# Service difficulty reports: N531JL

A list on [N531JL](https://openairdocs.org/aircraft/N531JL.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 · 88 reports

- [SDR YENA2026040900385](https://openairdocs.org/sdr/YENA2026040900385.md): Skin · damaged · Apr 8, 2026 · N531JL · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, RT WING BOTTOM SKIN PANEL NR 2 ACCESS PANEL 640JB FASTENER HOLE OUT OF ROUND E EA, AT RIB BAY 14-15. REFERENCE CAS WO 531-1485203 SASK 33 AND 34 AND WO 1485203- NR 13 AND 14. TWO EACH BUSING REPAIRS PERFORMED AT RIB BAY 14-15 AT PAN
- [SDR YENA2026040900384](https://openairdocs.org/sdr/YENA2026040900384.md): Skin · damaged · Apr 8, 2026 · N531JL · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, REF: SRM 53-41-11-300-004, DOSSIER 81769917, MX244. FOUND WITH CORROSION DAMAGE ON THE AFT LAV VENT AT FR 69-FR70 BETWEEN STGR31R AND STGR32R AFFECTING SKIN PANEL. REPAIRED, TRIMMING OUT THE DAMAGED AREA AND PERFORMING A HFEC INS
- [SDR YENA2026030900283](https://openairdocs.org/sdr/YENA2026030900283.md): Ped · odor · Mar 7, 2026 · N531JL · Airbus A320232 · Standard Practices/Structures
  > FLT# 1437 BDL- MCO. " BURNING SMELL NOTED BETWEEN ROWS 11-15 AIRCRAFT RIGHT. TURNING OFF THE PED POWER ELIMINATED THE SMELL.; COMPLIED WITH INFORMATION NOTICE 2017-T015 STEPS 1 AND 2. IDENTIFIED ODOR TYPE 9-ELECTRICAL. REF LOGPAGE 4458537-2 FOR CORRECTIVE ACTI
- [SDR YENA2026022300230](https://openairdocs.org/sdr/YENA2026022300230.md): Lamp · burned · Feb 22, 2026 · N531JL · Airbus A320232 · Lighting System
  > FLT # 1371 LGA-FLL. "SMOKY SMELL IN AFT GALLY ON ARR F3 REPORTED AFTER LIGHTS TURNS OFF SMELL WENT AWAY.; INSPECTED AND FOUND NO SMOKEY SMELL FROM AFT GALLEY LIGHTS OPERATING FOUND AFT DOOR L2 ENTRY DOOR LAMP BURNT. REMOVED AND REPLACED BOTH BALLAST UNIT & LA
- [SDR YENA2025070100667](https://openairdocs.org/sdr/YENA2025070100667.md): Frame · ground damage · Jun 28, 2025 · N531JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FR 5-7 & LH LOWER STRINGER-CENTERLINE / TUG IMPACT. REPAIRED.
- [SDR YENA2025042400426](https://openairdocs.org/sdr/YENA2025042400426.md): Shear Tie · corroded · Apr 23, 2025 · N531JL · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. AT LEVEL FR. 65 AND STRG 43R TO STRG 44 FLOOR STRUCTURE AREA IN AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1389929 TASKCARD: NR-00021) REF AEROMAN WO 2025-134/1, NR 2025 - 237264, REMOVED AND REPLACED CLIP (SHEA
- [SDR YENA2025042400425](https://openairdocs.org/sdr/YENA2025042400425.md): Frame · cracked · Apr 23, 2025 · N531JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE HORIZONTAL FLANGE RADIUS AT STGR 8, WEB AFT FACE. CRACK LENGTH IS 0.210 INCH APPROX AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389929 TASKCARD: NR-00028) REF AE WO 2025-134/1. N/R# 2025 - 237225
- [SDR YENA2025042400424](https://openairdocs.org/sdr/YENA2025042400424.md): Frame · cracked · Apr 23, 2025 · N531JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 STGR 8RH / HORIZONTAL FLANGE / HOLE 1 AND 7 / CRACKS – PERMANENT REPAIR; /1/ EA 53-0020-25 REV 0 (COVER AND PART (1-3)) /2/ RDAF 81571877/003/2025 ISSUE A /3/ DOSSIER 81571877 /4/ SRM 53-41-12-300-012.
