# Service difficulty reports: Airbus A320-251N

A list on [Airbus A320-251N](https://openairdocs.org/model/airbus-a320-251n.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 14 · 657 reports

- [SDR F3LA202610020451](https://openairdocs.org/sdr/F3LA202610020451.md): Door Sill · corroded · Oct 1, 2026 · N378FR · Airbus A320251N · Fuselage Main, Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF THE AFT CABIN FLOOR STRUCTURE FOUND CORROSION R2 DOORSILL BEAM FR-68. PERFORMED REPLACEMENT OF R2 DOOR SILL IAW-SRM-53-41-14-300-001 REV 50.
- [SDR F3LA202610020450](https://openairdocs.org/sdr/F3LA202610020450.md): Door Sill · corroded · Oct 1, 2026 · N378FR · Airbus A320251N · Fuselage Main, Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF THE AFT CABIN FLOOR STRUCTURE FOUND CORROSION R2 DOORSILL BEAM FR-68. PERFORMED REPLACEMENT OF R2 DOOR SILL IAW-SRM-53-41-14-300-001 REV 50. /END/
- [SDR F3LA202608070442](https://openairdocs.org/sdr/F3LA202608070442.md): Slide Raft · failed · Aug 6, 2026 · N389FR · Airbus A320251N · Escape Slide
  > FOUND DURING RON MAINTENANCE NO DELAY RECORDED. LP636349 ITEM #1. L2 DOOR SLIDE 7502MM FAILED EPSU TEST. REMOVED AND REPLACED L2 DOOR SLIDE 7502MM, OPS TEST GOOD. TORQUE WRENCH: F9TAB14213C DUE: 08-2026 AMM 25-62-44-000-012A, AMM 25-62-44-400-002A. /END/
- [SDR F3LA202608030441](https://openairdocs.org/sdr/F3LA202608030441.md): Actuator · failed · Jul 31, 2026 · N354FR · Airbus A320251N · Leading Edge Slat Actuator
  > REFERENCE LP 518114 #1 INFLIGHT SLATS FAULT, SLATS STUCK AT ZERO FOR LANDING. INBOUND FLT 3046. FOUND BY FLIGHT CREW UPON LANDING WITH ECAM WARNING MESSAGE. A/C WAS GROUNDED. FOUND ACTUATOR FLAG DEPLOYED. R & R ACTUATOR IAW AMM 27-84-49-000/400-002-A AND OPS
- [SDR F3LA202607300440](https://openairdocs.org/sdr/F3LA202607300440.md): Tube · broken · Jul 28, 2026 · N351FR · Airbus A320251N · Cabin Cooling System
  > CABIN FUME/ODOR EVENT CLIMB & CRUISE. FOLLOW UP TSM 05-50-00-810-831-A, DID FIND DAMAGED & BURN OUT THE COMPRESSOR TUBES AND THE DUCT ON PACK 1 (TYPE S), REMOVED & REPLACED HOSES IAW AMM 21-52-21-000-802-A/400-802-A. REMOVED AND REPLACED RECIRCULATION FILTERS
- [SDR F3LA202607210438](https://openairdocs.org/sdr/F3LA202607210438.md): Fitting · corroded · Jul 20, 2026 · N373FR · Airbus A320251N · Fuselage Main, Attach Fittings
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON FWD L1 DOORSILL SHAPE. REQUIRES TO BE REPLACED AS PER A320N SRM 51-72-11 REV 49. REPLACEMENT OF FWD L1 DOORSILL SHAPE AS PER SRM 51-72-11 REV.49 MX ACTION IS ACCEPTABLE. /END/.
- [SDR F3LA202607210437](https://openairdocs.org/sdr/F3LA202607210437.md): Beam · corroded · Jul 20, 2026 · N373FR · Airbus A320251N · Fuselage Main, Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON BEAM FR.66-70 Y765 AND OUT OF SRM ADL AS PER SRM 53-41-14 REV 49. REQUIRES TO BE REPLACED AS PER A320N SRM 51-72-11 REV 49. BEAM FR.66-70 REPLACED AS PER A320-SRM 51-72-11 REV 49.
