Airbus A321-271N
Service difficulty reports · 1,583
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.
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
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 HALA2020081000170Regulator · malfunctionedATB - ETOPS SIGNIFICANT SYSTEM - AIR ENGINE 1 BLEED FAULT. AIR ENGINE 2 BLEED FAULT FOLLOWED ECAMS. RETURN TO LAND. INSPECTED #1 ENGINE DUCTING FOR PNEUMATIC LINES BAD, INSPECTION CHECKED GOOD. PERFORMED HIGH POWER RUN, DURING RUN FOUND #2 ENGINE PRV BAD,#1SDR HALA2020080500168Pitot Head · damagedDURING PITOT STATIC TEST, FOUND PITOT PROBE 1 (9DA1) BURNED. REMOVED AND REPLACED PITOT PROBE 1 (9DA1) PER AMM 34-11-15. OPS TESTED GOOD.SDR HALA2020080400167Panel · leakingETOPS SIGNIFICANT SYSTEM - DURING CRUISE ECAM AIR ENG 2 BLEED LEAK. THIRD WRITE UP TODAY. FOUND GAP CLEARANCE OF OVER PRESSURE FLAP DOOR ON PANEL 423DT. REWORKED PRECOOLER PANEL 423DT #2 PYLON PER TASK CARD E105-213003-INI. REPLACED PANEL AND CLEARANCE CHESDR HALA2020071600147Bleed Air Sys · faultedOPEN - ETOPS SIGNIFICANT SYSTEM - AIR ENG 2 BLEED FAULT. REPAIR IN WORKSDR HALA2020060600122Flap · puncturedOPEN - ON MX WALK AROUND PUNCTURE DAMAGE ON LT IB FLAP 32" FROM OUTB EDGE AND 0.5" FWD OF TE. LT INBOARD FLAP TAB HAS BEEN REPAIRED PER E105-C30022-TER, OK TO CLOSE OK FOR SERVICE.SDR HALA2020060500121Valve · malfunctionedETOPS SIGNIFICANT SYSTEM. ENG 1 TURB COOL FAULT. PERFORMED DRY MOTOR OF ENG NR 1 PER AMM 73-21-00-710-809-A. PER MOC NEED TO CHANGE ACC VALVE. REMOVED AND REPLACED NR 1 ENG ACC VALVE PER AMM 75-24-01-400-801-A. PENDING OPS CHECK. OPS AND LEAK CHECK GOOD SDR HALA2020051700111Shutoff Valve · leakingETOPS SIGNIFICANT SYSTEM - FOUND FUEL LEAKING PASS LP SHUT OFF FUEL VALVE ON # 2 ENGINE. // REMOVED AND REPLACED LP SHUT OFF FUEL VALVE PER AMM 28-24-41-400-001-A ON # 2 ENGINE OPS AND LEAK CHECK GOOD.SDR HALA2020051600110Transducer · malfunctionedETOPS SIGNIFICANT SYSTEM - AIR BLEED MESSAGE ON ECAM. // REMOVED AND REPLACED BLEED DIFFERENTIAL PRESSURE TRANSDUCER ON # 1 ENGINE. BITE TEST OKAY, OKAY TO CONTINUE.SDR HALA2020050700107Light · shortedEPSU OPERATION BITE CHECK FAILS.// REMOVED 4R DOOR SLIDE FOR TROUBLE SHOOTING REF AMM 25-62-44-000-804-A. FOUND 4R SLIDE ESC EMERGENCY LITE SHORTED PER ASM 33-51-02. REPLACED 4R DOOR SLIDE IAW AMM 25-62-44-400-803A UP TO AND INCLUDING STEP 4B(1)(D). COMPLETED SDR HALA2020032300068Warning System · activatedOPEN - OPEN INDICATION, 3R EMERGENCY EXIT.SDR HALA2020031600060Computer · malfunctionedSUP - DMI # 202294. DOOR R EMERGENCY EXIT OPEN AFTER ENGINE START. BTB. ( ECAM DOOR