- [SDR YENA2025030700242](https://openairdocs.org/sdr/YENA2025030700242.md): Unknown · odor · Mar 6, 2025 · N531JL · Airbus A320232 · Air Distribution System
  > FLT#1199, LGA-MCO. 'DURING FINAL DESCENT THROUGH CLOUDS FLIGHT DECKAD MODERATE DIRTY SOCK ODOR FUME CONTINUED DURING DESCENT TURNED PACK 1 OFF POSSIBLE IMPROVEMENT; REVIEW OF AML AND TRAX SHOWS NO 30 DAY HISTORY. COMPLIED WITH INFO NOTICE 2017-T015 SEC A ISOLA
- [SDR YENA2024050200696](https://openairdocs.org/sdr/YENA2024050200696.md): Wire Harness · damaged · Apr 30, 2024 · N531JL · Airbus A320232 · Landing Gear System Wiring
  > FLT#1036, SJU-STT. (AIRCRAFT PERFORMED AN AIR TURN BACK) 'AUTO BRAKE FAULT ( TACHOMETER); FOUND 1M AXLE HARNESS FAULTY WHEN FLEXING CABLE. ALSO PIN GRIPS VERY WORN AND WEAK. REPLACED 1M AXLE HARNESS ON RIGHT MLG AND TESTED IAW AMM 32-11-43. OPS CHECK NORMAL.
- [SDR YENA2023090601046](https://openairdocs.org/sdr/YENA2023090601046.md): Unknown · unknown · Sep 5, 2023 · N531JL · Airbus A320232 · Air Conditioning System
  > FLT#1142, PBI-BDL. (AIRCRAFT DIVERTED TO MCO) 'AFTER AIRBORNE BLOWER FAULT AND VENT SKIN VALVE FAULT; FOLLOWING MX PERFORMED. REMOVED AND REPLACED AVEC, SKIN AIR OUTLET, AND INLET VALVES. ALL CHECKS NORMAL. PER AMM 21-26-00. AIRCRAFT OK FOR SVC.'
- [SDR YENA2022102101032](https://openairdocs.org/sdr/YENA2022102101032.md): None · none · Oct 19, 2022 · N531JL · Airbus A320232 · Fuselage Structure (General)
  > FLT#1567, HPN-PBI. ALL FA'S SAID THEY SMELLED AN AMONIA-TYPE SMELL DURING DECENT. DURING DEBRIEFING. 2 AFT FA'S SAID SMELLED THE SAME SMELL INITIAL CLIMB SERVICE BUT DID NOT NOTIFY THE FLIGHT CREW AT THE TIME. SYMPTOMS WERE WATERY EYES & BLURRY VISION; ACCOMP
- [SDR YENA2022081600803](https://openairdocs.org/sdr/YENA2022081600803.md): Frame · cracked · Aug 11, 2022 · N531JL · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APROXIN COCKPIT(1EA); REMOVED AND REPLACED CONTINUITY FITTING LH SIDE ON FRAME 2 WINDSHIELD CENTER POST LOWER NO
- [SDR YENA2022081600802](https://openairdocs.org/sdr/YENA2022081600802.md): Frame · cracked · Aug 11, 2022 · N531JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT(1EA); REMOVED AND REPLACED CONTINUITY FITTING RH SIDE ON FRAME 2 WINDSHIELD CENTER POST LOWER
- [SDR YENA2022081600801](https://openairdocs.org/sdr/YENA2022081600801.md): Frame · cracked · Aug 11, 2022 · N531JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK (2EA): FR16LH DOOR STOP 7 INBD. UPPER HOLE (1 O'CLOCK - 0.148") AND INBD. LOWER HOLE (1 O'CLOCK - 0.075"); REF AEROMAN NR 2022-376934 AND 2022-376938 W/O: 2022 174/1: REMOVED AND REPLACED INTERCOSTAL AT FR16 LH SIDE DOOR STOP 7