- [SDR F3LA202607210439](https://openairdocs.org/sdr/F3LA202607210439.md): Shear Plate · corroded · Jul 19, 2026 · N373FR · Airbus A320251N · Fuselage Miscellaneous Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON AFT WET AREA R/H SHEAR PLATE FR 69-70. REQUIRES TO BE REPLACED AS PER A320N SRM 51-72-11 REV 49. AFT WET AREA R/H SHEAR PLATE FR 69-70 WAS REPLACED AS PER SRM 51-72-11 REV 49. MA A
- [SDR SOKF2026072001](https://openairdocs.org/sdr/SOKF2026072001.md): Transmitter · faulted · Jul 18, 2026 · N901AV · Airbus A320251N · Hydraulic Indicating System
  > CONDUCTING FLIGHT AV408 FROM SAL TO ORD WHEN A BLUE HYD SYS MALFUNCTION OCCURRED DURING CRUISE PHASE OF FLIGHT. THE CREW REPORTED HYD B RSVR LO LVL & HYD B LO PR DURING FLIGHT, INDICATING A LOW RESERVOIR LEVEL INDICATION AND SUBSEQUENT LOSS OF PRESSURE IN TH
- [SDR F3LA202607180435](https://openairdocs.org/sdr/F3LA202607180435.md): Door Sill · corroded · Jul 18, 2026 · N373FR · Airbus A320251N · Fuselage Main, Structure
  > REFERENCE LTPR NR 5001494265-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON RT AFT DOOR SILL. REQUIRES TO BE EVALUATED AS PER SRM 53-41-14 REV 49. CORROSION WAS REMOVED AND REPAIR WAS PERFORMED ON DOOR SILL FROM FR 67 TO
- [SDR 2026FA0000559](https://openairdocs.org/sdr/2026FA0000559.md): Potable Water · inoperative · Jun 30, 2026 · N965AV · Airbus A320251N · Potable Water System
  > NO PORTABLE WATER DURING FLIGHT. IAW TSM 38-12-00-810-814-A REV.77 PERFORMED OPERATIONAL TEST OF PORTABLE WATER DRAIN SYSTEM AS PER AMM 38-14-00-710-001-A REV.77 DATE 01-MAY 2026 AND ALL OK
- [SDR F3LA202606140428](https://openairdocs.org/sdr/F3LA202606140428.md): Battery · no test · Jun 14, 2026 · N343FR · Airbus A320251N · Emergency Lighting
  > DURING SCHEDULED HEAVY CHECK EPSU TEST FOUND 10WL FAILED TEST. AIRCRAFT WAS NOT GROUNDED. REMOVED AND REPLACED 10WL EPSU BATTERY IAW AMM 33-51-38-400-002-A OPS TEST GOOD. A/C OK FOR SERVICE. AIRCRAFT WAS RETUNED TO SERVICE.
- [SDR F3LA202606120427](https://openairdocs.org/sdr/F3LA202606120427.md): Door Sill · corroded · Jun 12, 2026 · N375FR · Airbus A320251N · Fuselage Main, Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON RT AFT DOOR SILL CORRODED REQUIRES TO BE EVALUATED AS PER SRM 53-41-14-283-002 REV 49. CORROSION WAS REMOVED AND REPAIR WAS PERFORMED ON DOOR SILL FROM FR.67 TO FR.68 IAW SRM 53-41
- [SDR F3LA202606120426](https://openairdocs.org/sdr/F3LA202606120426.md): Shear Plate · cracked · Jun 12, 2026 · N375FR · Airbus A320251N · Fuselage Miscellaneous Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON RH SHEAR PLATE AND REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV 49. PERFORMED REPLACEMENT OF R/H SHEAR PLATE AS PER A320N SRM 51-72-11 REV 49. MX ACTION IS ACCEPTABLE. /END/.
