N214HA

Service difficulty reports · 75

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N214HA' AND registry_match = 'registration'
  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 HALA2021071800076Altimeter · stuckETOPS - F/O EFIS CONTROL PANEL ALTIMETER STUCK IN STANDARD// REMOVED AND REPLACED FCU PER AMM 22-81-12. OPS CHECK GOOD. PENDING LAND CAT 3 CAPABILITY TEST. AFS BITE TEST AND LAND CAT 3 CAPABILITY TEST PASSED.Jul 18, 2021 · N214HA · Airbus A321271N · Altimeter, Barometric/EncoderSDR 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.Mar 10, 2020 · N214HA · Airbus A321271N · Engine Oil PressureSDR 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.Mar 3, 2020 · N214HA · Airbus A321271N · Autopilot SystemSDR 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.Dec 3, 2019 · N214HA · Airbus A321271N · Escape SlideSDR 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 SNov 3, 2019 · N214HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR 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 SERVICENov 3, 2019 · N214HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR 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.Oct 30, 2019 · N214HA · Airbus A321271N · Aircraft Fuel Filter/StrainerSDR HALA2019070900351Unknown · malfunctionedETOPS SIGNIFICANT SYSTEM - AUTO LAND UNSAT, AP DISCONNECTED AT 75'. PERFORMED OPERATIONAL TEST OF THE AFS PER AMM 22-96-00-710-001-A AND OPERATIONAL TEST OF THE LAND CAT III CAPABILITY PER AMM 22-97-00-710-001-A. BOTH TEST OK TO CONTINUE.Jul 8, 2019 · N214HA · Airbus A321271N · Autopilot SystemSDR HALA2019053100269Warning System · false activationETOPS SIGNIFICANT SYSTEM - ECAM AIR ENG 1 BLEED ABNORMAL PR COMPLIED WITH ECAM PACK 1 OFF. PERFORMED BITE TEST IAW AMM 36-11-00. TEST OK.May 30, 2019 · N214HA · Airbus A321271N · Pneumatic Indicating SystemSDR HALA2019051500245Warning System · false activationETOPS SIGNIFICANT SYSTEM - DURING DESCENT ECAM MESSAGE AIR ENG 1 BLEED ABNORMAL PR ECAM ACTIONS COMPLETED PACK 1 OFF. PERFORMED RESET AND BITE TEST OF BMC 1 AND 2 IAW AMM 36-11-00 NO FAULTS NOTED. OK FOR SERVICE.May 13, 2019 · N214HA · Airbus A321271N · Pneumatic Indicating SystemSDR HALA2019011100023Motor · malfunctioned-ATB- F/CTL ELAC 2 PITCH FAULT UNABLE TO RESET. REPLACED RELAY-PITCH ACT MOTOR 1 SUPPLY(36CE1) PER TSM 27-93-00-810-836A. CONDITION SAME. PERFORMED ALL WIRING CHECKS PER TSM 27-93-00-810-836-A.(7). CONTINUITY AND INSULATION CHECKS GOOD. PERFORMED THS - ACTUATOJan 10, 2019 · N214HA · Airbus A330243 · Elevator Tab Control SystemSDR HALA2018122740679Switch · closedETOPS SIGNIFICANT SYSTEM - APU AUTO SHUTDOWN ON GROUND.// PERFORMED APU BITE CHECK. FAULT CODE 499141 & 499114. PERFORMED TSM TASK 49-00-81-810-849-A. MINUTE PARTICLES FOUND IN GEN SCAV FILTER. REMOVED AND REPLACED APU GEN PER AMM 24-23-51. CONDITION SAME. PERDec 26, 2018 · N214HA · Airbus A321271N · AC Generator-AlternatorSDR HALA2018121000638Smoke Warning · noneINTERMITTENT (3 SECONDS) LAV SMOKE INDICATION ON ECAM. (SUSPECT PASSENGER VAPING - COULD NOT CONFIRM.