- [SDR YENA2022081600800](https://openairdocs.org/sdr/YENA2022081600800.md): Intercostal · cracked · Aug 11, 2022 · N531JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK (2EA): FR 16 RH DOOR STOP 7 INBD. UPPER HOLE (9 O'CLOCK - 0.112") AND INBD. LOWER HOLE (9 O'CLOCK - 0.070"); REF AEROMAN NR 2022-376943 AND 2022-376944 W/O: 2022 174/1: REMOVED AND REPLACED INTERCOSTAL AT FR16 RH SIDE DOOR STOP
- [SDR YENA2022081600799](https://openairdocs.org/sdr/YENA2022081600799.md): Frame · cracked · Aug 11, 2022 · N531JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / FR 16 RH / DOUBLE JOGGLE AREA / HOLES 4 & 6 / CRACK DAMAGE – TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2022081600798](https://openairdocs.org/sdr/YENA2022081600798.md): Frame · cracked · Aug 11, 2022 · N531JL · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / FR 16 LH / DOUBLE JOGGLE AREA. HOLES 6, 8, B & C / CRACK DAMAGE. TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2022061300595](https://openairdocs.org/sdr/YENA2022061300595.md): Tachometer · failed · Jun 12, 2022 · N531JL · Airbus A320232 · Brake Anti-Skid Section
  > FLT#272, FLL-LGA. (AIRCRAFT DIVERTED TO JFK) 'BRAKES AUTO BRAKE BRAKES RELEASED FAULT ON THE AROUND WITH 1 ENG STARTED IN FLL RESET WITH MCC SAME FAULT ON DEPARTURE AFTER SAT CALL WITH MCC DIVERT TO JFK NORMAL LANDING WITH LOW BRAKES SELECTED; PERFORMED TSM 32
- [SDR YENA2022032100294](https://openairdocs.org/sdr/YENA2022032100294.md): None · none · Mar 18, 2022 · N531JL · Airbus A320232 · Hydraulic Power System
  > FLT#768, PSE-MCO. (AIRCRAFT DECLARED AN EMERGENCY). 'HYDRAULIC GREEN RESERVOIR LOW LEVEL IN FLIGHT; REF LOG PAGES #3338353 (REMOVED AND REPLACED #1 ENG HYD PRESSURE LINE IAW AMM 29-11-49. LEAK CHECK GOOD. OK FOR SERVICE), ITEM 2 FOR #1 ENG GREEN HYD LINE REPLA
- [SDR YENA2022012600025](https://openairdocs.org/sdr/YENA2022012600025.md): Limiter · tripped · Jan 22, 2022 · N531JL · Airbus A320232 · Trailing Edge Flap Control System
  > FLT # 2512, BOG-JFK. FROM FLAP 3 TO FULL, F/CTL FLAP FAULT. RECYCLED ACCORDING TO QRH, RESET SUCCESSFUL.; T/S PER 27-51-00-810-810-0A. ISNP FLAP MOVABLE SURFACES, FOUND L/H I/B FLAP TORQUE LIMITER TRIPPED, RESET TORQUE LIMITER. FOUND L/H BELLY FAIRING SLIDE PA
- [SDR YENA2021122800872](https://openairdocs.org/sdr/YENA2021122800872.md): Flow Valve · failed · Dec 23, 2021 · N531JL · Airbus A320232 · Cabin Pressure Control System
  > FLT 276, SJU-BDL(AIR TURN BACK TO SJU). CAB PR EXCESS CAB ALT WARNING DISPLAYED CLIMBING THROUGH FL310 PACK 1 APPARENTLY WEAK.; C/W R/R VALVE-FLOW CONTROL ASSY. PACK #1 AND SECURED AS PER A.M.M. 21-51-51-PB 401 PERFORMED BITE TEST A/C SYSTEM PASSED NO FAULT ON
- [SDR YENA2021100100634](https://openairdocs.org/sdr/YENA2021100100634.md): A/C Pack · leaking · Sep 27, 2021 · N531JL · Airbus A320232 · Cabin Cooling System
  > FLT 1045, EWR-SAN. INFLIGHT REPORTED DIRTY SOCK SMELL DESCENDING THRU 10,000FT NO SMELL APPARENT IN COCKPIT; DURING ODOR INSPECTION FOUND #1 PACK PUTTING OUT OIL SMELL ( PACKS). ACCOMPLISHED ECS DECONTAMINATION IAW AMM: 21-00-00. PACK #1 AIR QUALITY OK. MEL C
