Airbus A321-271N

Service difficulty reports · 1,580

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 = 'A321271N'
  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.

SDR HALA20250609167Rod · damagedATB - ON CLIMB OUT ECAM ENG 1 BLEED RESET PER MOC. RETURN TO HNL. FOUND #1 ENG FAV ACTUATOR ROD DAMAGED @ FAV LEVER ARM. REPLACED FAV ACTUATOR ROD AND BOLT PER AMM 36-11-54. COND/SECURITY/OPS CHK OK. A/C OK FOR SVC.Jun 7, 2025 · N204HA · Airbus A321271N · Compressor Bleed ValveSDR HALA20250609168Starter · faultedETOPS - APU AUTOSHUTDOWN 3 TIMES. REMOVED AND REPLACED STARTER ON APU PER AMM 49-42-51. REPLACED CLUTCH PER AMM 49-42-51. REPAIRED DAMAGED WIRE PER E105 -C30086-INI OPS CHECK GOOD OK TO CONTINUEJun 6, 2025 · N214HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20250606163Igniter · failedETOPS - ENG 2 IGN A FAULT DURING START. REMOVED AND REPLACED IGN A IGNITER PLUG ON ENG 2 PER AMM 74-21-01. OPS CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICEJun 5, 2025 · N208HA · Airbus A321271N · Spark Plug/IgniterSDR HALA20250604162Duct · damagedETOPS - WHILE PERFORMING TASK CARD E36-24-01-32 HPV VALVE. TUBE ASSY- ECS MUSCLE PRV FITTING WAS DAMAGED ON P/N 636100005-519 DUCT ASSY STARTER ECS. FOUND ON REMOVAL ENG 2. REMOVED AND REPLACED ECS DUCT ASSY PER AMM 36-11-49. INSTALLED NEW PRV FITTING LINE PERJun 3, 2025 · N205HA · Airbus A321271N · Air Distribution SystemSDR HALA20250604161Fire Loop · faultedETOPS - ENG 1 FIRE LOOP B FAULT IN CRUISE. REMOVED & REPLACED FWD FIRE / OVERHEAT DETECTOR PER AMM 26-12-17. ECAM CLEARED OPS TEST OF FDU 1 PER AMM 26-12-00 TEST OK. OK FOR SERVICE.Jun 3, 2025 · N202HA · Airbus A321271N · Fire DetectionSDR HALA20250602157Igniter · faultedETOPS - APU AUTO SHUT DOWN TWICE CALLED MX, SHUT DOWN THRID TIME ALSO NOTICED FUEL SLOWLY DRIPPING FROM APU DRAIN MAST. REMOVED AND REPLACD APU IGNTIER PLUG PER AMM 49-41-41 AND APU IGNITION UNIT PER AMM 49-41-38. OPS AND LEAK CHK GOOD. OK FOR SVCMay 30, 2025 · N226HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20250529154Display · faultedETOPS - MCDU'S DON'T MATCH WHEN IT COMES TO FUEL PREDICTION, TIME PREDICTION, AND VERTICAL PATH ERROR. FO'S MCDU APPEARS TO SHOW TIME: 4 MINUTES EARLIER, FUEL BURN: 400 MORE POUNDS, ABOVE DESCENT PATH: 400 FEET. REMOVED AND REPLACED FQIC PER AMM 28-42-34-04. NMay 27, 2025 · N208HA · Airbus A321271N · Fuel Indicating SystemSDR HALA20250527150Valve · faultedATB DUE TO ECAM ENG 2 BLEED FAULT. REMOVED AND REPLACED #2 ENGINE FAN AIR VALVE PER AMM 36-11-54. BITE TEST OF LEFT ENGINE BLEED SYSTEM GOOD. PERFORMED IDLE RUN OF #2 ENGINE. ALL CHECKS GOOD. OK TO