# Service difficulty reports: N508JL

A list on [N508JL](https://openairdocs.org/aircraft/N508JL.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 · 143 reports

- [SDR YENA2026101200942](https://openairdocs.org/sdr/YENA2026101200942.md): Control Servo · malfunctioned · Oct 10, 2026 · N508JL · Airbus A320232 · Flight Control System
  > FLT#789, DTW-FLL. DURING CLIMB NOTICED A SMALL AMOUNT OF FWD STICK ABOUT 1/4" REQUIRED TO FOLLOW FLIGHT DIRECTORS(NOSE WANTED TO PITCH UP) CONTINUED FOR 30 MINS AFTER TOC & WENT AWAY UNTIL DESCENT, RETURNED & WAS PRESENT FOR DURATION OF FLT. ACFT COMPLETELY CO
- [SDR YENA2025090900919](https://openairdocs.org/sdr/YENA2025090900919.md): Warning Light · false activation · Sep 8, 2025 · N508JL · Airbus A320232 · Passenger/Crew Doors
  > FLT#1251, HPN-RSW. "MULTIPLE DOOR/SLIDE INDICATORS DURING TAXI OUT INDIACTING SLIDES DISARMED WHEN THEY WERE ARMED; C/W WITH RESET OF PAX DOORS SLIDE INDIACTION SYSTEM IAW TSM 52-11-00 C/W WITH ARMING AND DIARAMING PROCEDURES.NO FAULTS NOTED.A/C OK FOR SVC."
- [SDR YENA2025062700656](https://openairdocs.org/sdr/YENA2025062700656.md): Door Frame · cracked · Jun 26, 2025 · N508JL · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE 3 (LOWER/INBOARD POSITION) LOCATED AT FR68 LH, DOOR STOP FITTING 1. AT PASSENGER CABIN. CRACK DEPTH = 0.088 INCHES, CRACK DIRECTION: 12 OCLOCK; (RESOLVED ON W/O: 1380871 TASKCARD: NR-00010) FUR-
- [SDR YENA2025062700655](https://openairdocs.org/sdr/YENA2025062700655.md): Shear Tie · corroded · Jun 26, 2025 · N508JL · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATION FR28 BTW STR43L TO STR44 IN FWD CARGO COMPARTMENT; REF AEROMAN N/R 2025-385562, REMOVED AND REPLACED SHEAR TIE LOCATED FR28 BTW STR43L TO STR44 IN FWD CARGO COMPARTMENT I.A.W A320 SRM 51-42-11 AND SRM 51-
- [SDR YENA2025062700654](https://openairdocs.org/sdr/YENA2025062700654.md): Shear Tie · corroded · Jun 26, 2025 · N508JL · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED FR28 BTW STR41L TO STR42L IN FWD CARGO COMPARTMENT; REF AEROMAN N/R 2025-385561, REMOVED AND REPLACED SHEAR TIE LOCATED FR28 BTW STR41L TO STR42L IN FWD CARGO COMPARTMENT I.A.W A320 SRM 51-42-11. AND SRM 51
- [SDR YENA2025062700653](https://openairdocs.org/sdr/YENA2025062700653.md): Skin · damaged · Jun 26, 2025 · N508JL · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: SECONDARY FINDING ELONGATED HOLES ON REFORCING PLATE LOC. AFT LOWER SK IN BTW RIB7 AND RIB8 ON RH WING; REF AEROMAN N/R 2025-373108, REMOVED AND REPLACED MOUNTING PLATE (REFORCING PLATE) LOC. AFT LOWER SKIN BTW RIB7 AND RIB8 ON RH WIN
- [SDR YENA2025062700652](https://openairdocs.org/sdr/YENA2025062700652.md): Power Supply · inoperative · Jun 26, 2025 · N508JL · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: INOP EPSU 13WL AFT GALLEY AREA; REF AEROMAN NR 2025-285591 WO 2025 183/1 REMOVED AND REPLACED EPSU 13WL AFT GALLEY AREA. IAW AMM 33-51-38-000-002-A, AND AMM 33-51-38-400-002-A, AND PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-001-A
- [SDR YENA2024120601532](https://openairdocs.org/sdr/YENA2024120601532.md): A/C Pack · leaking · Dec 2, 2024 · N508JL · Airbus A320232 · Engine Cowling System
  > FLT#1601, JFK-FLL.'AFT OLD SOCK SMELL; INSPECTED APU IAW AMM 49-00-00-200-811-A. FOUND NO LEAK. AIRFRAME SHOWS EVIDENCE OF HYDRAULIC FLUID GOING IN TO PACK #2 PERFORMED LEVEL A DECON IAW AMM 21-00-00-615-802-A. AIR QUALITY GOOD. TROUBLESHOOTING PERFORMED PER I
