N213HA

Service difficulty reports · 53

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 = 'N213HA' 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 ASAA2026081466337Smoke Detector · no discrepancyINFO TO MX: SMOKE LAVATORY SMOKE ECAM DURING CRUISE, F/A REPORTS PAX VAPING IN MID CABIN LAC ON A/C L SIDE. NO VISABLE DAMAGE. GROUNDED - YES. INFO NOTED BY MX. OPS CHECK OK PER AMM 26-17-00. A/C OK FOR SERVICE.Aug 14, 2026 · N213HA · Airbus A321271NX · Fire DetectionSDR ASAA2026050364573Epsu · failedEPSU SYS TEST: EPSU 11WL FAIL. GROUNDED - YES. REMOVED & REPLACED EPSU 11WL. OPS CHECK PASS. REFERENCE AMM 33-51-00.May 3, 2026 · N213HA · Airbus A321271N · Emergency LightingSDR HALA20251002297Fire Loop · faultedETOPS - FIRE LOOP A CORE ECAM MESSAGE. REPLACED FIRELOOP A CORE PER AMM 26-12-17. OPS CHECK NOT GOOD. REPLACED LOOP A FIRE LOOP HARNESS PER AMM 26-12-61. OPS CHECK NOT GOOD. REMOVED AND REPLACED FIRE LOOP CORE LOOP B PER AMM 26-12-17. OPS CHECK IS GOOD. OKAY TOct 1, 2025 · N213HA · Airbus A321271N · Fire DetectionSDR HALA20250929291Pressure Switch · faultedETOPS - APU AUTO SHUTDOWN. REMOVED & REPLACED. ECB & OIL PRESSURE SW PER AMM 49-61-34 & AMM 49-91-14. OPS + LEAK CK GOOD. OK FOR SVCSep 27, 2025 · N213HA · Airbus A321271N · APU Oil SystemSDR HALA20250620187Sdu · leakingETOPS - DIRTY SOCK SMELL DECSENDING THROUGH 6,000' - 3,000'. DURATION APPROXIMATELY 10 MIN. PUSHED DFDR EVENT BUTTON. FOUND OIL STREAKS COMING FROM #1 ENG INLET CONE WEEP HOLES AND OIL PUDDLING INSIDE OF #1 ENG INLET CONE. REPLACED THE FAN SHAFT COVER SEAL PE Jun 18, 2025 · N213HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA20250617184Sensor · faultedETOPS - ON DECENT AS THRUST WENT TO IDLE "ENG 1 SENSOR FAULT". REMOVED BURNER PRESSURE SENSOR AND BURNER PRESSURE SENSOR TUBE IN REFERENCE TO AMM 73-21-23-000-801-A AND 73-21-23-000-802A K.H. 25197 06/15/2025. INSTALLED BURNER PRESSURE AND LINE PER AMM 73-21-2Jun 16, 2025 · N213HA · Airbus A321271N · Engine Indicating SystemSDR 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 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 HALA20250124031Wire Harness · damagedETOPS - FOUND 440VT2 TERMINAL BLOCK & WIRE 704001-000W24-22 DAMAGED WHILE TROUBLESHOOTING REPEAT GEN 2 FAULT. REMOVED AND REPLACED 440VT2 TERMINAL BLOCK AND WIRE 704001-000W24-22. PER AMM 24-21-61 AND AMM 24-92-00. OPS CHECK OKAY. OK FOR SVC. OSD: 1/24/2025Jan 22, 2025 · N213HA · Airbus A321271N · Electrical Power System WiringSDR HALA20250110015Bleed Valve · damagedETOPS - WHILE PERFORMING ASSIGNED BOROSCOPE TASK CARDS, FOUND BLEED PRESSURE REGULATING VALVE DAMAGED. REMOVED AND REPLACED BLEED PRESSURE REGULATING VALVE IAW A321 AMM 36-11-52. LEAK CHECK OK. ENGINE IDLE RUN PERFORMED. A/C OK FOR SERVICE.Jan 9, 2025 · N213HA · Airbus A321271N · Compressor Bleed ValveSDR HALA20240816228Sensor · faultedETOPS - CLASS 2 TEMP CONTROL MESSAGE FOUND ON STATUS PAGE. REMOVED AND REPLACED PACK 1 INLET SENSOR PER AMM 21-51-13-400-001-A. OPS CHECK GOOD, OK FOR SERVICEAug 15, 