CONTINUEMay 25, 2025 · N208HA · Airbus A321271N · Engine Bleed Air SystemSDR HALA20250527151Igniter · faultedETOPS - APU AUTO SHUTDOWN. REMOVED AND REPLACED APU IGNITER PLUG PER AMM 49-41-41. REMOVED AND REPLACED IGNITION UNIT PER AMM 49-41-38. OP'S CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE.May 24, 2025 · N209HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20250522146Wire Harness · faultedETOPS - ENG 1 FIRE LOOP A FAULT ON ECAM PAGE. REMOVED AND REPLACED FIRE LOOP A HARNESS AND REMOVED AND REPLACED FIRE LOOP A DETECTOR CABLE ( 418KS) PER AMM 26-12-61. OPS CHECK GOOD OK FOR SVCMay 21, 2025 · N212HA · Airbus A321271N · Fire Protection System WiringSDR HALA20250520143Exciter · faultedETOPS - APU START FAILED 3 TIMES WHEN ATTEMPTING TO START AFTER LANDING. ECAM VERIFIED AUTO SHUTDOWN EACH TIME. FOLLOWED TSM 49-00-81-810-825,REMOVED AND REPLACED IGNITION EXCITER PER AMM 49-41-38 AND REMOVED & REPLACED IGNITER PLUG PER AMM 49-41-41. OPS CHECKMay 19, 2025 · N205HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20250514134Sensor · faultedETOPS - AIR PACK 2 REGUL FAULT IN CRUISE. AMBER XX C SENSOR ON BLEED PAGE. PERFORMED A320 FIM TASK 21-61-00-810-A. REMOVED AND REPLACED P2 COMP TEMP SENSOR PER A320 AMM 21-61-11. OPS CHK GOOD. OK FOR SVC.May 13, 2025 · N217HA · Airbus A321271N · Cabin Temperature Control SystemSDR HALA20250514133Igniter · faultedETOPS - ON START ENG 2, ENGINE REATTEMPT 2ND ATTEMPT SUCCESSFUL ENG 2 IGN A FAULT. REPLACED #2 ENG A IGNITER PLUG PER AMM 74-11-01. AUDIBLE CHECK GOOD. OK FOR SVC.May 13, 2025 · N214HA · Airbus A321271N · Spark Plug/IgniterSDR HALA20250514132Fire Loop · faultedETOPS - ENG 1 FIRE LOOP B FAULT CAME ON MULTIPLE TIMES DURING CRUISE AND WOULD EXTINGUISH. FOUND THERMAL DAMAGE ON CONTACTS OF 454VC1. REPLACED ALL 4 CONTACTS OF 454VC1 PER ESPM 20-48-24. FDU 1 OPS CHECK OK PER AMM 26-12-00. PERFORMED ENGINE RUN PER AMM 71-00-May 13, 2025 · N214HA · Airbus A321271N · Fire DetectionSDR YENA2025051300475Slide · unwanted deployDURING HEAVY MAINTENANCE: LH OVERWING EXIT SLIDE INADVERTENTLY DEPLOYED BY BUSINESS. SLIDE REMOVED FROM AIRCRAFT; REF TO MZJ W/O FL2164 NR 20004, INSTALLED SERVICEABLE EMERGENCY SLIDE WING LH I.A.W A321 AMM 25-62-42-400-007-A.May 10, 2025 · N2017J · Airbus A321271N · Escape SlideSDR YENA2025051300474Indicator · inoperativeDURING HEAVY MAINTENANCE: LH OVERWING "SLIDE ARMED" LIGHT INOP; REF TO ASCENT WO FL2164 NR 20036, PERFORMED T/S PROCEDURE EPSU 17WL TO COMMUNICATE WITH THE CIDS PER A321 TSM TASK 33-73-00810-900-A AND RESET DEU-B PER A321 AMM 23-73-00-740-005-B, PERFORMED OPS May 10, 2025 · N2017J · Airbus