- [SDR F3LA202606120425](https://openairdocs.org/sdr/F3LA202606120425.md): Shear Plate · cracked · Jun 12, 2026 · N375FR · Airbus A320251N · Fuselage Miscellaneous Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON LH SHEAR PLATE AND REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV 49. PERFORMED REPLACEMENT OF L/H SHEAR PLATE AS PER SRM 51-72-11 REV 49 MX ACTION IS ACCEPTABLE. /END/.
- [SDR F3LA202606080423](https://openairdocs.org/sdr/F3LA202606080423.md): Battery · failed · Jun 8, 2026 · N389FR · Airbus A320251N · Emergency Lighting
  > NR 1 EPSU BITE TEST FAILED 12WL BATTERY. AC WAS NOT GROUNDED FOR THIS EVENT IT WAS SCHEDULED MX. REMOVED AND REPLACED EPSU BATTERY AT 12WL REF AMM 33-51-38-400-002-A. AC OK FOR SERVICE.
- [SDR F3LA202606040422](https://openairdocs.org/sdr/F3LA202606040422.md): Flap System · malfunctioned · Jun 3, 2026 · N361FR · Airbus A320251N · Trailing Edge Flap Control System
  > REFERENCE LP 557839 #2 AT ABOUT 4000' MSL, UNCOMMANDED ROLL WHILE GOING FLAPS 1 TO FLAPS 2 WITH SPEED BRAKE DEPLOYED. AUTO PILOT WAS OFF. OBSERVED ON FLIGHT CONTROL. SD PAGE LEFT AIL HALF DOWN, RIGHT AIL HALF UP. FELT REDUCED ROLL AUTHORITY WHILE TURNING. AC
- [SDR 2026FA0000475](https://openairdocs.org/sdr/2026FA0000475.md): Sensor · unserviceable · May 30, 2026 · N963AV · Airbus A320251N · Engine Pressure Ratio (EPR)
  > DURING TAKE OFF ENG 2 N2 OVERLIMIT 117.0% DURING 5 SECONDS. DUE TO PFR MESSAGES AND FOLLOWING TSM 73-21-00-810-B46-A REV 77 DATED 01/MAY/2026: THE OPERATIONAL TEST OF THE FADEC ON EEC CHANNEL B WAS PERFORMED IAW AMM 73-29-00-710-802-A REV 77 DATED 01/MAY/20
- [SDR F3LA202605190417](https://openairdocs.org/sdr/F3LA202605190417.md): Shear Plate · cracked · May 19, 2026 · N376FR · Airbus A320251N · Fuselage Miscellaneous Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON RH SHEAR PLATE AFT WET AREA AND REQUIRES REPLACEMENT IAW SRM 51-72-11 REV 49. PERFORMED REPLACEMENT OF RT SHEAR PLATE IAW SRM 51-72-11 REV 49. MX ACTION IS ACCEPTABLE.
- [SDR F3LA202605190416](https://openairdocs.org/sdr/F3LA202605190416.md): Door Sill · corroded · May 19, 2026 · N376FR · Airbus A320251N · Fuselage Main, Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON RT AFT DOOR SILL. REQUIRES TO BE EVALUATED IAW SRM 53-41-14 REV 49. CORROSION WAS REMOVED AND REPAIR WAS PERFORMED ON DOOR SILL AT FR. 68 IAW SRM 53-41-14 REV 49. MX ACTION IS ACCE
- [SDR F3LA202605190415](https://openairdocs.org/sdr/F3LA202605190415.md): Shear Plate · cracked · May 19, 2026 · N376FR · Airbus A320251N · Fuselage Miscellaneous Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON LT SHEAR PLATE AFT WET AREA AND REQUIRES REPLACEMENT IAW SRM 51-72-11 REV 49. PERFORMED REPLACEMENT OF LT SHEAR PLATE IAW SRM 51-72-11 REV 49. MX ACTION IS ACCEPTABLE.