2024 · N213HA · Airbus A321271N · Cabin Cooling SystemSDR HALA20240319070Shuttle Valve · faultedETOPS - ENG1 OIL SYSTEM FAULT ON ECAM AFTER SHUTDOWN AT GATE. PERFROMED TSM 79-33-00810840A- NO DECTS NOTED REPLACED SHUTTLE VLV PER AMM 79-21-15-000-801A- REPLACED MAIN OIL PRESS OIL SENSOR PER AMM 79-33-21-400-801 SWAPPED #1 AND #2 PHMU TO ASSIT TROUBLESHOOTMar 18, 2024 · N213HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA20230908193Unknown · faultyETOPS - ON PDC FOUND ECAM MESSAGE ENG 1 FUEL VALVE FAULT FUEL VALVE NOT OPEN AND ENG 1 FADEC IDENT FAULT. PERFORMED TSM 77-31-00-810-801A FOUND #1 PHMU FAIL MESSAGE. REPLACED #1 PHMU PER AMM TASK 77-31-400-801A, RAN ENG NO FAULTS NOTED, OK TO CONTINUE.Sep 7, 2023 · N213HA · Airbus A321271N · Engine Indicating SystemSDR HALA20230906191Unknown · unknownETOPS - ON ENG START UP FOUND ENG 2 FADEC FAULT ON ECAM. N2 SPEED VIB INDICATION HAD AMBER X'S. REPLACED EEC PER AMM 73-21-01-400-801-A & AMM 73-21-01-400-801-A. OPS CHECK IS GOOD. OK TO CONTINUE.Sep 5, 2023 · N213HA · Airbus A321271N · Fuel Controlling SystemSDR HALA2023083100184Unknown · unknownETOPS - ENG2 FADEC SYS FAULT ECAM ILLUMIANTED FOR 5 SECONDS AND CLEARED. PERFORMED TSM 77-11-00-818-811-A TO (3) (D), CHECKED CONTINUITY AT WIRE HARNESS WO4, P63 AND P3. PINS Y-4,1,5. CONTINUITY CHECKED GOOD. SWAPPED PHMU 1+2 CONDITION SAME. RETURNED PHU 1+2 TAug 29, 2023 · N213HA · Airbus A321271N · Engine Fuel and ControlSDR HALA2023082800179Unknown · unknownETOPS - ENG 2 FADEC SYS FAULT ON ENGINE START. ATTEMPTED ENGINE START BY MAINT DIRECTION. NORMAL ENGINE START. FAULT CLEARED WHEN AVAIL APPEARED. REMOVED & REPLACED #2 ENG EEC PER AMM 73-21-01. OPS CHECK GOOD. RAN #2 ENG IDLE. NO FAULTS NOTED OK TO CONTINUAug 27, 2023 · N213HA · Airbus A321271N · Fuel Controlling SystemSDR HALA2023082500178Unknown · faultyETOPS - ENG 2 FADEC SYS FAULT CODE 733101. REPLACED #2 PHMU PER AMM 77-31-01 NO FAULTS NOTED ENG RUN GOOD OK FOR SERVICAug 24, 2023 · N213HA · Airbus A321271N · Engine Indicating SystemSDR HALA2023080400167Igniter · faultyETOPS - DURING BOROSCOPE INSPECTION FOUND #2 IGNITER WORN. REMOVED AND REPLACED IGNITER PER AMM 74-21-01. OPS CHK GOOD. A/C OK FOR SVC.Aug 3, 2023 · N213HA · Airbus A321271N · Spark Plug/IgniterSDR HALA2023071700144Unknown · unknownETOPS - APU AUTO SHUT DOWN ON ARRIVAL, ATEMPTED 3 STARTS UNSUCCESSFULLY. REMOVED AND REPLACED APU IGNITION EXCITER UNIT PER AMM 49-41-38. OPS CHECK GOOD NO FAULTS DETECTED.Jul 15, 2023 · N213HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) SystemSDR HALA2023062000129Unknown · unknownETOPS - SKIN INLET FAULT. INITIALLY OVRD FOR BOTH INLET/EXHAUST EXTINGUISHED THE ECAM. DESCENDING THROUGH 13,000 FT, ECAM REOCCURED AND FORCED INTO MANUAL MODE TO DEPRESSURIZED TO SL. REMOVED AND REPLACED SKIN OUTLET VALVE PER AMM 21-26-53. REF DMI 207107 FJun 18, 2023 · N213HA · Airbus A321271N · Air Conditioning SystemSDR HALA2023061600128Unknown · unknownETOPS - INFO TO MX INFLIGHT ENG2 FIRE LOOP A FAULT ECAM. THE ECAM WENT AWAY