PAGE INDICATIONS PASSENGER DOORS OPEN INDICATION (MAY BE INOPERATIVE PROVIDED: A VISUAL CHECK IS MADE BEFORE EACH DEPARTURE TO ENSURE THAT THE AFFECTED DOOR(S) IS CLOSED AND LOSDR HALA2020031100059Eec · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB - ECAM: ENG 2 FADEC SYS FAULT FOLLOWED BY ENG 2 MINOR FAULT OIL CHIP DETECTED. // INSTALLED NEW PHMU ON #2 ENG, CONDITION SAME. RE-INSTALLED ORIGINAL PHMU PER AMM 77-31-01. REMOVED AND REPLACED #2 EEC PER AMM 73-21-01. LAND TEST SDR HALA2020031000057Pressure Sensor · faultyETOPS SIGNIFICANT SYSTEM - MX STATUS MSG "ENG 1 FADEC". // PERFORMED FADEC 1 SYS TEST, #1 OIL PRESS SENSOR FAULTING. REMOVED & REPLACED ENG 1 OIL PRESS SENSOR PER AMM 79-33-21. MX STATUS CLEARED OK FOR SERVICE.SDR HALA2020030600052Engine · overservicedFLIGHT CREW REPORTED THAT DURING DESENT THERE WAS DIRTY SOCKS SMELL IN THE CABIN//PERFORMED TSM71-00-00-810-847-A FOUND #1 ENGINE OIL OVER SERVICED DRAIND OIL TO CORRECT AMOUNT REF AMM 79-00-00-610-801 PERFOMED IDLE RUN REF AMM 71-00-00 BOTH PACKS OPERATED NO SDR HALA2020030300045Fcu · malfunctionedATB - ETOPS SIGNIFICANT SYSTEM - FCU ALT SEL-INOP, V/S WORKS. OPEN C/B/DEC-INOP. FCU RESET ACCOMPLISHED WITH NO CHANGES. // REMOVED AND REPLACED FCU PER AMM 22-81-12. AFS TEST PASSED. LAND CAT 3 TEST PASSED. OK FOR SERVICE.SDR HALA2020022700044Chip Detector · false indicationETOPS SIGNIFICANT SYSTEM- AFTER LANDING: ECAM ENG 1 OIL CHIP DETECTED. // PERFORMED TSM 79-35-00-810-808-A "CHIP DETECTED ALERT BY ODM" NO METAL DEBRI FOUND. OK TO CONTINUE. REMOVED AND REPLACED OIL FILTER PER AMM 79-21-06-960-801-A. PERFORMED IDLE RUN LEAK CHSDR HALA2020022100041Apu · shutdownETOPS SIGNIFICANT SYSTEM - X2 APU SHUTDOWN DURING START. // RESTART APU BY EXTERNAL POWER PER AMM 49-00-00-860-008-A. OPS CHECK OKAY OK FOR SERVICE. NO ISSUE NOTEDSDR HALA2020021300036Engine · making metalETOPS SIGNIFICANT SYSTEM - #1 ENG FBC MAG CHIP DETECTOR FOUND METAL. // PERFORMED AMM 79-00-00-281-802-A CH4 A SECTION 6.0 FINDINGS SENT TO MANAGEMENT. REF CASE NUMBER: CAS-69938-Q9M7V2 PRATT AND WHITNEY. LAB REF SEMUS816. LAB REF SEMUS817. NO FOLLOW UP ACTIONSDR HALA2020021210034Autothrust Sys · malfunctionedETOPS SIGNIFICANT SYSTEM - BLOCK TURN BACK - AUTO THRUST AND CAT 3 SYSTEM INOP. SHUTDOWN ENGINE AND RESET AUTO/THRUST AND DISCONNECT. // PERFORMED AFS TEST PER AMM 22-96-00, OPS TEST PASSED. OK FOR SERVICE. LAND TEST PASSED PER AMM 22-97-00.SDR HALA2020020500029Display · abnormalETOPS SIGNIFICANT SYSTEM - WX RADAR DISPLAY ERROR, 60 DEGREE LEFT, OA MONITOR. // PERFORMED BITE TEST OF WEATHER RADAR SYSTEM PER