- [SDR F3LA202605160413](https://openairdocs.org/sdr/F3LA202605160413.md): Power Supply · faulted · May 15, 2026 · N373FR · Airbus A320251N · Emergency Lighting
  > DURING HEAVY CHECK EPSU TEST FOUND AFT EPSU (13WL) FAULTING FOR INTERIOR AND EXTERIOR LIGHTS. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED R4 DOOR SLIDE IAW AMM 25-62-44-400-803-A. OPS TEST GOOD. RE-TESTED EPSU BATTERY TEST IAW AMM 33-51-38-400-002-A. OPS TES
- [SDR F3LA202604200404](https://openairdocs.org/sdr/F3LA202604200404.md): Door Sill · corroded · Apr 17, 2026 · N371FR · Airbus A320251N · Fuselage Main, Structure
  > REFERENCE LTPR NR 5001479407-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON R/H AFT DOORSILL. REQUIRES TO BE EVALUATED AS PER A320N SRM 53-41-14-283-002 REV 48. CORROSION WAS REMOVED AND REPAIR WAS PERFORMED ON DOORSILL FR
- [SDR F3LA202604200403](https://openairdocs.org/sdr/F3LA202604200403.md): Door Sill · corroded · Apr 17, 2026 · N371FR · Airbus A320251N · Fuselage Main, Structure
  > REFERENCE LTPR NR 5001479406-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON L/H AFT DOORSILL. REQUIRES TO BE EVALUATED AS PER A320N SRM 53-41-14-283-002 REV 48. CORROSION WAS REMOVED AND WAS FOUND IN ALLOWABLE LIMITS (CAT
- [SDR F3LA202604200402](https://openairdocs.org/sdr/F3LA202604200402.md): Floorbeam · corroded · Apr 17, 2026 · N371FR · Airbus A320251N · Fuselage Main, Floor Beam
  > REFERENCE LTPR NR 5001480168-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND CABIN FLOORBEAM Y-765 IN FR68 CORRODED. REQUIRED REPLACEMENT IAW SRM 53-41-14 REV 48. FLOORBEAM Y-765 IN FR 68 REPLACED IAW SRM 53-41-14 RE
- [SDR F3LA202604200401](https://openairdocs.org/sdr/F3LA202604200401.md): Shear Plate · cracked · Apr 17, 2026 · N371FR · Airbus A320251N · Fuselage Miscellaneous Structure
  > REFERENCE LTPR NR 5001479409-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON RH SHEAR PLATE AND REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV.48. PERFORMED REPLACEMENT OF R/H SHEAR PLATE AS PER A320N SRM 51-72-11 REV. 48 M
- [SDR F3LA202604200400](https://openairdocs.org/sdr/F3LA202604200400.md): Shear Plate · cracked · Apr 17, 2026 · N371FR · Airbus A320251N · Fuselage Miscellaneous Structure
  > REFERENCE LTPR NR 5001479408-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON LH SHEAR PLATE AND REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV.48. RERFORMED REPLACEMENT OF LT SHEAR PLATE AS PER A320N SRM 51-72-11 REV. 48 MX
- [SDR F3LA202604100399](https://openairdocs.org/sdr/F3LA202604100399.md): Battery · no test · Apr 9, 2026 · N358FR · Airbus A320251N · Emergency Lighting
  > NR 3 EPSU BATTERY 10WL FWD L FAILED TEST, AIRCRAFT WAS NOT GROUNDED, SCHEDULED HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (10WL) IAW AMM 33-51-38-000-002-A/33-51-38-400-002-A. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR F3LA202604100398](https://openairdocs.org/sdr/F3LA202604100398.md): Battery · no test · Apr 9, 2026 · N358FR · Airbus A320251N · Emergency Lighting
