Airbus A320-251N
Service difficulty reports · 663
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR F3LA202509150289Battery · failedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING OPS CHK, FOUND EPSU BATTERY 11WL INOPERATIVLE. REPLACEMENT REQUIRED IAW AMM-33-51-38-400-002-A REV.103.
REPLACED EPSU BATTERY 11WL IAW AMM 33-51-38-400-002-A REV.103.SDR ANCF20250915128Pump · faultedHYD B SYS LO LVL FOLLOWED BY B SYS LO PR BLUE ELEC PUMP WAS TURNED OFF REQUEST BY ECAM WAS REMOVED THE HYD PUMP BLUE SYS (2075GJ) DUE WAS FOUND WITH HYD LEAK AT DRAIN IAW AMM TASK 29-12-51-000-001-A REV 73 WAS INSTALLED THE HYD PUMP BLUE SYS (2075GJ) IAW AMSDR RJEF20250901001Transducer · faultedON ENGINE 1: PERFORMED BORESCOPE OF BOOSTER BLADES IAW AMM 72-21-00-290-802-A NO DISCREPANCIES FOUND. REPLACED LEFT VSV ACTUATOR AMM 75-32-05-000/400-802-A. REPLACED RIGHT VSV ACTUATOR AMM 75-32-05-000/400-801-A. PERFORMED BSI OF HPT STG 1 BLADES AMM 72-52-0SDR F3LA202508270288Battery · failedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INCOMING CHECKS FOUND EPSU BATTERY 10WL INOP REPLACEMENT REQUIRED IAW AMM 33-51-38-400-002-A REV. 102. REPLACED EPSU BATTERY 10WL AMM 33-51-38-400-001 CONF 00 REV 102. MX ACTION IS ACCEPTABLESDR F3LA202508260287Power Supply · no testAIRCRAFT WAS UNDERGOING HEAVY SERVICE CHECK DURING RON MAINTENANCE, ITEM #3 BATT/EPSU (11WL) EMER L FAULT. R&R EPSU BATTERY 11WL REF AMM 33-51-38-400-001-A/AMM 33-51-38-400-001 TEST OK.SDR F3LA202508200283Battery Pack · failedAIRCRAFT WAS UNDERGOING A HEAVY SERVICE CHECK DURING RON MAINTENANCE, NO FLIGHT DELAY. LP492867 ITEM 3 EPSU BATTERY 13WL FAIL. INSTALLED NEW EPSU BATTERY IN REF TO AMM 33-51-38-400-002-A.SDR F3LA202508200282Battery Pack · failedAIRCRAFT WAS UNDERGOING A HEAVY SERVICE CHECK DURING RON MAINTENANCE, NO FLIGHT DELAY. LP492867 ITEM 2 EPSU BATTERY 12WL FAIL. INSTALLED NEW EPSU BATTERY IN REF TO AMM 33-51-38-400-002-A.SDR F3LA202508200285Servo Valve · failedAIRCRAFT WAS UNDERGOING SERVICE CHECK DURING RON MAINTENANCE AND WORKING MDDR# 1235083, NO FLIGHT DELAY. LP599245 ITEM 1 F/CTL AIL SERVO FAULT PLACED ON MEL 27-14-01B CN 1235081 PLACARD INSTALLED AND R/H WING INBOARD SERVO VALVE 33CE2 DEACTIVED. REMOVED ANDSDR F3LA202508190281Seat Track · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. PERFORMED REMOVAL OF CORRODED SEAT TRACK AT Y-1292 FROM FR.16 TO FR.20 IAW SRM 51-44-11 REV 45. PERFORMED INSTALLATION OF NEW SEAT TRACK AT Y1292 FROM FR.16 TO FR.20 IAW SRM 51-44-11 REV 45. MX ACTISDR F3LA202508190280Shear Plate · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF THE AFT CABIN FLOOR STRUCTURE A CRACK WAS FOUND ON LH SHEAR PLATE BETWEEN FR. 69 TO FR. 70. REPLACEMENT IS REQUIRED. PERFORMED REPLACEMENT OF LH SHEAR PLATE IAW SRM-51-72-11 REV SDR F3LA202508190279Shear Plate · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. R/H SHEAR PLATE BETWEEN FR.69-70 WAS FOUND CRACKED. PERFORMED REPLACEMENT OF R/H SHEAR PLATE BETWEEN FR. 69-70 I.A.W 51-72-11 REV 45. MX ACTION IS ACCEPTABLE.SDR F3LA202508130278Floor Support · corrodedFLOOR SUPPORT Y765 AT FR 66-70 FOUND CORRODED. REPLACEMENT IS REQUIRED IAW SRM 51-72-11 REV 44. FLOOR SUPPORT Y-765 AT FR66-FR67 INSTALLED IAW SRM 51-72-11 REV 44.SDR F3LA202508130277Door Sill · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF THE AFT CABIN FLOOR STRUCTURE FOUND