AMM 34-41-00-740-002-A. NO FAULTS DISPLAY TEST PATTERN OPERATING NORMALLY, OK FOR SERVICE.SDR HALA2020020300025Unknown · odorOPEN - FUMES, DIRTY SOCK SMELL ON DESCENT THROUGH 4000'. REPEAT WRITE-UP, FUME FORM FILLED OUT. // FERRY FLIGHT REQUIRED. THIS AIRCRAFT HAS BEEN INSPECTED THIS DATE AND IS SAFE FOR THE INTENDED FLIGHT.SDR HALA2020021000920Fire Loop · faultedSUP - ECAM: ENG. 2 FIRE LOOP A FAULT ON CLIMB. // REPLACED FIRE LOOP A DETECTOR PER AMM 26-12-16, FUNCTIONAL CHECK OK. OK FOR SERVICE.SDR HALA20200130020Warning Light · false activationETOPS: ECAM - ENG 2 FIRE LOOP A FAULT ON CLIMB. REPLACED FIRE LOOP A DETECTOR PER AMM 26-12-16, FUNCTIONAL CHECKED OK.SDR HALA2020011700016Engine · vibrationATB, NR 2 ENGINE. HIGH VIBRATION. IFSD. REMOVED AND REPLACED THE NR 2 ENGINE.SDR HALA2020011500015Engine · vibrationETOPS SIGNIFICANT SYSTEMS - ECAM ENG 1 - ENG VIB. BTB. NR 1 ENGINE REPLACEMENT. REMOVED NR 1 ENGINE S/N P770609 AND INSTALLED NR 1 ENGINE S/N P770677, PER W/O 172866 TASK CARD J321-72-HWI-02.SDR HALA2020010800007Fire Loop · chafedETOPS - ENG 2 FIRE LOOP A FAULT ILLUMINATED AFTER ENGINE SHUTDOWN // FOUND #2 ENG AGB LOOP A HIGH TEMP CABLE CHAFED. REPLACED LOOP A HARNESS AND RAIL ASSY PER AMM 26-12-61. MECH 5418. OPS CHECK PENDING. REPLACED #2 ENG LOOP A FORWARD FIRE/OVERHEAT DETECTOR PERSDR HALA2020010600001Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER GO AROUND ECAM "ENG 1 START VALVE FAULT. START VALVE NOT CLOSED"
COMPLIED WITH ECAM ACTIONS. // PERF EEC OPS TEST NO.6 PER AMM 73-21-00-710-807-A. NO DEFECTS NOTED.SDR HALA2019122600528Warning Message · false activationDURING DESENT THROUGH 12500, THE NR 1 ENGINE FIRE LOOP, A FAULT APPEARED ON ECAM WITH NO ASSOCITED CAUTION ALERT MASSAGE LASTED APPROX 2 MIN ON ECAM//T/S REF TSM 26-12-00-810-825-A, PERFORMED VI IAW AMM 26-12-00-200-802, VERFIED ALL CONNECTIONS TIGHT AND SECUSDR HALA2019122300527Unknown · odorAT 1250Z A GARBAGE TYPE ODOR STARTED IN THE CABIN AND INCREASED FOR THE NEXT TEN MINUTES. ONE PASSENGER FELT ILL, AT FIRST, THE SMELL WAS IN CABIN. IT LATER DISAPPEARED. NOTED BY MX. OK TO CONTINUE.SDR HALA2019122300526Warning Message · false activationNR 1 ENGINE FIRE LOOP -A- FAULTED ECAM DURING APPROACH. TROUBLESHOT IAW TAM 26-12-00-810-851-A, POST SB 26-1112. DETECTOR CONFIRMED AND NO FAULTS NOTED ON OPERATIONAL TEST, VISUAL INSPECTION OF DETECTORS AND HARNESS FOUND NO DEFECTS NOTED, RESTIANCE CHESDR HALA2019122000525Sensor · malfunctionedETOPS SIGNIFICANT SYSTEM - ECAM AIR PACK 2 OVHT 37 MIN INTO FLIGHT @FL320. FOLLOWED ECAM PROC. AFTER COOL DOWN TURNED PACK BACK ON. FAILED AGAIN. LEFT PACK 2 OFF.