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 HALA2018100500473Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENGINE NR 2 LOOP A FAULT DISPLAYED ON ECAM DURING CRUISE AT FL350,THEN SELF CLEARED. PERFORMED VISUAL INSP NR 2 ENG FIRE LOOPS, REF TSM 26-12-00-810-805. NO DEFECTS NOTED, FOUND BITE MCDU FDU TEST OK. NOTIFIED RON MOC PRIOR HISTORY ISDR HALA2018100500472Indication Sys · false activationETOPS SIGNIFICANT SYSTEM - BTB ECAM ENG 1 IL CHIP DETECTED. PERFORMED TSM 79-35-00-810-808-A CHECK MAIN ENG NR 1 OIL FILTER PER AMM 79-00-00-210-809. NO PARTICALS NOTED. REMOVED AND REPLACED OIL FILTER AS PRECAUTION. CHECK MAGNETIC CHIP DETECTORS (5 EA). NO DESDR HALA2018100100462Not Reported · malfunctionedETOPS SIGNIFICANT SYSTEM - WX RADAR SYS 2 IN AUTO HAS ERRONEOUS READINGS. NEEDS TO BE CALIBRATED. SYS 1 OPS OK. PERFORMED BITE TEST AND SYSTEM TEST OF WEATHER RADAR SYSTEM 2 PER AMM 34-41-00. NO DEFECTS NOTED. OPS TEST GOOD. OK FOR SVCSDR HALA2018100100458Tie Down · contaminatedAT GATE, FA'S AND PILOTS NOTICED STRONG CHEMICAL SMELL CONCENTRATED TOWARDS AFT/LAST 10 ROWS OF AIRCRAFT. FA'S COMPLAINED OF LIGHT HEADINESS. REMOVED EXCESS SEALANT AROUND BARRIER TIE DOWNS. VENTED AFT CARGO COMPARTMENT. NO CHEMICAL ODOR NOTED.SDR HALA2018092500435Mmr · malfunctionedETOPS SIGNIFICANT SYSTEM, HF DATA LINK INTERMITTENT. RESET MMR AND ATSU C/B AS REQUIRED. OPS CHECK GOOD.SDR HALA2018092500433Monitor · faultyETOPS SIGNIFICANT SYSTEM, ENG 1 OIL CHIP DETECTED. TROUBLESHOOT PER TSM 79-35-00-810-808-A PER STEP 8(A) REPLACED OIL DEBRIS MONITOR IAW AMM 79-35-21. RAN NR 1 ENGINE AND PERFORMED TEST NO 3 PER AMM 71-00-00-720-811-A AND TEST NO 6 PER AMM 73-21-00-710-807-A SDR HALA2018092500431Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 1 OIL CHIP DETECTED ECAM ON TAXI. INSPECTED NR 1 ENG OIL CHIP DETECTORS PER AMM 79-00-00-281-802A. NO CHIPS NOTED. INSPECTED NR 1 ENG OIL FILTER ELEMENT PER AMM 79-00-00-210-809A. NO CONTAMINATION NOTED. RAN ENGINE NO LEAK NOTED.SDR HALA2018092500434Warning System · false activationETOPS SIGNIFICANT SYSTEM - BTB ENG 2 IGN A FAULT. PERFORMED TASK 74-00-00-810-830-A. NO FAULTS NOTED ON GROUND. OK FOR SERVICE. ENG RUN ON GROUND FOUR TIMES ALL START SUCCESSFUL.SDR HALA2018091500422Carbon Seal · damagedSUP - ETOPS SIGNIFICANT SYSTEM - NR 2 ENGINE CHIP DETECTOR. FOUND AFT CARBON SEAL BAD. REMOVED AND REPLACED NR 2 ENGINE. OP'S AND LEAK CHECK OK.SDR HALA2018091500423Gps · malfunctionedATB - ON CLIMB OUT F/O ND DISPLAYED "GPS PRIMARY LOST" CHECKED NAVIGATION ERROR W/GROUND BASED VOR AND NAV ERROR +/- 6-7 / +1.0 DME. MCDUS SHOWED ACCUR HIGH, GPS PRIMARY, GPS MONITOR WAS NAV WITH 9 SATS EACH. PERFORMED AMM 34-55-00 BITE TEST OF VOR AND PERFORMSDR HALA201809170422Carbon Seal · failedNR 2 ENGINE OIL CHIP DETECTOR ACTIVATED. FOUND AFT CARBON SEAL