CORROSION L2 DOOR SILL BEAM FR-69. PERFORMED REPAIR OF THE L2 DOOR SILL IAW-SRM-53-41-14-300-001 REV 45. MX ACTION IS ACCEPTABLE.SDR F3LA202508130276Door Sill · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF THE AFT CABIN FLOOR STRUCTURE FOUND CORROSION R2 DOOR SILL BEAM FR-68. PERFORMED REPAIR OF R2 DOORSILL IAW SRM-53-41-14-300-001 REV 45. MX ACTION IS ACCEPTABLE. /END/.SDR F3LA202508130275Floor Support · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND CABIN FLOOR SUPPORT Y-1292 CORRODED. REQUIRES REPLACEMENT AS PER SRM 51-72-11 REV 44. FLOOR SUPPORT AT Y-1292 WAS REPLACED AS PER SRM 51-72-11 REV 44. FLOOR SUPPORT AT Y-129SDR F3LA202508120274Seat Track · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION FOUND ON SEAT TRACK Y-1292 REPLACEMENT IS REQUIRED AS PER A320N SRM 53-11-15 REV 44. PERFORMED REMOVAL OF CORRODED SEAT TRACK AT Y-1292 FR 16, FR18, FR20 AS PER A320N SRM 51-44-11 REV 44.SDR F3LA202508120273Floor Support · corrodedREFERENCE LTPR NR 5001415390-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND FLOOR BEAM Y-756 AT FR66-FR70 CORRODED. REQUIRES REPLACEMENT AS PER SRM 51-72-11 REV 44. FLOOR BEAM Y-765 AT FR66-FR70 WAS REPLACED AS PER SDR F3LA202508120272Shear Plate · crackedREFERENCE LTPR NR 5001415392-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND R/H SHEARPLATE FR 69-70 CRACKED. REQUIRES REPLACEMENT AS PER SRM 51-72-11 REV 44. CORRECTIVE ACTION: R/H SHEARPLATE WAS REPLACED AS PER SRM 5SDR F3LA202508120271Shear Plate · crackedREFERENCE LTPR NR 5001415391-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND LH SHEAR PLATE FR 69 TO FR 70 CRACKED, REPLACEMENT IS REQUIRED AS PER 51-72-11 REV 44. PERFORMED REPLACEMENT OF LH SHEAR PLATE AS PER SRM 51-SDR F3LA202507250269Slide Raft · no testTHIS AC WAS NOT PULLED OUT OF SERVICE FOR THIS EVENT: REFERENCE LP511009 ITEM 1, FWD L/H SLIDE FAILED EPSU TEST. AMM 25-62-44-000-007-A1, 25-62-44-400-007-A REPLACED L/H FWD SLIDE EPSU TEST GOOD. TW F9TAB12568C DD 04/2026.SDR F3LA202507140267Skin · damagedDISCREPANCY: AC WAS PULLED OOS FOR THIS EVENT REFERENCE LOG PAGE LP585145 SUSPECTED TAIL STRIKE UPON LANDING.SDR F3LA202507140268Servo Valve · faultedLP461953 #2 ON CLIMB OUT IN A RIGHT TURN PLANE SHOOK VIOLENTLY SPEED 320 ALT 260 FOLLOWED BY FLT CTL AIL SERVO FAULT. FOLLOWED TSM 27-10-00-810-820-A, REMOVED AND REPLACED RH AILERON INBD SERVO CONTROL (33CE2) PER A320 AMM 27-14-51-000-001-A, 27-14-51-400-00SDR F3LA202507060265Slide · no testUPON INSTALLATION OF L1 SLIDER DOOR ON LP334753/3 EPSU TEST FAULT SHOWING ESCAPE SLIDE LT. AFT (L2). REMOVED AND REPLACED L2 DOOR SLIDE PACK-ASSY AS PER AMM 25-62-44-000-012-A/25-62-44-400-007-A. OPS CHECK GOOD T/W: F9TAB14011C.DD06/26/ /END/.SDR F3LA202507080266Eec · defectiveENG 2 FADEC SYS FAULT ON DEPARTURE CLIMBOUT, EMERGENCY CHECKLIST APPLIED, RETURNED TO ATL. REMOVED AND REPLACED ELECTRONIC ENGINE CONTROL (EEC) CHANNEL A IAW AMM 73-21-55-080-802-A/400-802-A OPS CHECKED GOOD.SDR ANCF20250707321Pump · faultedHYD Y RSVR LOW LVL AND LO PRESS SYSTEM HYD Y RSVR LOW LVL AND LO PRESS SYSTEM, IAW TSM 29-13-00-810-804-A, REPLACED ENGINE PUMP ON ENGINE #2 FOLLOWING INSTRUCTIONS GIVEN IN AMM 29-13-51-000-809-A AND AMM 29-13-51-400-809-A. PENDING ENGINE RUN UP AND TEST.SDR F3LA202507020262Power Supply · inoperativeBAT/EPSU (10WL) FWD L CLASS 1 FAULT. R & R ESPU AND