER (L=0.115"), CRACK 4: 16TH FASTENER (L=0.672"), CRACK 5: 17TH FAST
- [SDR YENA2022072200691](https://openairdocs.org/sdr/YENA2022072200691.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACKS 4EA: OVERWING EMERGENCY EXIT HATCH 834 FWD INNER SEGMENT UPPER SIDE. CRACK 1: 8TH FASTENER (L=0.121"), CRACK 2: 16TH FASTENER (L=0.693"), CRACK 3: 17TH FASTENER (L=0.610"), CRACK 4: 18TH FASTENER (L=0.592"); REF AEROMAN NR 2022
- [SDR YENA2022072200690](https://openairdocs.org/sdr/YENA2022072200690.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION: STR43L FR64-65 AFT CARGO; REF AEROMAN NR 2022-317689 W/O: 2022 68/1: REPAIRED IAW SRM 53-41-13-300-004. CAT A REPAIR, NO FURTHER ACTION REQUIRED.
- [SDR YENA2022072200689](https://openairdocs.org/sdr/YENA2022072200689.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Engine Cowling System
  > DURING HEAVY MAINTENANCE: CORROSION: ENGINE #1 INLET BARREL LIP SKIN 6 O'CLOCK POSITION; REF AEROMAN NR 2022-317490 W/O"2022 68/1: REPAIRED LIP SKIN #1 ENGINE 6 O'CLOCK POSITION IAW GOODRICH AEROSTRUCTURES SRM 54-10-00 REPAIR 19 AND SPM TASK 70-39-03-390-501.
- [SDR YENA2022072200688](https://openairdocs.org/sdr/YENA2022072200688.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: FASTENER HOLE OF THE DOOR STOP N7 FR16LH AT LOWER INBOARD HOLE; REF AEROMAN NR 2022-317799 W/O:2022 68/1: REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS AT FR16LH LOWER INBOARD HOLE LEVEL OF DOOR STOP #7 IAW SRM 51-42-
- [SDR YENA2022072200687](https://openairdocs.org/sdr/YENA2022072200687.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: FASTENER HOLE OF THE DOOR STOP N7 FR16RH AT UPPER INBOARD HOLE; REF AEROMAN NR 2022-317801 W/O:2022 68/1: REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS AT FR16LHUPPER INBOARD HOLE LEVEL OF DOOR STOP #7 IAW SRM 51-42-1
- [SDR YENA2022072200686](https://openairdocs.org/sdr/YENA2022072200686.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: FASTENER HOLE OF THE DOOR STOP FR16RH AT LOWER INBOARD HOLE; REF AEROMAN NR 2022-317802 W/O:2022 68/1: REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS AT FR16RH LOWER INBOARD HOLE LEVEL OF DOOR STOP #7 IAW SRM 51-42-11,
- [SDR YENA2022072200685](https://openairdocs.org/sdr/YENA2022072200685.md): None · none · Jul 20, 2022 · N527JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: FASTENER HOLE OF THE DOOR STOP FR16RH AT LOWER INBOARD HOLE; REF AEROMAN NR 2022-317798 W/O:2022 68/1: REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS AT FR16LH UPPER INBOARD HOLE LEVEL OF DOOR STOP #7 IAW SRM 51-42-11,
- [SDR YENA2020090300445](https://openairdocs.org/sdr/YENA2020090300445.md): Battery · no test · Sep 3, 2020 · N527JL · Airbus A320232 · Emergency Lighting
  > FLIGHT 573, EMERGENCY LIGHT TEST FAILED. REMOVED & REPLACED EMERGENCY LIGHT BATTERY FIN 10WL IAW AMM 33-51-38.
- [SDR YENA2019042390211](https://openairdocs.org/sdr/YENA2019042390211.md): Bulb · inoperative · Apr 19, 2019 · N527JL · Airbus A320232 · Emergency Lighting
  > FT # 857, HPN-PBI. L1 DOOR EXIT SIGN BULBS BURNT OUT, ALSO RH /W EXIT SIGN, ALSO AFT CTR AISLE EXIT SIGN; RELAMPED L1 DOOR EXIT SIGN & REPLACED R/H O/W EXIT SIGN 42WL & AFT CTR AISLE 52WL PER AMM 33-51-16. TEST OF EMERGENCY LIGHTS OK.42W
- [SDR YENA201812070841](https://openairdocs.org/sdr/YENA201812070841.md): Lens · broken · Dec 7, 2018 · N527JL · Airbus A320232 · Emergency Lighting
  > FLT 894, STI-EWR. EMERG LIGHT COVER BROKEN 1C AISLE. REPLACED ROW 1C EMERGENCY LIGHT LENS. EMERG LIGHT SYS OPS CHECK OK REF AMM 33-51-00.