BAD. REMOVE AND REPLACED THE NR 2 ENGINE.SDR HALA201809050410Fire Loop · false activationDURING CLIMB OUT, THE NR 2 ENGINE LOOP A FAULT ECAM MESSAGE DISPLAYED. MESSAGE CLEARED ITSELF. IAW FIM 26-12-00-810-825-A, PERFORMED AN OPS CHECK OF THE LOOP. NO DEFECTS NOTED. OK FOR SERVICE.SDR HALA2018090100409Fire Loop · malfunctionedDURING CLIMB OUT, THE NR 2 ENGINE FIRE LOOP A FAULT ECAM MESSAGE DISPLAYED, MESSAGE CLEARED ITSELF. IAW FIM 26-12-00-810-825-A PERFORMED AN OPS CHECK OF THE FIRE LOOP. NO DEFECTS NOTED. OK FOR SERVICE.SDR HALA201811060395Unknown · odorSUP - BTB - AFTER ENGINE START FA'S REPORTED UNUSUAL SMELL & VAPORS IN CABIN.// REMOVED AND REPLACED ENG #2 PER TASK CARD J321--72-HWI-01 AND J321 -72-HWI-02. ACCOMPLISHED DECONTAMINATION OF THE ECS SYS. PER AMM 21-00-00-615-004-A. RAN BOTH ENG'S & BOTH PACKS SDR HALA0218082100396Smoke Warning · false activationLAV SMOKE ECAM & MASTER WARNING FOR 10-15 SECONDS, FA'S INSPECTED W/ NO SMOKE OR SMELL -SIGNAL FROM LAV "D". RESET C/B CIDS NR 1 & NR 2 NO FAULTS NOTED, NO MESSAGE, OK TO CONTINUE. SYSTEM TESTED OK.SDR HALA0218082100395Oil System · leakingAFTER ENGINE START, FLT ATTENDANTS REPORTED AN UNUSUAL ODOR & VAPORS IN THE CABIN. MX REPORTED AN OIL LEAK FROM THE NR 2 ENGINE, AT THE 6 O'CLOCK POSITION, BEHIND FAN BLADES. OPEN.SDR HALA208082000385Warning Message · false activationDURING START OF THE NR 2 ENGINE, ING FAULT APPEARED. PERFORMED TASK 73-25-00-810-A45-A, NO FAULTS FOUND. CREW RAN THE NR 2 ENGINE, CYCLED A & B WITH NO FAULTS. OK FOR SERVICE.SDR 2018FA0000528Structure · bentTAIL STRIKE ON FUSELAGE BELLY AT FRAMES 62 TO 68, FOUND ON GROUND DURING WALK AROUND. SECTION 18 FRAMES 65-70 AND PARTIAL REPLACEMENT OF SECTION 17 FRAMES 61-64 STRINGER 32 LT TO 32 RT. ON AUGUST 13 2018 THE SUBJECT ACFT OPERATED BY HAWAIIAN AIRLINES. SUSTAISDR HALA2018081400376Metering Unit · malfunctionedNR 1 ENGINE OIL CHIP DETECTED DURING ENGINE START, SHUTDOWN THE ENGINE. PERFORMED TSM 79-35-00-810-808-A, EXAMINED THE W03 HARNESS & P10 CONNECTOR ON PHMU & P36 CONNECTOR ON OIL DEBRIS MONITORING SENSOR, NO DEFECTS NOTED. EXAMINED PINS & SOCKETS ON P10 ON TSDR HALA2018081400374Exciter · failedNR 2 ENGINE IGNITER A, FAULTED ON START. REPLACED THE NR 2 ENGINE IGNITER A IAW AMM 74-21-01-000-801-A. PERFORMED AN OPS TEST IAW 74-00-00-710-802-A, OPS OK FOR AUDIBLE TEST. RAN THE NR 2 ENGINE AND IGNITER FAULT RETURNED. REPLACED THE NR 2 ENGINE EXCITER ISDR HALA2018081300367Sensor · dirtyCABIN TEMP HIGH, 90F. BETWEEN ROWS 17 - 27, DURING CRUISE, CONDITION DISPLAYED. FWD 72/72, AFT 70/88 COCKPIT 76/92. FOUND THE TEMP SENSOR DIRTY. CLEANED THE TEMP SENSOR IAW 21-63-00. OPS CHECKED AND PERFORM CABIN TEMP SYSTEM IAW AMM 21-61-00.SDR HALA0218080800365Warning Message · false activationNR 1 ENG IGNITER A FAULTED ON START. PERFORMED TSM 74-00-00-810-834A, & AMM 