BATTERY IAW AMM 33-51-38-000-001-A 33-51-38-400-001-A OPS CHECK OF ESPU COMPLETE IAW 22-51-00-710-001-A TEST OK INTERFACE AND PWR UP TEST DONE ON CIDS 1+2 IAW 23-73-00-740-005-B TEST OK FOR SERVICE.SDR F3LA202506210258Floor Support · corrodedREFERENCE LTPR NR 5001406003-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND CABIN FLOOR SUPPORT Y-254 AT FR 12-24 CORRODED. REQUIRED REPLACEMENT AS PER SRM 51-72-11 REV 44. CABIN FLOOR SUPPORT Y-254 AT FR66-70 REPLACSDR F3LA202506210257Door Sill · corrodedREFERENCE LTPR NR5001405999-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND CORROSION ON LH AFT DOOR SILL AT FRAME 68. PERFORMED REPAIR LAY OUT ON LH AFT DOOR SILL AT FRAME 68. REF A320 NEO SRM 53-41-14 REPAIR PRINCIPLSDR F3LA202506210256Floor Support · corrodedREFERENCE LTPR NR5001405976-0020 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND CABIN FLOOR SUPPORT Y1162.5 BETWEEN FR 68-69 CORRODED. REQUIRED REPLACEMENT AS PER SRM 53-41-14 REV 44. FLOOR SUPPORT Y1162.5 BETWEEN FR 68-SDR F3LA202506200255Floorbeam · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND CABIN FLOOR BEAM Y765 BETWEEN FR66-70 CORRODED. REQUIRED REPLACEMENT AS PER SRM 53-41-14 REV 44. FLOOR BEAM Y765 BETWEEN FR66-70 REPLACED AS PER SRM 53-41-14 REV 44. /END/.SDR F3LA202506200254Floorbeam · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND CABIN FLOOR BEAM Y765 BETWEEN FR66-70 CORRODED. REQUIRED REPLACEMENT AS PER SRM 53-41-14 REV 44. FLOOR BEAM Y765 BETWEEN 66-70 REPLACED AS PER SRM 53-41-14 REV 44.SDR ANCF2025062719Blower · faultedVENT BLOWER FAULT DURING CRUISE, PRESENTING NOISE AND FUMES. IAW AMM 21-26-51-000-001-A/400-001-A REMOVAL AND INSTALLATION BLOWER FAN WAS REPLACED SATISFACTORILY. OPERATIONAL TEST OF THE AEVC WAS PERFORMED TEST OK.SDR F3LA202506190252Shear Tie · crackedREFERENCE LTPR NR 5001406001-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON LH SHEAR PLATE BETWEEN FR 69-70. REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV 44. PERFORMED REPLACEMENT OF LH SHEAR PLATE IAW-SRM-51-72-11 REV 4SDR F3LA202506190251Shear Tie · crackedREFERENCE LTPR NR 5001406002-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON RH SHEAR PLATE BETWEEN FR 69-70. REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV 44. PERFORMED REPLACEMENT OF R/H SHEAR PLATE BETWEEN FR 69-70 ASSDR RJEF20250601001Servo Control · failedF/CTL R AILERON WITH OSCILATION AFTER TAKE OFF INCREASING WITH AIRSPEED INCREASE.THIS CONDITION PRODUCE HIGHT VIBRATION ON THE AC//REMOVED AND REPLACED AILERON SERVO CONTROL 33CE4 PER AMM A320 27-14-51-400-001-A TOOL USED QD2R200 SN 12046034907 02 NOV 2025 PN SDR F3LA202506110247Battery · failedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INCOMING CHECKS FOUND EPSU BATTERIES 13 WL INOP, REPLACEMENT REQUIRED AS PER AMM 33-51-38-04 CONF 00 REV. 102
CORRECTIVE ACTION: REPLACED EPSU BATTERY 13WL IAW AMM 33-51-38-400-001 CONF 00 RESDR F3LA202506090246Computer · faultedAC WAS PULLED OOS FOR THIS EVENT. REFERENCE LP493674 ITEM 1, ALMOST 3000LB FUEL IMBALANCE ON A 2.5 HOUR FLIGHT. RIGHT SIDE LOW. CORRECTIVE ACTION: REF NR-137619 -R/R FQIC 3QT OPS CK OK. REF AMM 28-42-34-000-001-A, 28-42-34-400-001-A.SDR F3LA202506040245Plate · crackedREFERENCE LTPR NR 5001403273-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON RH SHEAR PLATE BETWEEN