- [SDR YENA2024022900303](https://openairdocs.org/sdr/YENA2024022900303.md): Gasket · leaking · Feb 27, 2024 · N508JL · Airbus A320232 · Navigation System
  > FLT#1680, FLL-DCA. 'DURING CRUISE FLIGHT AT FL310 THE FLIGHT ATT CALLED AND STATED THERE WAS AN EXTREMELY LOUD AIR SEAL TYPE NOISE AT ROW 3 A/C LEFT. CONFIRMED BY DH CA TO BE VERY UNUSUAL WEAR WINDOW 3A; REPLACED AOA SENSOR 3FP1 SEAL ON LH FUSALAGE AND REPLACE
- [SDR YENA2023021400173](https://openairdocs.org/sdr/YENA2023021400173.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Emergency Equipment
  > DURING HEAVY MAINTENANCE: OVERPRESSURE OFFWING SLIDE RESERVOIR RH; REF: ARM W/O 2022-453/1 NR 2022-676108 REMOVED AND REPLACED OFFWING RESERVOIR RH (7507MM) IAW AMM 25-62-46-000-001-A STEP 1 THRU 4.A AND AMM 25-62-46-400-001-A. FUNCTIONAL AND OPS TEST OK. TECH
- [SDR YENA2023021400172](https://openairdocs.org/sdr/YENA2023021400172.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON CENTER FRONT WINDSHIELD FRAME, CENTER POST, AROUND UPPER BOLT LH SIDE IN COCKPIT. REF: ARM W/O 2022 453/1 N/R 2022-676202; REF: ARM W/O 2022-453/1 NR 2022-676202 ACCOMPLISHED PERMANENT REPAIR ON LH WINDSHIELD FRAME
- [SDR YENA2023021400171](https://openairdocs.org/sdr/YENA2023021400171.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR36 VERTICAL STRG FLOOR BEAM 4 ZONE 1. THE CRACK DIRECTION IS 12 O'CLOCK. REF: ARM W/O 2022-453/1 N/R 2022-676216; REF: ARM W/O 2022-453/1 NR 2022-676216 PERFORMED REPAIR LOCATED ON Y-254 (BEAM 4) ZONE 1, VERTICAL
- [SDR YENA2023021400170](https://openairdocs.org/sdr/YENA2023021400170.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Aerodynamic Fairings
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR55 AND FR56 IN AFT CARGO COMPARTMENT (CPC P RELATED REFER TO MPD TASK 534107-01); (RESOLVED ON W/O: 1176129 TASKCARD: NR-00027) ALL WORK ACCOMPLISHED REF AEROMAN NRC 2022-676486. REMOVED AND REPLACED ST
- [SDR YENA2023021400169](https://openairdocs.org/sdr/YENA2023021400169.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Aerodynamic Fairings
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR57 AND FR58 IN AFT CARGO COMPARTMENT (CPC P RELATED REFER TO MPD TASK 534107-01); (RESOLVED ON W/O: 1176129 TASKCARD: NR-00028) ALL WORK ACCOMPLISHED ON AEROMAN NR 2022-676482, REMOVED AND REPLACED STRIN
- [SDR YENA2023021400168](https://openairdocs.org/sdr/YENA2023021400168.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE HORIZONTAL FLANGE RADIUS AT STGR 22 AFT WEB FACE, CRACK LENGTH IS 1.500 INCH APPROX, AT AFT GALLEY AREA (1EA); ACCOMPLISHED PERMANENT REPAIR IAW AEROMAN WO 2022-453/1, NR 2022-676465 AND JETBLUE EC
- [SDR YENA2023021400167](https://openairdocs.org/sdr/YENA2023021400167.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON VERTICAL STRG FLOOR BEAM 3 ZONE 2. THE CRACK DIRECTION IS 12 O'CLOCK. REF AEROMAN NRC 2022-676209; REF: ARM W/O 2022 453/1 N/R 2022-676209 REPAIRED IAW EC NO. A23-034-01 AND EA 53-0635-22, REV 0 (COVER, PART 1 AND
- [SDR YENA2023021400166](https://openairdocs.org/sdr/YENA2023021400166.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON VERTICAL STRG FLOOR BEAM 4 ZONE 2. CRACK DIRECTIONS ARE 12 O'CLOCK AND 8 O'CLOCK. REF AEROMAN NRC# 2022-676210; REF: ARM W/O 2022 453/1 N/R 2022-676210. REPAIRED PER EC NO. A23-034-01 AND EA 53-0635-22. ITEM IS CAT