74-00-80-710-802. IGNITERS A & B CHECKED OK. AUDIBLE SOUND HEARD. OK FOR SERVICE. NO 30 DAYS HISTORY.SDR HALA2018080100356Igniter · inoperativeNR 2 ENGINE IGNITER A SYSTEM INOPERATIVE. R & R THE IGNITER PLUG ON ENG#2 SYSTEM A. PER AMM 74-21-01. PERFORMED OPS CHECK, OPS CHECKS GOOD. A/C OK FOR SERVICE.SDR HALA2018073100355Display · malfunctionedDURING FLIGHT, LOWER ECAM DISPLAY STARTED CHANGING COLORS AND THEN WENT BLANK. TURNED BACK ON AFTER A COUPLE MINUTES. TROUBLESHOT LOWER ECAM DISPLAY IAW TSM 31-63-82-810-838-A, CLEANED DUST FROM BACK OF UNIT. PERFORMED FAULT CONFIRMATION IAW AMM 31-60-00-86SDR HALA2018073100354Display · malfunctionedLOWER ECAM DISPLAY DURING FLIGHT, STARTED CHANGING COLORS AND THEN WENT BLANK. TURNED BACK ON AFTER A COUPLE MINUTES. TROUBLESHOT THE LOWER ECAM DISPLAY IAW TSM 31-63-82-810-838-A. CLEANED DUST FROM BACK OF UNIT. PERFORMED FAULT CONFIRMATION IAW AMM 31-6SDR HALA2018073000351Smoke Warning · false activationSMOKE DETECTED ECAM IN LAVATORY C. PERFORMED TSM 26-17-00-810-804A, NO DEFECTS NOTED. OK FOR SERVICE.SDR HALA2018061100294Solenoid · failedNR 1 ENGINE SYS FAULT ILLUMINATED. PERFORMED TSM 75-32-00-810-844-A. REPLACED THE LT ENGINE ACTIVE HPC BLEED VALVE CONTROL SOLENOID IAW AMM 75-32-03-400-801-A. TEST 3 IDLE & LEAK CHECKED GOOD. OK FOR SERVICE.SDR HALA2018032000110Warning Message · false activationSTATUS MESSAGES CAT2 AND GLS AUTOLAND. POWERED DOWN AND POWERED UP THE ACFT. MESSAGES ERASED. NO FAULTS NOTED. OK TO CONTINUE.SDR HALA2018013000019Warning Message · false activationAIR SYS 2 FAULT ECAMS DURING DESCENT. PERFORMED ECAMS ACTION WITH ENG 2 BLEED OFF AND PACK 2 OFF. PERFORMED TSM 75-26-00-810-818-A. NO FAULTS NOTED. PERFORMED ALTERNATE METHOD PARA 4. NO FAULTS NOTED. OK TO CONTINUE.SDR HALA2018013000020Warning Light · false activationAIR SYS 2 FAULT DURING DESCENT. PERFORMED TSM 75-26-00-810-818A, OPERATED THE RT ENGINE AT 80% N1 IAW AMM 71-00-00-720-816-A. NO FAULTS DURING ENGINE RUN. EIU2 AND FADEC2 SHOW NO FAULTS ON LAST LEG REPORT. COULD NOT DUPLICATE ISSUE, ACFT OK FOR SERVICE.SDR HALA2018012600016Smoke Detector · false activationECAM WARNING FOR LAVATORY SMOKE DURING CRUISE ALTITUDE. F/A REPORTED IN LAVATORY D. PERFORMED TSM 26-17-00-810-804-A, LAVATORY SMOKE WARNING WITHOUT FIRE FOR LAV 'D'. ALL TEST PASSED, NO FAULTS NOTED, OK TO CONTINUE.SDR HALA2018012300009Warning System · false activationAFTER THE NR 2 ENGINE START, STATUS A/THR APPEARED 'BTB'. RESET FMGC 1& 2, PERFORMED AFS TEST IAW AMM 22-96-00 NO FAULTS NOTED. ALL TEST PASSED OK TO CONTINUE.SDR HALA2017122200312Circuit Breaker · malfunctionedON SHUTDOWN, FUEL CENTER TRANSFER FAULT AMBER XX ON RT TRANSFER PUMP. RESET CENTER RIGHT TRANSFER CIRCUIT BREAKER. OPS CHECKED NORMAL. OK FOR SERVICE.
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