FR69-70. REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11 REV 44. PERFORMED REPLACEMENT OF R/H SHEAR PLATE BETWEEN FR 69-70 AS SDR F3LA202506040244Plate · crackedREFERENCE LTPR NR 5001403272-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF THE AFT CABIN FLOOR STRUCTURE A CRACK WAS FOUND ON LH SHEAR PLATE BETWEEN FR69 TO FR70. REPLACEMENT IS REQUIRED AS PER A320N SRM 51-72-11 REV 44.SDR F3LA202505220237Power Supply · dischargedEPSU (11WL) EMER L/DEU-B (300 RHG) FAULT. REMOVED AND REPLACED EPSU (11WL) IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPS CHECK NORMAL. BITE OK. A/C OK FOR CONTINUED SERVICE.SDR F3LA202505220236Power Supply · dischargedNUMBER 3 BAT/EPSU (13WL) AFT L FAULT. REMOVED AND REPLACED EPSU (13WL) IAW AMM 33-51-38-000-002-A & 33-51-38400-002-A. OPS CHECKED NORMAL. BITE CHECK OK. A/C OK FOR CONTINUED SERVICE.SDR F3LA202505100233Shear Tie · crackedDISCREPANCY: REFERENCE AIRBORNE N/R 16065.0272 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT LH FUSE FR 69-70 SHEAR WEB IS CRACKED.
CORRECTIVE ACTION: REMOVED AND REPLACED L/H SHEAR WEB AT FR 69-70 IAW A320 NEO SRM 51-72-11. MX ACTION IS ACCSDR F3LA202505100232Shear Tie · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT RH FUSE FR 69-70 SHEAR WEB IS CRACKED. REMOVED AND REPLACED SHEAR WEB R/H BETWEEN FR 69-70 IAW A320 NEO SRM 51-42-11. MX ACTION IS ACCEPTABLE.SDR F3LA202505100231Seat Track · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. L1 DOOR O/B SEAT TRACK HAS CORROSION BETWEEN FR 18-20. REMOVED AND REPLACED L1 DOOR O/B SEAT TRACK IAW A320 SRM 51-72-11-911-001. MX ACTION IS ACCEPTABLE.SDR F3LA202505110234Unknown · odorDISCREPANCY: LP483210 ITEM #1 ODOR IN AFT CABIN DURING DESCENT THROUGH 10,000 AIRCRAFT REMOVED FROM SERVICE. COMPLETED TSM 05-50-00-810-831-A AND COMPLETED LEVEL A DECONTAMINATION OF THE ENVIRONMENT CONTROL SYSTEM IAW AMM 21-00-00-615-807-A. NO ODOR REMAINS SDR F3LA202505080229Beam · corrodedREFERENCE LTPR NR 5001395194-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORRODED BEAM AT Y-254 FRAME 20 REQUIRES REPLACEMENT REF A320NEO SRM 51-72-11-911-001 REV 43. PERFORMED REMOVAL OF CORRODED BEAM AT Y-254 BETWEEN FR 12-24 IAW SRM SDR F3LA202505080225Coupling · corrodedREFERENCE LTPR NR 5001395108-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND CABIN COUPLING ATTACHED TO FLOOR BEAM Y765 AT FR66-70 CORRODED. REQUIRED REPLACEMENT AS PER SRM 51-72-11 REV 43. CABIN COUPLING ATTACHED TOSDR F3LA202505080223Power Supply · failedDISCREPANCY: AIRCRAFT WAS UNDERGOING A HEAVY SERVICE CHECK DURING RON MAINTENANCE, NO FLIGHT DELAY. LP492867 ITEM #1 EPSU (11WL) FLAGGED UNIT FAULT EPSU, TEST FAILED.
CORRECTIVE ACTION: REF AMM 33-51-38-000-001-A AND 33-51-38-400-001-A. REMOVED AND REPLACED ESDR F3LA202505080228Shear Plate · crackedREFERENCE LTPR NR 5001395030-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CRACK ON RH SHEAR PLATE BETWEEN FR69-70. REQUIRES REPLACEMENT AS PER A320N SRM 51-72-11-911-001 REV 43. PERFORMED REPLACEMENT OF R/H SHEAR PLATE BETWEEN FR.69-SDR F3LA202505080227Shear Plate · crackedREFERENCE LTPR NR5001395102-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF THE AFT CABIN FLOOR STRUCTURE A CRACK WAS FOUND ON LH SHEAR PLATE BETWEEN FR69 TO FR 70. REPLACEMENT IS REQUIRED AS PER A320 NEO SRM 51-72-11-911-
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