// PERFORMED TSM 21-61-00-810-802-A, CLEANED TEMP SENSOR 32HH & 34HH, CONDITION IMPROVED, NO OVER SDR HALA2019121800521Check Valve · leakingETOPS SIGNIFICANT SYSTEM - BTB ECAM APU BLEED LEAK AFTER ENGINE START FOLLOWED BY APU LEAK FED BY ENGINES, INTERMITTENT FAULT LIGHT ON ENG 1 BLEED SWITCH. // INSPECTED APU COMPARTMENT, CARGO BAY PANEL AFT COMPARTMENT AND THE COMPARTMENT DUCTS FOR ANY BLEED LEASDR HALA2019121700520Fire Detector · malfunctionedETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP A FAULT ON DESCENT INTO HNL. // REMOVED ENG 1 FDU 1 FOR TROUBLESHOOTING. REINSTALLED SAME. OPS CHK PENDING. CB'S Q38, Q39, A06, A07 PULLED + COLLARED. OPS CHK PENDING. FOUND HARDWARE NOT SECURED ON FIRE DETECTOR LOOP SDR HALA2019121700519Fire Loop · faultedETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP A FAULT, REPEAT WRITE-UP // T/S PER TSM 26-12-00-810-803-A. REMOVED AND REPLACED #1 ENGINE LOOP A AFT DETECTOR PER AMM 26-12-17-000-803-A. OPS CHECK GOOD. NO DEFECTS NOTED.SDR HALA2019121700518Connector · looseETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP A FAULT, REPEAT WRITE-UP // INSPECTED ENG 1 FIRE LOOP, FOUND LOOSE CONNECTOR @ ENG 1 FIRE LOOP. RE-TORQUED CONNECTOR AS REQUIRED. PERFORMED FDU BITE CHECKED, PER AMM 26-12-00. TEST PASSED NO FAULTS NOTED. OK TO CONTINSDR HALA2019121600514Connector · looseETOPS - ENG 1 FIRE LOOP A FAULT, REPEAT WRITE-UP // INSPECTED ENG 1 FIRE LOOP, FOUND LOOSE CONNECTOR @ ENG 1 FIRE LOOP A. RETORQED CONNECTOR AS REQUIRED. PERFORMED FDU BITE CHECKED, PER AMM 26-12-00. TEST PASSED NO FAULTS NOTED.SDR HALA2019121300513Fire Detector · false indication4 ADDITIONAL INSTANCES OF ECAM ENG 1 FIRE LOOP A FAULT DURING DESCENT//REMOVED AND REPLACED ENG 1 AFT FIRE/OVERHEAT DETECTOR (4001WD1) IAW AMM 26-12-17. OPS CHK OF LOOP/ SQUIB NORMAL IAW AMM 26-12-00SDR HALA2019121100512Sensor · malfunctionedETOPS SIGNIFICANT SYSTEM - FOUND AIR BLEED ON MAINTENANCE. STATUS MESSAGE DURING PDC. // REMOVED & REPLACED DELTA PRESSURE SENSOR ON ENG #2 PER AMM 36-11-18-000-801-A & AMM 36-11-18-400-801-A. OP'S CHK GOOD. OK TO CONT. SVC.SDR HALA2019120500506Slide · unwanted deploy1R ESCAPE SLIDE RAFT DEPLOYED BY CATERING SERVICE. // INSTALLED 1R ESCAPE SLIDE RAFT PACK PER AMM 25-62-44-400-803-A. SECURITY CHECK OK. OK FOR SERVICE.SDR HALA2019120400504Warning Message · false activationINFO TO MAINTENANCE: ENG 1 FIRE LOOP A ON APPROACH//PERFORMED VISUAL INSPECTION OF THE ENG FIRE DETECTION SYSTEM PER AMM 26-12-00-200-802-A NO DEFECT FOUND AND PERFORMED OPERATIONAL TEST OF THE ENG FIRE AND