- [SDR YENA2021092200613](https://openairdocs.org/sdr/YENA2021092200613.md): Unknown · odor · Sep 17, 2021 · N531JL · Airbus A320232 · Air Distribution System
  > FLT 2135, JFK-PHX. ON DESCENT INTO PHX FA'S REPORTED A STRONG GLUE ODOR THAT SPREAD ACROSS THE CABIN; COMPLIED WITH INFO NOTICE 2017-T015 SEC ""A"" ISOLATED FAULT TO TRANSIENT ENVIRONMENTAL ODOR PER TSM 05-50-00-810-085-B. NO ODOR WITHIN 25 FLT CYCLES. A/C OK
- [SDR YENA2021082700543](https://openairdocs.org/sdr/YENA2021082700543.md): O-Ring · leaking · Aug 24, 2021 · N531JL · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT # 104, LAS-RIC. DURING DESCENT ENTIRE AIRCRAFT REEKED OF THE DIRTY SOCK ODOR. CABIN ODOR REPORT FILLED OUT. ( APU BLEED AIR SUPPLY SYSTEM); T/S STSTEM PER 05-50-00-810-831, FOUND THE SOURCE OF THE OIL LEAK AS A LOOSE HIGH OIL TEMP SENSOR. R/R THE HIGH OI
- [SDR YENA2021080600500](https://openairdocs.org/sdr/YENA2021080600500.md): Unknown · odor · Jul 28, 2021 · N531JL · Airbus A320232 · Air Distribution System
  > FLT 827, FUMES DURING LOW POWER IN THE DESCENT. AGAIN AFTER LANDING ON THE APU BLEED. T/S PER TSM 05-50-00-810-831-A) NO FLUIDS LEAKS NOTED. INSPECTED APU PER AMM 49-00-00-200-812-A. NO OIL LEAKS NOTED. OPERATED BOTH PACKS ON GROUND NO ODOR PRESENT. COMPLIE
- [SDR YENA2021051100309](https://openairdocs.org/sdr/YENA2021051100309.md): Slide · misoverhauled · May 4, 2021 · N531JL · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, IMPROPERLY PACKED ESCAPE SLIDE PASSENGER CREW DOOR 841 AT FWD GALLEY AREA (1EA); (REF AEROMAN NR 2021-192921) R & R SLIDE RAFT AT PASSENGER CREW DOOR 841 IAW AMM 25--62-44-000-804-A
- [SDR YENA2021042000252](https://openairdocs.org/sdr/YENA2021042000252.md): Light · malfunctioned · Apr 12, 2021 · N531JL · Airbus A320232 · Emergency Lighting
  > FLT 227, SJU-MCO. EMERGENCY EXIT LIGHTS STAY ON IN FLIGHT IN ARM. TRIED RESETING BUT DID NOT HELP; T/S SYST PER TSM 33-51-00-810-881 R & R (8WL) RELAY NO HELP. R & R (4WL) TOGGLE SWITCH OPS CKD NORMAL OK FOR SERVICE PER ESPM 20-45-21
- [SDR YENA201911110648](https://openairdocs.org/sdr/YENA201911110648.md): Warning Message · illuminated · Nov 11, 2019 · N531JL · Airbus A320232 · Cabin Pressure Control System
  > FT # 38, SJO-FLL. ECAM CAB PRESSURE SAFETY VALVE OPEN, CAME ON IN APP AT 5000 FEET LEVEL FLIGHT DIFF P 0.4; R & R BOTH CAB. PRESSURE SAFETY VALVES REF. AMM 21-31-52. OPS CHECK GOOD PER 21-31-00. NO DEFECTS NOTED AT THIS TIME. SUPPLEMENTAL INFORMATION TO FOLLOW
- [SDR YENA201808138309](https://openairdocs.org/sdr/YENA201808138309.md): Battery Pack · failed · Aug 8, 2018 · N531JL · Airbus A320232 · Emergency Lighting
  > DURING AN EMERGENCY LIGHTS TEST. EPSU BATTERY FWD FAILED. REPLACED THE EPSU 10WL BATTERY. EMERGENCY LIGHTS SYS TESTED GOOD.