// INSPECTED DETECTOR,OK PERFORMED GROUND SCAN NO FAULTS. ACP LAV SMOKE TEST PER 26-14-00-710-001. TEST OK.Dec 8, 2018 · N214HA · Airbus A321271N · Smoke DetectionSDR HALA2018112760613Warning Light · false activationETOPS SIGNIFICANT SYSTEM - BTB ENG 1 OIL CHIP DETECTED. DURING ENG START.// PERFORMED TSM 79-35-00-810-806-A FOR RELATED GROUND REPORT ENG1A-0571- LOSS OF ODM. PERFORMED TSM 77-31-00-810-807-A FOR RELATED GROUND REPORT ENG1D-0730 PHMU INTERNAL SNSR INTERFACE. Nov 22, 2018 · N214HA · Airbus A321271N · Central WarningSDR HALA2018112000604Warning Light · false activationETOPS SIGNIFICANT SYSTEM - UPON ENGINE START ENG 1 OIL CHIP DETECTED ECAM DISPLAYED.// INSPECTED ALL CHIP DETECTORS PER AMM 79-00-00-281-802-A. ALL CHECK OK. RAN #1 ENGINE AND NO ECAM MESSAGES, NO LEAKS NOTED. OK FOR SVC.Nov 19, 2018 · N214HA · Airbus A321271N · Central WarningSDR HALA2018111300579Warning Light · false activationETOPS / ECAM UPON # 2 ENGINE START ENG 1 OIL CHIP DETECTED (BTB)// INSPECTED #1 ENGINE CHIP DETECTORS (ALL)PER AMM 79-00-00-281-802. A .WITH NO FAULTS NOTED. RAN # 1 ENG AND NO MESSAGES. NO LEAKS NOTED. OK FOR SVCNov 13, 2018 · N214HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2018110700570Warning Message · false activationETOPS SIGNIFICANT SYSTEM - DURING PREFLIGHT - ECAM ENG 1 OIL CHIP DETECTED- DISPLAYED.// INSPECTED ALL CHIP DETECTORS WITH NO FINDINGS. IDLE RAN ENGINE AND NO MESSGAE. OK FOR SERVICE.Nov 6, 2018 · N214HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2018110100556Warning Message · false activationDURING NR 2 ENGINE START, ECAM FOR NR 1 ENGINE OIL CHIP DETECTOR. DURING NR 2 ENGINE CRANKING, MESSAGE DISAPPEARED. STARTED NR 1 ENGINE, ALL INDICATIONS NORMAL.. PERFORMED TSM 79-35-00-810-808-A, NR 1 ENGINE OIL CHIP DETECTOR ECAM REPORTED BY CREW WITH Oct 31, 2018 · N214HA · Airbus A321271N · Central WarningSDR HALA2018101900529Fire Loop · faultyETOPS SIGNIFICANT SYSTEM - UPON AIRCRAFT POWER UP FIRE DET ENG 1 AGB ON ECAM. REMOVED AND REPLACED ENG 1 AGB FIRE LOOP PER AMM 26-12-17-000-802 AND AMM 26-12-17-400-802.Oct 18, 2018 · N214HA · Airbus A321271N · Fire DetectionSDR HALA2018101600501Nose Cowl · dentedOPEN - DURING NR 1 ENG BIRD STRIKE INSPECTION FOUND DENT ON NOSE COWL LIP AT APPROX 2 O'CLOCK POSITION. FWD LOOKING AFT. REPAIR IN WORK.Oct 14, 2018 · N214HA · Airbus A321271N · Engine Cowling SystemSDR 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 DEOct 3, 2018 · N214HA · Airbus A321271N · Engine Oil Indicating SystemSDR 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.Sep 15, 2018 · N214HA · Airbus A321271N · Turbine Engine Oil SystemSDR 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 PERFORMSep 15, 2018 · N214HA · Airbus A321271N · Global Positioning SystemSDR HALA201809170422Carbon Seal · failedNR 2 ENGINE OIL CHIP DETECTOR ACTIVATED. FOUND AFT CARBON SEAL BAD. REMOVE AND REPLACED THE NR 2 ENGINE.Sep 15, 2018 · N214HA · Airbus A321271N · Turbine Engine Oil SystemSDR 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 TAug 13, 2018 · N214HA · Airbus A321271N · Turbine Engine Oil System
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