A321271N · Emergency EquipmentSDR HALA20250509026Smoke Detector · false activationSMOKE LAVATORY SMOKE LAV D. FA REPORTED ALL CLEAR. PERFORMED OPERATIONAL CHECK OF THE LAV SMOKE DETECTION PER AMM 26-17-00-710-001-A. OPS CHECK GOOD. NO FAULTS NOTED. A/C OK TO CONTINUEMay 6, 2025 · N227HA · Airbus A321271N · Fire DetectionSDR HALA20250507127Fire Loop · false indicationETOPS - ENG 1 FIRE LOOP B FAULT 3X IN CRUISE. CLEARED ON ITS OWN. REMOVED & REPLACED ENG 1 FIRE LOOP B IAW AMM 26-12-17, OPS TEST OK. NO FAULT NOTED. OK FOR SVCMay 6, 2025 · N214HA · Airbus A321271N · Fire DetectionSDR HALA20250507126Wire Harness · shortedETOPS - ENG 2 FIRE LOOP B FAULT ECAM MESSAGE APPEARED BRIEFLY AFTER ENGINE START. CLEARED ON ITS OWN. FOUND SHORT TO GROUND ON ENGINE 2 FIRE LOOP B HARNESS (4166KS) REMOVED & REPLACED HARNESS PER AMM 26-12-62.May 6, 2025 · N205HA · Airbus A321271N · Fire Protection System WiringSDR HALA20250506124Fire Loop · faultedETOPS - SPURIOUS ENG1 FIRE LOOP B ECAM. ECAM ILLUMINATED 4 TIMES DURING FLIGHT. REMOVED AND REPLACED ENG1 AGB LOOP B PER AMM 26-12-17, PERFORMED FDU BITE TEST PER AMM 26-12-00 TEST OK. A/C OK FOR SVC.May 5, 2025 · N214HA · Airbus A321271N · Fire DetectionSDR HALA20250505121Oil Filter · faultedETOPS - APU AUTO SHUTDOWN AFTER 2 ATTEMPTS. PERFORMED TSM 49-00-81-810-849-A. REMOVED & REPLACED APU OIL FILTER ELEMENTS PER AMM 49-91--41-200-002-A. OPERATED APU PER AMM 49-00-00-860-009-A. NO DEFECTS NOTED. OK FOR SERVICE.May 3, 2025 · N213HA · Airbus A321271N · APU Oil SystemSDR HALA20250505025Radome · damagedFOUND BIRD STRIKE ON RADOME DAMGE BEYOND LIMITS. REMOVED AND REPLACED RADOME IAW AMM 53-15-11. OPS CHECK GOOD . OK TO CONTINUEMay 2, 2025 · N214HA · Airbus A321271N · Aerodynamic FairingsSDR HALA20250502119Engine · bird ingestionETOPS - #2 ENGINE BIRD STRIKE DAMAGE. NEED TO REMOVE ENG 2 FAN BLADES (1-20) DAMAGE OUT OF LIMITS. REMOVED FAN BLADES ON ENG 2 (1-20) PER AMM 72-11-01-000-801-A. REMOVED INLET CONE PER AMM 72-11-01-000-801-A. INSTALLED #2 ENGINE FAN BLADES #1-20 PER A321 TASK May 1, 2025 · N218HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA20250428115Apu · shutdownETOPS - APU: AUTO SHUT DOWN. REMOVED STARTER AND CLUTCH AND INSTALLED STARTER AND CLUTCH PER AMM 49-42-51 AND 49-42-52. FUCTIONAL CHECK GOOD. REPLACED APU FUSE PER AMM 49-42-00-960-003-A OPS CHECK GOOD. A/C OK FOR SVCApr 25, 2025 · N205HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) SystemSDR HALA20250423114Display · intermittentETOPS-CAPTAIN'S MCDU 3L BUTTON WORKS ONLY INTERMITTENTLY. REMOVED AND REPLACED CAPT'S MCDU PER AMM 22-82-12. OPS CHECK GOOD, OK TO CONT. SERVICE.Apr 