  > EPSU BATTERY 11WL EMER L FAILED TEST, AIRCRAFT WAS NOT GROUNDED AS A RESULT OF THE SDR REPORTABLE EVENT, SCHEDULED HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (11WL) IAW AMM 33-51-38-000-002-A/33-51-38-400-002-A. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO S
- [SDR F3LA202604030394](https://openairdocs.org/sdr/F3LA202604030394.md): Battery · failed · Apr 2, 2026 · N390FR · Airbus A320251N · Emergency Lighting
  > DISCREPANCY: REFERENCE LP178762 #1 EPSU BATTERY (12WL) FAILED TEST. AIRCRAFT WAS NOT GROUNDED AS A RESULT OF THE SDR REPORTABLE EVENT, SCHEDULED RON HEAVY CHECK. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERY (12WL) IAW AMM 33-51-38-000-002-A/33-51-38-4
- [SDR F3LA202603280393](https://openairdocs.org/sdr/F3LA202603280393.md): Battery · no test · Mar 28, 2026 · N350FR · Airbus A320251N · Emergency Lighting
  > NR 3 EPSU BATTERY (12WL) FAILED TO TEST, ACFT WAS NOT GROUNDED, SCHEDULED RON MAINTENANCE HEAVY CHECK. R & R THE EPSU BATTERY (12WL) IAW AMM 33-51-38-000-002-A, & 33-51-38-400-002-A. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
- [SDR F3LA202603280392](https://openairdocs.org/sdr/F3LA202603280392.md): Battery · no test · Mar 28, 2026 · N350FR · Airbus A320251N · Emergency Lighting
  > NR 2 EPSU BATTERY (11WL) EMERGENCY LIGHT FAILED TO TEST, ACFT WAS NOT GROUNDED. SCHEDULED RON MAINTENANCE HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (11WL) EMERGENCY LIGHT IAW AMM 33-51-38-000-002-A, & 33-51-38-400-002-A. OPS CHECKED GOOD. AIRCRAFT RE
- [SDR F3LA202603220390](https://openairdocs.org/sdr/F3LA202603220390.md): Shear Tie · cracked · Mar 22, 2026 · N372FR · Airbus A320251N · Fuselage Internal Mounting Structure
  > REFERENCE NR5001472996-0010. AC WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND R/H SHEAR PLATE FR69-70 CRACKED. REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV 47. PERFORMED REPLACEMENT OF R/H SHEAR PLATE BETWEEN FR 69-70 AS PE
- [SDR F3LA202603220389](https://openairdocs.org/sdr/F3LA202603220389.md): Shear Tie · cracked · Mar 22, 2026 · N372FR · Airbus A320251N · Fuselage Internal Mounting Structure
  > REFERENCE NR5001472996-0010. AC WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND L/H SHEAR PLATE FR69-70 CRACKED. REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV 47. PERFORMED REPLACEMENT OF L/H SHEAR PLATE BETWEEN FR 69-70 AS PE
- [SDR F3LA202603200386](https://openairdocs.org/sdr/F3LA202603200386.md): Power Supply · failed · Mar 20, 2026 · N378FR · Airbus A320251N · Emergency Lighting
  > REFERENCE LP702387 #2 EPSU BATTERY (10WL) FWD L FAILED TEST FAILED EPSU SYS TEST. AC WAS NOT GROUNDED AS A RESULT OF THIS SDR REPORTABLE EVENT, IT WAS A RON SCHEDULED HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (10WL) IAW AMM 33-51-38-000/400-002-A. OPS CH
- [SDR F3LA202603200385](https://openairdocs.org/sdr/F3LA202603200385.md): Power Supply · failed · Mar 20, 2026 · N378FR · Airbus A320251N · Emergency Lighting
  > REFERENCE LP702387 #3 EPSU BATTERY (11WL) EMERG L FAILED TEST FAILED EPSU SYS TEST. AC WAS NOT GROUNDED AS A RESULT OF THIS SDR REPORTABLE EVENT, IT WAS A RON SCHEDULED HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (11WL) IAW AMM 33-51-38-000/400-002-A. OPS