- [SDR YENA2023021400165](https://openairdocs.org/sdr/YENA2023021400165.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR36 VERTICAL STRG FLOOR BEAM 5 ZONE 2. THE CRACK DIRECTION IS 11 O'CLOCK. REF AEROMAN NRC 2022-676220; REF: W/O 2022 453/1 N/R 2022-676220 REPAIRED PER EC A23-034-01 AND EA 53-0635-22 REV 0 (COVER PART 1 AND PART
- [SDR YENA2023021400164](https://openairdocs.org/sdr/YENA2023021400164.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR57 AND FR58 IN AFT CARGO COMPARTMENT (CPCP RELATED REFER TO MPD TASK 534107-01); ALL WORK ACCOMPLISHED ON AEROMAN NR 2022-676482, REMOVED AND REPLACED STRINGER 43L BTW FR57 AND FR58 IN AFT CARGO COMPARTMEN
- [SDR YENA2023021400163](https://openairdocs.org/sdr/YENA2023021400163.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR55 AND FR56 IN AFT CARGO COMPARTMENT (CPC P RELATED REFER TO MPD TASK 534107-01); ALL WORK ACCOMPLISHED REF AEROMAN NRC 2022-676486. REMOVED AND REPLACED STRINGER 43L BTW FR54 AND FR60 IN AFT CARGO COMPART
- [SDR YENA2023021400162](https://openairdocs.org/sdr/YENA2023021400162.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC FR 66 TO FR 68 AT LEVEL STR 23L AFT GALLEY AR EA (CPCP RELATED REFER TO THE MPD TASK 534195-01); ALL WORK ACCOMPLISHED ON AEROMAN NR #2022-676475, PERFORMED REPAIR AT LOWER SILL LOC FR 66 TO FR 68 AT LEVEL STR
- [SDR YENA2023021400161](https://openairdocs.org/sdr/YENA2023021400161.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Wing Spar
  > DURING HEAVY MAINTENANCE: WINGS / CENTER WING / FRONT SPAR / FR 36 / VERTICAL STIFFENER / CRACK DAMAGES - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023021400160](https://openairdocs.org/sdr/YENA2023021400160.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / MLG ACTUATOR FITTING – STRUCTURAL REINFORCEMENT. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023021400159](https://openairdocs.org/sdr/YENA2023021400159.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage, Wing Attach Fittings
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR68 & STGR 22R HORIZONTAL FLANGE RADIUS & DOOR STOP FITTING #1 HOLE 3 / CRACK - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023021400158](https://openairdocs.org/sdr/YENA2023021400158.md): None · none · Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ FWD WINDSHIELDS / CENTER POST / CRACK DAMAGE - PERMANENT REPAIR (MIRROR FITTING SOLUTION). (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2022112101140](https://openairdocs.org/sdr/YENA2022112101140.md): A/C Pack · fod · Nov 20, 2022 · N508JL · Airbus A320232 · Air Distribution System
  > FLT#41, DURING APPROACH, LANDING, AND TAXI BACK, STRONG FUMES OBSERVED BY CREWMEMBERS AND PAX IN AFT PART OF CABIN. NO ECAM OR SYSTEM ABNORMALITIES WERE NOTED. NOTE PACK 2 REMAINED IN HIGH THE ENTIRE FLIGHT UNTIL IT RELEASED TO LOW UPON LANDING. PERFORMED LEV
- [SDR YENA2022110201084](https://openairdocs.org/sdr/YENA2022110201084.md): None · none · Oct 31, 2022 · N508JL · Airbus A320232 · Fuselage Structure (General)
  > FLT#1558, BOG-FLL.' INFLIGHT COMPLAINED ABOUT DIRTY SOCKS SMELL AT 18K TILL LANDING. THE FLIGHT CREW DIDN'T EXPERIENCE IT; INSPECTED A/C AND FOUND THE LEVEL TO BE LEVEL A. PERFORM TSM 05-50-00-810-831-A AND IDENTIFIED THE SOURCE OF ODOR TO BE APU. PERFORMED E
- [SDR YENA2022042800419](https://openairdocs.org/sdr/YENA2022042800419.md): Lgciu · failed · Apr 19, 2022 · N508JL · Airbus A320232 · Cargo Compartment Lighting
  > FLT# 252, RSW-HPN. (AIRCRAFT DIVERTED TO JFK). 'LG - LGCIU 1 FAULT; REMOVED AND REPLACED LGCIU #1 IAW AMM 32-31-71. OPS AND BITE CHECK GOOD. A/C OK FOR SERVICE.'