OVERHEAT DETECTION PER AMM 26-12-00-710-002-A. TESTSDR HALA2019120200501Fire Detector · false activationNR 1 ENGINE FIRE LOOP A ILLUMINATED DURING DESCENT, EXTINGUISHED ON LANDING. REMOVED AND REPLACED THE NR 1 ENGINE FIRE LOOP A AFT FIRE DETECTOR IAW AMM 25-12-17-04 CONF 21. PERFORMED OPERATIONAL TEST OF ENGINE FIRE DETECTION SYSTEM IAW AMM 26-12-00-710-001.SDR HALA2019120200502Warning Message · false activationENG 1 FIRE LOOP A FAULT 2X ON DESCENT MULTIPLE WRITE UP//TROUBLESHOT IAW HAL A321 TSM 26-12-00-810-912A LAST LEG FAULT ENG 1 LOOP A. NO CURRENT FAULTS OR FAILURES DURING TSM PROC. NO TROUBLE FOUND AT THIS TIME SYSTEM OPERATIONALLY CHECKS NORMALSDR HALA2019120200500Fire Warning · false activationENG FIRE LOOP A ECAM ON DECENT//PERFORMED OPERATIONAL TEST ENG FIRE AND DETECTION SYSTEM AMM 26-12-00 TEST PASS AIRCRAFT CONTINUE SERVICE MESSAGE CLEAREDSDR HALA2019111900491Smoke Warning · false activationSMOKE LAVATORY SMOKE ON POST FLIGHT REPORT. // PERFORMED T/S IAW TSM 26-17-00-810-804-A. NO FAULTS DETECTED. OK FOR SERVICE.SDR HALA2019111400485Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ON CLIMB OUT THROUGH FL260 ECAM MASTER CAUTION FUEL ACT XFR FAULT, PERFORMED ECAM ACTION ACT FWD TXFR OK. // FQI RESET, OPS CK GOOD. FUEL TRANSFER NORMALLY, A/C OK FOR SVC REF AMM28-46-00-740-001.SDR HALA2019111400484None · noneATB - BIRD STRIKE ON DEPARTURE. RIGHT SIDE OF AIRCRAFT. // ACCOMPLISHED AMM TASK 05-51-14-200-803-A. FOUND EVIDENCE OF BIRD STRIKE ON INBOARD RH FLAP. WILDLIFE SVC COLLECTED EVIDENCE. CLEANED AREA. NO DEFECTS NOTED. A/C OK FOR SVC.SDR HALA2019110600466Engine · stalledSUP - ATB- ENG 1 COMPRESSOR STALL (LOUD BANG), POWER LOSS, FOLLOWED BY HIGH ENG 1 VIBS. IN MIDDLE OF HIGH VIS QRH, ENG 1 FAILED FOLLOWED BY ECAM ENG 1 FAIL. // REF W/O 167588 REMOVED AND REPLACED #1 ENG PER T/C J321-72-HWI-02. OPS AND LEAK CHECK GOOD. OK FOR SSDR HALA20191106470Engine · damagedATB- ENG 1 COMPRESSOR STALL (LOUD BANG), POWER LOSS, FOLLOWED BY HIGH ENG 1 VIBS. IN MIDDLE OF HIGH VIS QRH, ENG 1 FAILED FOLLOWED BY ECAM ENG 1 FAIL. // REF W/O 167588 REMOVED AND REPLACED #1 ENG PER T/C J321-72-HWI-02. OPS AND LEAK CHECK GOOD. OK FOR SERVICESDR HALA2019110200465Life Raft · low pressureSUP - LIFE RAFT RESERVOIR PRESSURE AT 2650 PSI, FERRY FLIGHT REQUIRED. // REMOVED AND REPLACED LIFE RAFT PER AMM 25-66-41. SECURITY CHECK GOODSDR HALA201910310462Pump · inoperativeETOPS - FUEL R TK PUMP 1 LO PR // R&R RIGHT TK PUMP 1 PER AMM 28-21-51, PERFORMED OPS/LEAK CHECK WITH SATISFACTORY RESULTS. OK TO CONT. SVC.
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