- [SDR F3LA202603200384](https://openairdocs.org/sdr/F3LA202603200384.md): Power Supply · failed · Mar 20, 2026 · N378FR · Airbus A320251N · Emergency Lighting
  > REFERENCE LP702388 #1 EPSU BATTERY (13WL) AFT L FAILED TEST FAILED EPSU SYS TEST. AC WAS NOT GROUNDED AS A RESULT OF THIS SDR REPORTABLE EVENT, IT WAS A RON SCHEDULED HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (13WL) IAW AMM 33-51-38-000/400-002-A. OPS C
- [SDR F3LA202603190383](https://openairdocs.org/sdr/F3LA202603190383.md): Power Supply · failed · Mar 19, 2026 · N351FR · Airbus A320251N · Emergency Lighting
  > DISCREPANCY: REFERENCE LP532313#3 EPSU BATTERY (12WL) FAILED EMERGENCY LIGHT TEST. AC WAS NOT GROUNDED AS A RESULT OF THIS SDR REPORTABLE EVENT, IT WAS A RON SCHEDULED HEAVY CHECK. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERY (12WL) IAW AMM 33-51-38-0
- [SDR F3LA202603190382](https://openairdocs.org/sdr/F3LA202603190382.md): Battery Pack · failed · Mar 19, 2026 · N351FR · Airbus A320251N · Emergency Lighting
  > EPSU BATTERY (13WL) FAILED EMERGENCY LIGHT TEST. AC WAS NOT GROUNDED. REMOVED AND REPLACED EPSU BATTERY (13WL) IAW AMM 33-51-38-000/400-002-A. OPS CHECK GOOD. AC OK FOR SERVICE.
- [SDR F3LA202603190381](https://openairdocs.org/sdr/F3LA202603190381.md): Battery Pack · failed · Mar 19, 2026 · N351FR · Airbus A320251N · Emergency Lighting
  > EPSU BATTERY (11WL) FAILED EMERGENCY LIGHT TEST. ACFT WAS NOT GROUNDED. REMOVED AND REPLACED EPSU BATTERY (11WL) IAW AMM 33-51-38-000/400-002-A. OPS CHECK GOOD. AC OK FOR SERVICE.
- [SDR F3LA202603160380](https://openairdocs.org/sdr/F3LA202603160380.md): Water Heater · burned out · Mar 12, 2026 · N392FR · Airbus A320251N · Buffet/Galleys
  > BURNING ELECTRICAL SMELL FROM FORWARD LAV. AC WAS GROUNDED AS A RESULT OF THIS SDR REPORTABLE EVENT. PERFORMED ISOLATION/DEACTIVATION OF FWD WATER HEATER, SMELL DISSIPATED AFTER TIME PER AMM 05-50-00-510-831-A. LP680661 ITEM #1 PLACED ON MEL 38-10-01B CN 12450
- [SDR F3LA202603040377](https://openairdocs.org/sdr/F3LA202603040377.md): Bottle · disengaged · Mar 3, 2026 · N317FR · Airbus A320251N · Passenger/Crew Doors
  > DURING SCHEDULED MAINTENANCE, MAINTENANCE FOUND L1 DOOR STRIKER LEVER OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IN A DISENGAGED POSITION. MAINTENANCE ARMED THE L1 DOOR STRIKER LEVER OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-
- [SDR F3LA202603020375](https://openairdocs.org/sdr/F3LA202603020375.md): Power Supply · no test · Mar 1, 2026 · N354FR · Airbus A320251N · Emergency Lighting
  > DURING HEAVY CHECK EPSU TEST FAILED DUE TO POSITION 10WL UNIT FAILURE. REMOVED AND REPLACED EPSU UNIT AT POSITION 10WL IN REF TO AMM 33-51-38-000/400-001-A. EPSU SYSTEM TEST OK./END/
- [SDR F3LA202603020374](https://openairdocs.org/sdr/F3LA202603020374.md): Access Panel · missing · Feb 27, 2026 · N311FR · Airbus A320251N · Wing, Plate/Skin
  > AIRCRAFT GROUNDED DUE TO EVENT-REFERENCE LP664307, ITEM 1. PANEL MISSING UNDER LEFT WING (AILERON PANEL). INSTALLED NEW ACCESS PANEL (575KB), PER AMM 57-51-37-400-005-A.