- [SDR YENA2021011400060](https://openairdocs.org/sdr/YENA2021011400060.md): Filter · odor · Jan 10, 2021 · N508JL · Airbus A320232 · Air Distribution System
  > FLT 8168, PUJ-JFK. ODOR EVENT NOTICED FROM TOP OF DESCENT. MORE PROMINENT THROUGH 28K FEET. IT SEEMED TO HELP DESCENDING W A/I ON AND USING V/S IE KEEPING POWER LEVELS UP IN DESCENT. MOST PROMINENT MID CABIN. PERFORMED INFO NOTICE 2017-T015F- SECTION B- L
- [SDR YENA2021011400059](https://openairdocs.org/sdr/YENA2021011400059.md): Unknown · odor · Jan 8, 2021 · N508JL · Airbus A320232 · Air Distribution System
  > FLT 1869, JFK-PUJ. LEVEL 3 ODOR EVENT STARTED AT TOP OF DESCENT IN THE MAIN CABIN NOTED BY INFLIGHT. PERFORMED ENGINES RUN WITH THE FLT CREW AND ISOLATED BLEED 1 AND BLEED 2 WITH NO EVIDENCE ODOR AT THE CABIN AT THIS TIME. ALSO ISOLATED PACK 1 AND PACK 2 WI
- [SDR YENA2020031610231](https://openairdocs.org/sdr/YENA2020031610231.md): Slide Raft · deformed · Mar 11, 2020 · N508JL · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, DEFORMATION SLIDE RAFT AT DOOR 841; REMOVED AND REPLACED ESCAPE SLIDE AT DOOR 841 IAW AMM 25-62-44-400-803. REF AEROMAN NR 2020-79089
- [SDR YENA2020031610230](https://openairdocs.org/sdr/YENA2020031610230.md): Epsu · failed · Mar 11, 2020 · N508JL · Airbus A320232 · Emergency Lighting
  > "DURING HEAVY MAINTENANCE, INOP EPSU -EMERGENCY POWER SUPPLY UNIT IN PASSENGER CABIN 13WL; REF AEROMAN WO 2020-82/1 WCC 2020-79279- REMOVED AND REPLACED EPSU IN POSITION 13WL IAW AMM 33-51-38-400-001. AND PERFORMED CHECK OF THE EMERGENCY POWER SUPPLY UNIT BY B
- [SDR YENA2020031610229](https://openairdocs.org/sdr/YENA2020031610229.md): Door Frame · cracked · Mar 11, 2020 · N508JL · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 68 AFT DOOR RH SIDE BTW STR8 AND STR9; REF AEROMAN NR W/O#2020-97/1 WCC# 2020-79124 REAPIR PART TRANSVERSAL FLANGE MUST BE INSPECTED AT 40,800 FC FH NOT RELEVANT FROM ADL/REPAIER EMBODIMENT SUBSEQUENT INSPECT
- [SDR YENA2020031610228](https://openairdocs.org/sdr/YENA2020031610228.md): Door Frame · cracked · Mar 11, 2020 · N508JL · Airbus A320232 · Fuselage Main, Structure
  > "DURING HEAVY MAINTENANCE, CRACK INDICATION ON FR 68 AFT DOOR, RH SIDE, AFT UPPER CORNER, BTW STRG8 AND STGR9 WEB JOINT TO DOOR FRAME. LENGTH 0.700 IN; REF AEROMAN NR W/O#2020-82/1 WCC# 2020-79124 PERFORMED REPAIR ON FR 68 AFT DOOR RH SIDE BTW STR 8 AND STR 9
- [SDR YENA2019080210428](https://openairdocs.org/sdr/YENA2019080210428.md): Lamp · inoperative · Jul 31, 2019 · N508JL · Airbus A320232 · Emergency Lighting
  > FT 2931, FLIGHT ATTENDANT REPORTED THE EMERGENCY EXIT ROW DOOR LIGHTS OUT. RELAMPED THE EMERGANCY EXIT DOOR LIGHT IAW AMM 33-51-07. OPS CHECKED OK.