- [SDR YENA201801070011](https://openairdocs.org/sdr/YENA201801070011.md): Unknown · odor · Jan 7, 2018 · N531JL · Airbus A320232 · Air Distribution System
  > ODOR AT ROW 6 & 7 DURING CRUISE. DURING DESCENT THROUGH 10000FT A DIRTY SOCK ODOR. COMPLIED WITH INFO NOTICE 2017-T015B SECTION B. AIRCRAFT IS OK FOR SERVICE. INSPECTED THE ENGINES AND APU FOR OIL LEAKS, FOUND NO DEFECTS. INSPECTED AVIONICS COMPARTMENTS, N
- [SDR YENA201801030001](https://openairdocs.org/sdr/YENA201801030001.md): Oil System · overserviced · Jan 3, 2018 · N531JL · Airbus A320232 · APU Oil System
  > RETURNED TO FIELD DUE TO EXTREME ODOR AFTER POWER REDUCTION FROM TOGA THRUST AT APPROX 1500 FT AGL. OXYGEN MASKS UTILIZED. CABIN DUMPED AND RETURNED. ALL CREW & PAX SMELLED ODOR. APU BLEED AIR SUPPLY SYSTEM. COMPLIED WITH INFO NOTICE T015A. FOUND APU
- [SDR YENA201709110761](https://openairdocs.org/sdr/YENA201709110761.md): Window · failed · Sep 11, 2017 · N531JL · Airbus A320232 · Windshield/Door Rain/Ice Removal
  > DURING APPROACH, A LOUD CLICKING SOUND WAS HEARD FROM THE AREA OF THE CAPTAIN`S AFT WINDOW AND STORAGE BIN. SHORTLY AFTER THE CLICKING SOUND, BOTH PILOTS NOTED A SIGNIFICANT ELECTRICAL ODOR.THE SOUND STOPPED AFTER ABOUT 90 SECONDS THE ODOR CONTINUED. NO SMOKE
- [SDR YENA201705250402](https://openairdocs.org/sdr/YENA201705250402.md): Filter · failed · May 25, 2017 · N531JL · Airbus A320232 · Air Distribution System
  > STRONG AIRCRAFT ODOR OF DIRTY SOCKS EVIDENT DURING TAKEOFF. ODOR BEGAN APPROX. 5000' IN BOTH COCKPIT AND ENTIRE CABIN. COCKPIT ODOR DISIPATED AT APPROX FL 180. CABIN ODOR CONTINUED UNTIL REACHING CRUISE- FL 320 (APPROX 27 MIN. INTO FLT). TOGA T/O WITH BLEED ON
- [SDR YENA201705250401](https://openairdocs.org/sdr/YENA201705250401.md): Filter · failed · May 25, 2017 · N531JL · Airbus A320232 · Air Distribution System
  > STRONG ODOR OF DIRTY SOCKS EVIDENT DURING TAKEOFF. ODOR BEGAN APPROXIMATELY 5000 FT IN BOTH COCKPIT AND ENTIRE CABIN. COCKPIT ODOR DISIPATED AT APPROX FL 180. CABIN ODOR CONTINUED UNTIL REACHING CRUISE- FL 320 (APPROX 27 MIN. INTO FLT). TOGA T/O WITH BLEED ON
- [SDR YENA20160830772](https://openairdocs.org/sdr/YENA20160830772.md): Door Sill · corroded · Aug 30, 2016 · N531JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON L-2 DOOR SILL FWD SIDE AT FRAME 67+5" AND STR 23L AROUND SCREW HOLES FOR GIRT BAR FITTING. R & R L-2 DOOR SILL IAW SRM 51-72-11, PN D5348004320601.
- [SDR YENA20160830771](https://openairdocs.org/sdr/YENA20160830771.md): Door Sill · corroded · Aug 30, 2016 · N531JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON R2 DOOR SILL AFT SIDE AT FR67 AND 18 AND STR 23R UNDER GIRT BAR FITTING AREA. R & R WITH A DOUBLER REPAIR PLATE.
- [SDR YENA20160830770](https://openairdocs.org/sdr/YENA20160830770.md): Door Sill · corroded · Aug 30, 2016 · N531JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON REAR CARGO DOOR SILL WEB. REMOVED CORROSION BEYOND LIMITS, REPLACED WEB IAW SRM 51-72-11, PN D5347556521090.
- [SDR YENA20160830769](https://openairdocs.org/sdr/YENA20160830769.md): Floorbeam · corroded · Aug 30, 2016 · N531JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO FLOOR CENTER BEAM. R & R FLOORBEAM FRAME 53-54 IAW SRM 51-42-11.
- [SDR YENA20160830768](https://openairdocs.org/sdr/YENA20160830768.md): Floorbeam · corroded · Aug 30, 2016 · N531JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED CABIN FLOORBEAM Y-1292 AT FRAME 16; REMOVED AND INSTALLED NEW FLOORBEAM Y-1292 AT FRAME 16 IN FWD CABIN IAW SRM 51-42-11 AND 51-72-11, PN D5311281300251.
- [SDR YENA20160830767](https://openairdocs.org/sdr/YENA20160830767.md): Floor Support · corroded · Aug 30, 2016 · N531JL · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED AROUND FLOOR SUPPORT FASTENER HOLES Y-1732 AT FRAME 68. REMOVED AREA AROUND FLOOR SUPPORT FAST HOLES Y-1732 AT FRAME 68 IAW SRM 53-41-14-283-002, PG 1-4. CUT OUT DAMAGED AREA, LOCATED, DRILLED, DEBURRED, A
- [SDR YENA20160830766](https://openairdocs.org/sdr/YENA20160830766.md): Floorbeam · corroded · Aug 30, 2016 · N531JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN FLOORBEAM Y-1292, FRAME 16+12. REMOVED AND INSTALLED NEW FLOORBEAM Y-1292 FRAME 16 IN FWD CABIN IAW SRM 51-44-11 AND 51-72-11, PN D5311281300051.