- [SDR F3LA202602170370](https://openairdocs.org/sdr/F3LA202602170370.md): Oil System · leaking · Feb 13, 2026 · N317FR · Airbus A320251N · APU Oil System
  > REFERENCE LP533532 ITEM #1 FUME EVENT AFT CABIN VERY STRONG MOVED TO FORWARD CABIN DIRTY SOCK SMELL., AC WAS GROUNDED AS A RESULT OF THE SDR REPORTABLE EVENT. FERRY FLIGHT FROM ELP TO LAS PLACED APU ON MEL, TRANSFERRED TO NON-ROUTINE REF NR141160 FOR MX ACTIO
- [SDR F3LA202602130369](https://openairdocs.org/sdr/F3LA202602130369.md): Battery · failed · Feb 13, 2026 · N370FR · Airbus A320251N · Emergency Lighting
  > DISCREPANCY: FAULT HAPPENED DURING A RON MAINTENANCE VISIT, NO FLIGHT DELAY AS A RESULT. AC WAS NOT GROUNDED AS A RESULT OF THE SDR REPORTABLE EVENT. REFERENCE LP498087 #3 DURING CIDS EPSU TEST 13WL BATTERY FAULT FOUND. CORRECTIVE ACTION: REMOVED AND REPLACED
- [SDR F3LA202602130368](https://openairdocs.org/sdr/F3LA202602130368.md): Elec Connector · contaminated · Feb 13, 2026 · N370FR · Airbus A320251N · Light System Wiring
  > FAULT HAPPENED DURING A RON MAINTENANCE VISIT, NO FLIGHT DELAY AS A RESULT, AC WAS NOT GROUNDED AS A RESULT OF THE SDR REPORTABLE EVENT. REFERENCE LP498087 #2 DURING EPSU TEST FAULT EXTERIOR LT 2/EPSU (1WL) FWD L, FAULT FOUND. REF NON-ROUTINE #141147. FOUND
- [SDR F3LA202602130367](https://openairdocs.org/sdr/F3LA202602130367.md): Floor Support · cracked · Feb 13, 2026 · N369FR · Airbus A320251N · Fuselage Miscellaneous Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT CABIN FLOOR SUPPORT Y765 HAS CORROSION BETWEEN FR 67-69. REMOVED AND REPLACED FLOOR BEAM Y765 BETWEEN FR 66-70 IAW SRM 51-72-11-911-001.
- [SDR F3LA202602130366](https://openairdocs.org/sdr/F3LA202602130366.md): Floor Support · cracked · Feb 13, 2026 · N369FR · Airbus A320251N · Fuselage Miscellaneous Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT WET AREA LONGITUDINAL BEAM AT Y-765 HAS CORROSION FROM C66 TO C68. REMOVED AND REPLACED CORRODED FLOOR SUPPORT Y-765 BETWEEN FR 66-70 IAW SRM 51-72-11-911-001 AND SRM 53-41-14-283-009.
- [SDR F3LA202602130365](https://openairdocs.org/sdr/F3LA202602130365.md): Plate · cracked · Feb 13, 2026 · N369FR · Airbus A320251N · Fuselage Miscellaneous Structure
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. SILL PLATE BETWEEN FR 69-70 RH SIDE IS CRACKED. REMOVED CRACKED SILL PLATE BETWEEN FR 69-70 RH SIDE & REPLACED IT WITH A NEW PLATE IAW AIRBUS A320 NEO SRM 51-42-11-911-001. /END/.

Next page: https://openairdocs.org/model/airbus-a320-251n/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 aircraft_model_key = 'A320251N'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a320-251n/reports

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