22, 2025 · N216HA · Airbus A321271N · Central DisplaySDR HALA20250421110Fuel Filter · faultedETOPS-APU AUTO SHUTDOWN TWICE ON STARTUP. FOUND CLOGGED OIL FILTER GEN SCAV + LUBE FILTERS MSG. REMOVED AND REPLACED OIL FILTERS APU. OPS AND LEAK CHK GOOD REF AMM49-91-41. REMOVED AND REPLACED APU FUEL FILTER PER AMM 49-32-41-920-001-A. OPS CHECK GOOD NO LEAKApr 18, 2025 · N213HA · Airbus A321271N · APU Engine Fuel and ControlSDR HALA20240421109Igniter · faultedETOPS-APU AUTO SHUTDOWN X2. REPLACED IGNITION UNIT & IGNITER PLUG PER AMM 49-41-38/ AMM 49-41-41. APU ECB TEST GOOD + OPS TEST GOOD. OK FOR SVC.Apr 18, 2025 · N205HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20250416108Igniter · failedETOPS-BTB: APU FAIL. REPLACED APU IGNITOR PLUG AND LEAD REF AMM 49-41-41 AND 49-41-43, OPS TEST NORMAL. OK FOR SVC.Apr 15, 2025 · N208HA · Airbus A321271N · APU Start/Ignition SystemSDR HALA20250414105Fire Loop · faultedETOPS-ECAM - ENG 1 FIRELOOP B FAULT. REMOVED AND REPLACED ENG 1 FIRE LOOP B HARNESS (4166KS). PER AMM 26-12-62-400-802-A. FIRELOOP TESTS OK. OK FOR SVC.Apr 11, 2025 · N214HA · Airbus A321271N · Fire DetectionSDR HALA20250409104Igniter · damagedETOPS - DURING ENG 1 BORESCOPE INSP OF THE COMBUSTION CHAMBER AND HPT NOZZLE GUIDE VANES, IGNITER PLUG WAS REMOVED AND FOUND DAMAGED. REPLACED IGNITER REF AMM 74-21-01. CHECKS OKApr 8, 2025 · N214HA · Airbus A321271N · Spark Plug/IgniterSDR HALA20250407101Switch · brokenETOPS - INFO TO MAINTENANCE: RADAR "SYS SWITCH DETENT IS BROKEN ALLOWING IT TO BE BUMPED TO THE ON POSITION, WHICH CAN CAUSE A HAZARD AT THE GATE. REMOVED AND REPLACED WXR CONTROL UNIT . BITE TEST PER 34-41-00. TEST OK, NO FAULTS NOTED. OK FOR SERVICE.Apr 4, 2025 · N217HA · Airbus A321271N · Weather Radar SystemSDR HALA20250402096Speaker · inoperativeETOPS - FOUND CABIN LOUDSPEAKERS ABOVE SEATS 12A, 15A, 17A, 23A, 27A, 35A, 41A,45A, 2J, 11J, 14J, 16J, 21J, 33H, AND 39J NOT WORKING. REMOVED AND REPLACED CABIN LOUDSPEAKERS PER AMM 23-73-51. OPS CHECK OK FOR SERVICEApr 1, 2025 · N228HA · Airbus A321271N · Interphone/Passenger Announcement (PA) SystemSDR HALA20250331092Fire Loop · faultedETOPS - BTB FOR AN ENG 1 FIRE LOOP FAULT CLEARED AFTER 10 MINUTES . REMOVED AND REPLACED ENGINE 1 AGB LOOP B PER A321 AMM 26-12-17-000-802-A AND 26-12-17-400-802A. FDU BITE CHECK PASS PERFORMED ENGINE RUN ON EGNINE #1 NO FAULTS AC OK TO CONTINUEMar 29, 2025 · N214HA · Airbus A321271N · Fire DetectionSDR HALA20250328091Sensor · faultedETOPS - ENG 1 OIL SYS FAULT AMBER ECAM MESSAGE POPULATED AT ENGINE SHUTDOWN. REMOVED & REPLACED #1 ENG MAIN OIL PRESS SENSOR PER AMM 79-33-21/401. LEAK