AFTER 2 MINUTES. REPLACED ENG2 FIRE LOOP A HARNESS FIN 4165KS PER AMM 26-11-61. OPS CHECK OK. NO FAULTS NOTED. SECURITY CHECK GOOD OK FOR SERVICE.Jun 16, 2023 · N213HA · Airbus A321271N · Smoke DetectionSDR HALA2023061200123Unknown · unknownETOPS - DURING #1 ENGINE CHANGE FOUND DAMAGED FIRE DETECTOR HARNESS. REMOVED AND REPLACED FIRE DETECTOR HARNESS PER AMM 26-12-16. CHECK IS GOOD NO DEFECTS NOTED OK TO CONTUNE SERVICE.Jun 11, 2023 · N213HA · Airbus A321271N · Fire Protection SystemSDR HALA2023041200017Unknown · unknownMOMENTARY LAV SMOKE ECAM DURING CRUISE. PERFORMED SYS RESET AND INSPECTED IAW AMM 26-17-00. NO FAULTS FOUND, A/C GOOD FOR SERVICE.Apr 11, 2023 · N213HA · Airbus A321271N · Fire Protection SystemSDR HALA2022123000015Slide · unwanted deploySLIDE AT R1 DOOR ACCIDENTALLY DEPLOYED. R & R THE R1 DOOR DAMPER DIAPHRAM IAW AMM 52-11-14. NO LEAKS NOTED. R & R R1 DOOR ESCAPE SLIDE IAW AMM 25-62-44. INDICATIONS OK. OPS CHECKED OK. OK FOR SERVICE.Dec 29, 2022 · N213HA · Airbus A321271N · Escape SlideSDR HALA2022120200305Radar · faultedETOPS - WX RADAR GCS (GROUND CLUSTER SWITCH) IS BROKEN ( WEATHER RADAR SYSTEMS GROUND CLUTTER SUPPRESSION). REMOVED AND REPLACED WEATHER RADAR CTL UNIT AND BITE TEST OK IAW AMM 34-41-12 PB 401.Dec 1, 2022 · N213HA · Airbus A321271N · Weather Radar SystemSDR HALA2022101100270None · noneBTB - ENG 1 FIRE LOOP A FAULT, 5TH WRITE FROM 9-29-2022. FOUND WIRE 708003-20R26-12 SHORTED TO GROUND. REMOVED AND REPLACED HARNESS 4165KS PER AMM 71-51-75, OPS CHECK GOOD PER AMM 26-12-00. PLACARDS REMOVED & MIC SHEET CLEARED.Oct 7, 2022 · N213HA · Airbus A321271N · Fire DetectionSDR HALA2022061500113None · noneDESCENDING THOUGHT 5,000' - 3,000 ' ENGINE AT IDLE EXPERIENCE DIRTY SHOCK SMELL AGAIN // FOUND EVIDANCE OF OIL LEAK ON #1 ENG AT 9 O CHOCK POSITION IN THE FIC REPLACED SEAL FROM LP62 OIL PRESSURE TUBE REF AMM PW 10006-C-72-00-30-00A-702A-B LEAK CHECK GOOD 1843Jun 14, 2022 · N213HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2022011300014Switch · inoperativeETOPS - RAT FAULT DURING RAT EXTENSION AND STOWAGE TEST // REMOVED AND REPLACED RAT ACTUATOR PRESSURE SWITCH REF AMM 29-22-53-400-013-A. OPS CHECK AND LEAK CHECK GOOD.Jan 12, 2022 · N213HA · Airbus A321271N · Hydraulic Power SystemSDR HALA2021110500153Connector · damagedETOPS - ENG 1 FIRELOOP A FAULT CAME ON SHORTLY AFTER T/O. FOUND STUD C CONNECTOR OF ENG 1 LOOP A COMMON FWD DETECTOR CABLE BROKEN. REMOVED AND REPLACED (4181KS) PER AMM 26-12-61. ALSO PER MOC AS PRECAUTIONARY REMOVED & REPLACED #1 LOOP A AGB PER AMM 26-12-17Nov 3, 2021 · N213HA · Airbus A321271N · Fire Protection System WiringSDR HALA2021102800147Wire Harness · chafedETOPS - ENG 2 FIRE LOOP A FAULT. RESISTANCE CHECK AT PIN J - K AT FDU 2 (2WD2) CONNECTOR A. FOUND 1.49K OHMS. RESISTANCE GOOD WITH TAPPING DETECTORS. NO FAULT NOTED. NO SHORT TO GND. INSULATION TEST OK. DURING T/S FOUND CHAFED WIRE ON 4165KS HARNESS. REPLACEDOct 27, 2021 · N213HA · Airbus A321271N · Fire Protection System WiringSDR HALA2021061500072Gcu · faultedETOPS - ATB - ELECT GEN 2 FAULT//REMOVED AND REPLACED GCU 2 IAW AMM 24-22-34. BITE TEST OK. PERFORMED ENGINE 2 RUN UP. OPS TEST GEN 2 NORMAL. NO FAULLTS NOTED.Jun 15, 2021 · N213HA · Airbus A321271N · AC Generator-AlternatorSDR HALA2021012500010Gcu · defectiveETOPS ECAM MX STATUS "AC GEN". REMOVED & REPLACED NR 1 GCU, PER AMM 24-22-34. MX STATUS CLEARED, OK FOR SERVICE.Jan 22, 2021 · N213HA · Airbus A321271N · AC Generator-AlternatorSDR HALA2020091430181Blade · damagedNR 4 FAN BLADE ON NR 2 ENGINE S/N JB1AEA4305 MISSING POLYURETHANE COAT. REMOVED AND REPLACED NR 4 FAN BLADE, PER AMM 72-11-03-400-801-A. FUNCTIONAL TEST FAN TRIM BALANCE AMM TASK 71-00-00-710-807-A PENDING. PERFORMED FUNCTION TEST (FAN TRIM BALANCE), PER AMSep 13, 2020 · N213HA · Airbus A321271N · Turbine Engine Air Inlet SectionSDR 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 CHEAug 3, 2020 · N213HA · Airbus A321271N · Compressor Bleed ValveSDR 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.Nov 13, 2019 · N213HA · Airbus A321271N · Standard Practices/StructuresSDR HALA2019090300358Smoke Detector · false activationSMOKE AFT LAV ECAM WARNING ILLUMINATED MOMENTARILY NEAR TOP OF DESCENT. SUSPECTED VAPING NOTHING CONFIRMED. FLT ATTENDANT WITNESSED PASSENGER ENTER AFT LAV WITH VAPE PEN. OPS CHECKED DETECTOR - NO DEFECTS FOUND. OK FOR CONTINUED SVC.Sep 1, 2019 · N213HA · Airbus A321271N · Smoke DetectionSDR HALA2019041100185Warning Message · false indicationETOPS SIGNIFICANT SYSTEM - ENG 2 AIR SYSTEM FAULT ON APPROACH. // PERFORMED BITE TEST ON EEC 1 & 2, NO FAULTS NOTED. DID A HISTORY SEARCH ON THIS FAULT AND NONE WERE FOUND PREVIOUS OF THIS ONE. WILL CONTINUE MONITORING AS REQUIRED PER TSM 75-26-00-810-819-A. Apr 10, 2019 · N213HA · Airbus A321271N · Engine Cooling SystemSDR HALA2019010200003Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER 30S ON IGN/START,#2ENG OIL CHIP DETECTION ON ECAM. CLEARED AFTER 5 SECONDS, NO FURTHER INDICATIONS.//INSPECTED MAGNETIC CHIP DETECTORS PER AMM 75-00-00-281-802-A NO CHIP DETECTED. OK TO CONTINUE.Jan 1, 2019 · N213HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2018123100693Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER 30S ON IGN/START, NR 2 ENG OIL CHIP DETECTION ON ECAM. CLEARED AFTER 5 SECONDS, NO FURTHER INDICATIONS. INSPECTED MAGNETIC CHIP DETECTORS PER AMM 75-00-00-281-802-A NO CHIP DETECTED. OK TO CONTINUE.Jan 1, 2019 · N213HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2018123100692Warning System · false activationSUP - ETOPS SIGNIFICANT SYSTEM - NR 2 ENG OIL CHIP DETECTION ECAM WHEN IGN/START SELECTED. EXTINGUISHED AFTER 30 SECONDS. NO FURTHER INDICATIONS. CHECKED MAGNETIC CHIP DETECTORS PER AMM 79-00-00-281-802-A - NO CHIPS DETECTED - OK TO CONTINUE.Dec 31, 2018 · N213HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2018123100690Warning System · false activationETOPS SIGNIFICANT SYSTEM - NR 2 ENG OIL CHIP DETECTOR ECAM WHEN IGN/START SELECTED. EXTINGUISHED AFTER 1 MINUTE. NO FURTHER INDICATIONS. PERFORMED AMM TASK 79-00-00-281-802-A. CHECKED CHIP DETECTOR-NO CONTAMINANTS FOUND. RAN NR 2 ENG- NO ECAM MESSAGE ASSOCIATDec 28, 2018 · N213HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2018122400677Warning Light · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 OIL CHIP DETECTED WHILE ATTEMPTING TO START ENGINE #2.