- [SDR YENA20160830765](https://openairdocs.org/sdr/YENA20160830765.md): Floorbeam · corroded · Aug 30, 2016 · N531JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN FLOORBEAM Y503 AT FRAME 16. R & R FLOORBEAM Y503 IAW SRM 51-72-11, PN D5311282600200.
- [SDR YENA20160830764](https://openairdocs.org/sdr/YENA20160830764.md): Floorbeam · corroded · Aug 30, 2016 · N531JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON RT TRIPLE BEAM FORWARD SEGMENT Y1292, 4" FWD OF FRAME 66. R & R FLOORBEAM Y1292 IAW SRM 51-72-11, PN D5347219021100.
- [SDR YENA20160830763](https://openairdocs.org/sdr/YENA20160830763.md): Floorbeam · corroded · Aug 30, 2016 · N531JL · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN FLOORBEAM Y254 FROM FRAMES 16-20. R & R FLOORBEAM Y254 IAW SRM 51-72-11, PN D5311281700420.
- [SDR YENA20150220029](https://openairdocs.org/sdr/YENA20150220029.md): Stringer · corroded · Feb 20, 2015 · N531JL · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > ON MAINTENANCE CHECK FOUND STRINGER 41L AT FRAME 53 SPLICE HAS CORROSION. IAW NR 440214-20290, FOUND STR 41L, FR 53 TO BE OUT OF LIMITS, REMOVED DAMAGED PART OF STR 41L FR53 TO FR54, FABRICATED SPLICE REPAIR AND INSTALLED IAW SRM 53-00-13, FIG 201.
- [SDR YENA20150220028](https://openairdocs.org/sdr/YENA20150220028.md): Skin · contaminated · Feb 20, 2015 · N531JL · Airbus A320232 · Elevator, Plate/Skin
  > ON HEAVY MAINTENANCE CHECK, FOUND RT ELEVATOR UPPER SURFACE HAS A WATER INDICATION 12" FROM OTBD EDGE, 6" FROM T/E, 1.5" DIAMETER. REF NR 440214-20267, CUT OUT TRAPPED WATER INDICATION ON RT ELEVATOR UPPER SURFACE 12" FROM OTBD. 6" FROM T/E, 1.5" DIAMETER ZONE
- [SDR YENA20130719153](https://openairdocs.org/sdr/YENA20130719153.md): Filter · odor · Jul 19, 2013 · N531JL · Airbus A320232 · Air Distribution System
  > BAD ODOR INFLT, ODOR CAUSED NUMEROUS CUSTOMERS TO COMPLAIN DURING FLT. R & R LT AND RT OZONE FILTERS IAW AMM 21-51-41. OPS AND LEAK CHECKED OK IAW AMM 21-21-45.
- [SDR YENA20110815321](https://openairdocs.org/sdr/YENA20110815321.md): Slide · defective · Aug 15, 2011 · N531JL · Airbus A320232 · Escape Slide
  > FLT 724 NAS-JFK, DURING MAINTENANCE ON NON-ROUTINE-00010 CANNOT SAFELY PIN R2 ESCAPE SLIDE TO FACILITATE MAINTENANCE. REMOVED AND REPLACED R2 DOOR SLIDE IAW AMM 25-62-44-04. ALL REQUIRED OPS CHECK OK.
- [SDR YENA20110328225](https://openairdocs.org/sdr/YENA20110328225.md): Computer · failed · Mar 28, 2011 · N531JL · Airbus A320232 · Auto Throttle System
  > FLT 811 JFK-POP, AIR RETURN TO JFK DUE DURING TAKEOFF AUTOTHRUST KICKED OFF. CREW TURNED IT BACK ON DURING CLIMB & IT WORKED NORMAL. NR 2 FMGC FAILED AFTER TAKEOFF. RESET NR 2 FMGC HAD NO EFFECT A/C POSITION INVALID MESSAGE CAME UP. REMOVED AND REPLACED NR

Next page: https://openairdocs.org/aircraft/N531JL/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 = 'N531JL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N531JL/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