AND OPS CK GOOD. NO OTHER FAULTS NOTED. A/C OK FOR SVC.Mar 27, 2025 · N228HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA20250325089Sensor · faultedETOPS - AIR PACK 1 REGUL FAULT AT GATE. REMOVED AND REPLACED PACK 1 COMP TEMP SENSOR PER A321 AMM 21-61-11-000-001-A. OPS CHK GOOD. OK FOR SVCMar 24, 2025 · N228HA · Airbus A321271N · Cabin Temperature Control SystemSDR HALA20250324084Wire Harness · looseETOPS - ENG 1 FIRE LOOP B FAULT APPEARED SEVERAL TIMES DURING FLIGHT. CLEARED AFTER 30-60 SEC. GROUND CHECK HARNESS 4166KA FOUND LOSE AND DAMAGED CLAMP NEAR 4001WD2 REMOVED AND REPLACED CLAMP CHECKED OK. OPS TEST FDU #1 TEST OK PER: AMM 26-12-00. CHECKED 454VCMar 22, 2025 · N214HA · Airbus A321271N · Fire Protection System WiringSDR HALA20250317081Igniter · damagedETOPS - DURING #2 COMBUSTION LINER INSPECTION FOUND LOWER IGNTITOR PLUG DAMAGED. REMOVED AND REPLACED RIGHT HAND LOWER IGNITOR PLUG PER AMM 74-21-01, OPS CHECK GOOD, OK TO CONTINUE.Mar 16, 2025 · N228HA · Airbus A321271N · Spark Plug/IgniterSDR HALA20250317016Skin · corrodedCORROSION FOUND ON RHW AILERON AT UPPER EXTERNAL SKIN NEAR TRAILING EDGE AREA. PERFORMED REPAIR IAW RI-HAL-57-023. DAMAGE IS RAISED TO SPEAR DUE TO NO ADL OR REPAIR. SEE SPEAR REF NO. N226HA/B4836/SPEAR001. SEE SJC NR 8027 AND NR 20005, 20006. SILVER DOT APPLIMar 14, 2025 · N226HA · Airbus A321271N · AileronsSDR HALA20250317015Skin · corrodedCORROSION FOUND ON LHW LOWER SURFACE OUTBOARD SIDE OF PYLON BETWEEN RIBS 8 AND 9. PERFORMED DAMAGE EVALUATION IAW A321N SRM 57-21-11-283-014 FIG 001 SHT 1 REV 35 DTD 01NOV24. REWORK EXTENDS OVER FASTENER HEAD, CONTACT AIRBUS. PERFORMED REPAIR IAW RI-HAL-57-022Mar 14, 2025 · N226HA · Airbus A321271N · Wing, Plate/SkinSDR HALA20250314011Radome · damagedPOSSIBLE BIRD STRIKE DESCENDING BETWEEN 6-5000 FEET. REMOVED & REPLACED RADOME PER AMM 53-15-11. OK FOR SERVICE.Mar 12, 2025 · N227HA · Airbus A321271N · Aerodynamic FairingsSDR HALA20250314080Wire Harness · faultedETOPS - ENG 1 FIRE LOOP A ECAM FOR ABOUT 1 MINUTE ON CLIMB OUT. GROUND CHECK 452VCA PIN 1 TO PIN 2 FOR 4002WD1 AND 452VCA PIN 3 TO PIN 4 FOR 4001WD1 INSULATION AND RESISTANCE CHECK OK. REMOVED AND REPLACED HARNESS 4165KS ON ENG #1 PER AMM 26-12-61. OPS CHECK OMar 12, 2025 · N214HA · Airbus A321271N · Fire Protection System WiringSDR HALA20250310077Sensor · dirtyATB - ALL LAVS NOT FLUSHING. FOUND LIQUID LEVEL SENSOR DIRTY. CLEANED LIQUID LEVEL SENOSR PER AMM 38-31-00. OPS CHECK GOOD. NO FAULTS/DEFECTS NOTED. OK FOR SVC.Mar 9, 2025 · N209HA · Airbus A321271N · Waste Disposal SystemSDR YENA2025031200250Apu · odorFLT#2637, JFK-STI. CLIMBING OUT AFT PA