- [SDR YENA201806186254](https://openairdocs.org/sdr/YENA201806186254.md): Connector · loose · Jun 16, 2018 · N527JL · Airbus A320232 · Light System Wiring
  > LEFT WINDSCREEN EMERGENCY LIGHT INOPERATIVE. SECURED A LOOSE CONNECTOR IAW 33-50-00. OPS OK.
- [SDR YENA2018061860253](https://openairdocs.org/sdr/YENA2018061860253.md): Connector · loose · Jun 16, 2018 · N527JL · Airbus A320232 · Light System Wiring
  > ROW 1 ABC SEAT MOUNTED EMERGENCY LIGHT WAS INOPERATIVE. SECURED A LOOSE CONNECTOR IAW 33-50-00, OPS OK.
- [SDR YENA201711300973](https://openairdocs.org/sdr/YENA201711300973.md): Battery · discharged · Nov 30, 2017 · N527JL · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, 11WL BATTERY FAILS EMERGENCY LIGHT TEST FROM CIDS PANEL. REMOVED AND REPLACED 11WL BATTERY IAW AMM 33-51-38.
- [SDR YENA201711300972](https://openairdocs.org/sdr/YENA201711300972.md): Battery · failed · Nov 30, 2017 · N527JL · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, AFT EMERGENCY LIGHT TEST FROM CIDS PANEL. REMOVED AND REPLACED AFT LEFT EMERGENCY IAW AMM 33-51-38.
- [SDR YENA201711300971](https://openairdocs.org/sdr/YENA201711300971.md): Battery · failed · Nov 30, 2017 · N527JL · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, FWD RIGHT EMERGENCY LIGHT TEST FROM CIDS PANEL. R & R FWD RIGHT EMERGENCY IAW AMM 33-51-38.
- [SDR YENA201711300970](https://openairdocs.org/sdr/YENA201711300970.md): Battery Pack · failed · Nov 30, 2017 · N527JL · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, FWD LEFT EMERGENCY LIGHT BATTERY PACK FAILS CIDS TEST. R&R L1 DOOR SLIDE IAW AMM 25-62-44-400-803. EMERGENCY LIGHTS OPS CHECK GOOD.
- [SDR YENA201711300969](https://openairdocs.org/sdr/YENA201711300969.md): Angle · cracked · Nov 30, 2017 · N527JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, A CRACK WAS SUSPECTED RT AT FR41-42 TI ANGLE BETWEEN THE BELLY FAIRING AND KEEL BEAM SIDE PANEL. R&R TI ANGLE P/N D5337260120795 PER SRM 51-42-11.
- [SDR YENA201709260798](https://openairdocs.org/sdr/YENA201709260798.md): Battery Pack · failed · Sep 26, 2017 · N527JL · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS WON'T COME ON IN THE ARM POSITION. R & R THE EPSU & EMERGENCY BATTERY. OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR YENA201709260797](https://openairdocs.org/sdr/YENA201709260797.md): Power Supply · failed · Sep 26, 2017 · N527JL · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS WON'T COME ON IN THE ARM POSITION. R & R THE EPSU & EMERGENCY BATTERY. OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR YENA20160531525](https://openairdocs.org/sdr/YENA20160531525.md): Floor Support · corroded · May 31, 2016 · N527JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAMES 64-67 -Y512 RT. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA20160531539](https://openairdocs.org/sdr/YENA20160531539.md): Floor Support · corroded · May 31, 2016 · N527JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAMES 67-69, Y1162 RT. R & R FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA20160531538](https://openairdocs.org/sdr/YENA20160531538.md): Floor Support · corroded · May 31, 2016 · N527JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT FRAME 66-67, Y1292 RT. R & R FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA20160531537](https://openairdocs.org/sdr/YENA20160531537.md): Door Sill · corroded · May 31, 2016 · N527JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT PASSENGER/CREW DOOR SILL FRAME 68. PERFORMED REINFORCEMENT REPAIR IAW SRM 53-41-14-300-001.
- [SDR YENA20160531536](https://openairdocs.org/sdr/YENA20160531536.md): Door Frame · corroded · May 31, 2016 · N527JL · Airbus A320232 · Fuselage Main, Structure
  > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT LT PASSSENGER/CREW DOOR FRAME 68. PERFORMED REINFORCEMENT REPAIR IAW SRM 53-41-14-300-001.
- [SDR YENA20160531535](https://openairdocs.org/sdr/YENA20160531535.md): Door Frame · corroded · May 31, 2016 · N527JL · Airbus A320232 · Fuselage Main, Structure
  > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT PAS/CREW DOOR FRAME 66. PERFORMED REINFORCEMENT REPAIR IAW SRM 53-41-14-300-001.

Next page: https://openairdocs.org/aircraft/N527JL/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 = 'N527JL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N527JL/reports

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