- [SDR YENA2019062418336](https://openairdocs.org/sdr/YENA2019062418336.md): Unknown · odor · Jun 18, 2019 · N508JL · Airbus A320232 · Air Distribution System
  > STRONG DIRTY SOCK ODOR TRANSIENT APPROX 10000 FROM ROW 20 AND AFT FROM AIR SUPPLY VENTS; FOUND CONDITION TO BE A LEVEL 1 COMPLIED WITH INFO NOTICE 2017-T015E SECTION A. AIRCRAFT IS OK FOR SERVICE.
- [SDR YENA2018122640881](https://openairdocs.org/sdr/YENA2018122640881.md): Battery Pack · no test · Dec 24, 2018 · N508JL · Airbus A320232 · Emergency Lighting
  > FT # 225, JFK-TPA. EMERGENCY LIGHT BATTERY 10WL FAILED TEST; REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 10WL IAW AMM 33-51-38
- [SDR YENA201806250927](https://openairdocs.org/sdr/YENA201806250927.md): Pressure Panel · cracked · Jun 25, 2018 · N508JL · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE, SEVERAL CRACKS WERE FOUND. REFER TO EC A18-504-01. FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36 / LT & RT SIDES / PRESSURE PANEL ATTACHMENT HOLES / CRACK DAMAGE - PERMANENT REPAIR; THIS TIME LIMITED REPAIR HAS BEEN APPROVED
- [SDR YENA201806250926](https://openairdocs.org/sdr/YENA201806250926.md): Window Post · cracked · Jun 25, 2018 · N508JL · Airbus A320232 · Fuselage Main, Structure
  > DURING CURRENT (6/2018) C10 HEAVY CHECK AT SAL, UNDERGOING REF /3/ INSPECTION WHEN A CRACK WAS FOUND ON WINDSHIELD LT SIDE POST UPPER SECTION AT FR4 (SEE REF /1/ EA FOT DETAILS). WITHOUT ANY SRM REPAIR OPTIONS, CONTACTED AND PROVIDED REF /4/ REPAIR DRAWING. TH
- [SDR YENA201805290220](https://openairdocs.org/sdr/YENA201805290220.md): Battery Pack · failed · May 29, 2018 · N508JL · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED THE BATTERY ASSY AT 13WL IAW 33-51-11.
- [SDR YENA201803050123](https://openairdocs.org/sdr/YENA201803050123.md): Epsu · failed · Mar 5, 2018 · N508JL · Airbus A320232 · Emergency Lighting
  > RIGHT EMERGENCY EXIT DOOR LIGHT ILLUMINATED, AS WELL AS ISLE EXIT LIGHT, IN CRUISE WITH LDG GR UP; R & R EMERGENCY PSU 11WL AND 12WL IAW AMM 33-51-38, OPS CHECK OK. R & R BATTERIES ON EPSU 11WL AND 12WL IAW CMM 33-51-07 OPS CHECK OK.
- [SDR YENA201803050122](https://openairdocs.org/sdr/YENA201803050122.md): Battery Pack · failed · Mar 5, 2018 · N508JL · Airbus A320232 · Emergency Lighting
  > RIGHT EMERGENCY EXIT DOOR LIGHT ILLUMINATED, AS WELL AS ISLE EXIT LIGHT, DURING CRUISE WITH LANDING GEAR UP. R & R EMERGENCY PSU 11WL AND 12WL IAW AMM 33-51-38, OPS CHECK OK. R & R THE BATTERIES ON EPSU 11WL AND 12WL IAW CMM 33-51-07 OPS CHECK OK.