REPORTED AN OILY SMELL THAT STARTED ON T/O RAN ODOR CHECKLIST. ISOLATION UNSUCCESSFUL. JUMPSEAT CA WENT TO INVESTIGATE AND SMELLED AND INTERMITTENT KEPT OILY SMELL IN THE AFT GALLEY; C/W INFO NOTICE 2017 T055K PER DECISIMar 7, 2025 · N2044J · Airbus A321271N · Airborne Auxiliary Power Unit (APU) SystemSDR HALA20250303010Oil System · overservicedWEAK DIRTY SOCKS SMELL THROUGHOUT CABIN AND COCKPIT. STRONGER IN BACK OF PLANE. STARTED UNDER 5000'. TURNED ON APU BLEED AND SMELL DISAPATED. DURING ETOPS PDSC NOTICED #2 ENG OIL OVERSERVICED. REMOVED 2 QRTS. PERFORMED TSM 71-00-00-810-847-A. NO SMELLS NOTED.Feb 28, 2025 · N217HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA20250303074Generator · faultedETOPS - RECEIVED ELEC APU GEN FAULT ECAM AFTER LANDING. ECAM PROCEDURE DID NOT RESTORE APU GENERATOR POWER. REMOVED AND REPLACED APU GENERATOR PER AMM 24-23-51. OPS AND LEAK CHECK GOOD. NO FAULTS NOTED. OK FOR SERVICE.Feb 28, 2025 · N202HA · Airbus A321271N · AC Generator-AlternatorSDR YENA2025030300226Pressure Switch · failedFLT$137, JFK-STI. (AIRCRAFT PERFORMED AN AIR TURN BACK) ' HYD Y ENG 2 PUMP LO PR; REMOVED AND REPLACED #2 ENG HYDRAULIC YELLOW PRESSURE SWITCH 3074 GD IAW AMM 29-13-17 LEAK CHECK AND OPS CHECK GOOD NO MSGS NOTED ON ECAM.'Feb 27, 2025 · N2039J · Airbus A321271N · Hydraulic System, MainSDR HALA20250226072Pressure Sensor · faultedETOPS - FOUND OIL PRESSURE DIFFERENTIAL SENSOR BAD PER TASKCARD 321-730000-WI-1 W/O 335093 FIN- 4077KS. REMOVED AND REPLACED OIL PRESSURE DIFFERENTIAL SENSOR PER AMM 79-33-23. OPS AND SECURITY CHECK GOD. BITE AND LEAK CHECK GOOD.Feb 25, 2025 · N217HA · Airbus A321271N · Engine Oil PressureSDR YENA2025022400189Unknown · odorFLT#149, JFK-GND. 'VERY STRONG MAGIC MARKER SMELL DESCENDING THROUGH 10' DISSIPATED AT 6', FLT DECK & FWD GALLEY ( PACKS ).Feb 23, 2025 · N2047J · Airbus A321271N · Air Distribution SystemSDR HALA20250220065Packing · failedATB - GREEN HYD RES LOW LEVEL ECAM REACHING 32,000'. THEN GREEN LOW HYD LO PRES ECAM. AIR TURN BACK TO HNL. FOUND BROKEN PACKING AT #1 ENG PUMP PRESSURE SWITCH. INSTALLED NEW PACKING PER AMM 29-13-17/802-A. OPS CHECK GOOD. NO LEAKS NOTED. A/C OK FOR SVC.Feb 19, 2025 · N214HA · Airbus A321271N · Hydraulic System, MainSDR HALA20250218007Autothrottle Sys · faultedRTO APPROX 70 KTS. ECAMS: AUTO FLT/ AUTO THROTTLES OFF, RUD TRAVEL LIMIT & RED SPD LIMIT ANNUNCIATOR ON PFD. F.O. AIRSPEED READ ZERO THRU 70 KTS. REMOVE /REPLACED #2 ADM PER AMM 34-11-17-400-001-A. REPLACED FAC 1& 2 PER AMM22-66-34-400-002-A. PERFORMED AFFeb 16, 2025 · N202HA · Airbus A321271N · Auto Throttle System
Back to Airbus A321-271N