- [SDR YENA201803050121](https://openairdocs.org/sdr/YENA201803050121.md): Battery Pack · failed · Mar 5, 2018 · N508JL · Airbus A320232 · Emergency Lighting
  > RIGHT EMERGENCY EXIT DOOR LIGHT ILLUMINATED, AS WELL AS ISLE EXIT LIGHT, DURING CRUISE, WITH LANDING GEAR UP. R & R EMERGENCY PSU 11WL AND 12WL IAW AMM 33-51-38, OPS CHECKED OK. R & R THE BATTERIES IN THE EPSU 11WL AND 12WL IAW CMM 33-51-07. OPS CHECKED
- [SDR YENA201803050120](https://openairdocs.org/sdr/YENA201803050120.md): Power Supply · failed · Mar 5, 2018 · N508JL · Airbus A320232 · Emergency Lighting
  > RIGHT EMERGENCY EXIT DOOR LIGHT ILLUMINATED, AS WELL AS ISLE EXIT LIGHT, DURING CRUISE WITH LANDING GEAR UP. R & R THE PSU 11WL AND 12WL IAW AMM 33-51-38, OPS CHECKED OK. R & R BATTERIES ON EPSU 11WL AND 12WL IAW CMM 33-51-07. OPS CHECKED OK.
- [SDR YENA201711120966](https://openairdocs.org/sdr/YENA201711120966.md): Proximity Switch · malfunctioned · Nov 12, 2017 · N508JL · Airbus A320232 · Accessory Compartment
  > FT # 772, CUN-BOS. DOOR L/H AFTER EMERGENCY EXIT ECAM DURING TAXI ( ECAM DOOR PG OVERWING EXITS OPEN IND--SLIDE IND ON ECAM OK); REMOVED OVERWING DOOR AND PINNED BOTTLE. REPLACED LH AFT EMERGENCY DOOR PROX SWITCH PER AMM 52-71-11. OPS CHECK GOOD. MDDR CLEARED
- [SDR YENA201708090654](https://openairdocs.org/sdr/YENA201708090654.md): Slide · unwanted deploy · Aug 9, 2017 · N508JL · Airbus A320232 · Escape Slide
  > RECEIVED AN ECAM MESSAGE FOR DOOR LEFT AFT EMERGENCY EXIT. RAN NON-NORMAL THROUGH QRH SPOKE WITH INFLIGHT TO CHECK DOOR AREA ECT. REPORTED SLIDE ARM (GREEN LIGHT) WAS ON AND WARM. OUR INDICATIONS IN COCKPIT WENT NORMAL AND INFLIGHT REPORTED ALL NORMAL AS WELL.
- [SDR YENA201612071084](https://openairdocs.org/sdr/YENA201612071084.md): Battery · no test · Dec 7, 2016 · N508JL · Airbus A320232 · Emergency Lighting
  > DURING MAINTENANCE, AN OPS CHECK WAS PERFORMED. FWD ESPU BATTERY FAILED DURING BATTERY TEST. EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. R & R L2 DOOR ESPU BATTERY IAW AMM IAW 33-51-38. R & R L2 ESPU (10WL) IAW AMM 33-51-38. PERFORMED OPS CHECK. OPS CHECK
- [SDR YENA201612071083](https://openairdocs.org/sdr/YENA201612071083.md): Epsu · failed · Dec 7, 2016 · N508JL · Airbus A320232 · Emergency Lighting
  > DURING MAINTENANCE, AN OPS CHECK WAS PERFORMED. FWD ESPU BATTERY FAILED DURING BATTERY TEST. EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. R & R THE BATTERY PACK IAW AMM IAW 33-51-38. R & R L2 ESPU (10WL) IAW AMM 33-51-38. OPS CHECK PASSED.
- [SDR YENA201612011069](https://openairdocs.org/sdr/YENA201612011069.md): Floor Support · corroded · Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT +Y765 FRAME 66. R & R THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472815.
- [SDR YENA201612011068](https://openairdocs.org/sdr/YENA201612011068.md): Floor Support · corroded · Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT -Y254 FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW 51-72-11 AND DRAWING D53111462.

Next page: https://openairdocs.org/aircraft/N508JL/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 = 'N508JL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N508JL/reports

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