// PERFORMED CHIP DETECTOR INSP PER TSM 79-00-00-281-802A. NO FAULTS FOUND. CLOSED COWLS. RAN ENGINE, NO ECAM MESSAGE NOTED.Dec 22, 2018 · N213HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2018111400580Warning Message · false activationETOPS SIGNIFICANT SYSTEM - UPON PLACING ENGINE MODE SELECTOR TO IGN/START, ENG 2 OIL CHIP DETECTED ECAM DISPLAYED. MAINTENANCE ADVISED TO START ENG 2, ENG HAD A NORMAL START AND CAM DISAPPEARED WHEN ENG 2 MASTER SWITCH WAS PLACED TO ON.// PERFORMED AMM 79-00-0Nov 13, 2018 · N213HA · Airbus A321271N · Central WarningSDR HALA2018111400579Warning Light · false activationETOPS SIGNIFICANT SYSTEM - UPON PLACING ENGINE MODE SELECTOR TO IGN/START, ENG 2 OIL CHIP DETECTED ECAM DISPLAYED. MAINTENANCE ADVISED TO START ENG 2, ENG HAD A NORMAL START AND CAM DISAPPEARED WHEN ENG 2 MASTER SWITCH WAS PLACED TO ON.// PERFORMED AMM 79-00-0Nov 13, 2018 · N213HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2018110700571Warning Message · false activationETOPS SIGNIFICANT SYSTEM - DURING PREFLIGHT - ECAM ENG 2 BOWED ROTOR PROTECTION FAULT DISPLAYED. // PERFORMED EEC SYSTEM TEST PER AMM 73-21-00. TEST OK. PERFORMED EEC RESET TO CONFIRM IF ACTUAL FAULT. MESSAGE CLEARED. CONTACT PRATT & WHITNEY REP. PERFORMED IDNov 6, 2018 · N213HA · Airbus A321271N · Engine Indicating SystemSDR HALA2018102300537Unknown · odorSTRONG ODOR CIRCULATED THROUGHOUT ENTIRE AIRCRAFT DURING DESCENT FROM FL200 DOWN TO THE SURFACE, SMELLED LIKE DIRTY SOCKS & CHEMICALS. NOTICED SMELL IN CABIN UPON ENTRY TO AIRCRAFT. ISOLATED EACH BLEED SYSTEM AND OPERATED PACKS ON FULL HOT/ FULL COLD. SMELL DOct 22, 2018 · N213HA · Airbus A321271N · Air Distribution SystemSDR HALA2018102300538Bearing · failedETOPS SIGNIFICANT SYSTEM - IN CRUISE, ECAM MASTER WARNING AIR-BLEED LEAK. FOLLOWED ECAM PROCEDURE AND ECAM CLEARED. REMAINING ECAM: AIR ENG 1 AND 2 BLEED FAULT RIGHT COND HOT AIR FAULT, ENG 1 OIL CHP DETECTED. SMOKE SMELL DETECTED AFTER ENGINE NR 1 START// BOROct 21, 2018 · N213HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2018101500496Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER LANDING ENG 1 OIL CHIP DETECTED. PERFORMED ENG 1 OIL CHIP DETECTORS INSPECTION PER AMM 79-00-00 281-802-A. NO DEBRIS FOUND INSPECTED AND REPLACED ENG 1 OIL FILTER PER 79-21-06-960-801-A. ENG 1 RUN OK.Oct 13, 2018 · N213HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2018101500495Duct · contaminatedBTB SMOKE SMELL DETECTED AFTER ENGINE NR 1 START. FOUND OIL INTERMEDIATE PRESSURE DUCTING ON ENG NR 1.Oct 13, 2018 · N213HA · Airbus A321271N · Pneumatic Distribution SystemSDR HALA2018101000486Igniter · faultedETOPS SIGNIFICANT SYSTEM - BTB ENG 2 IGN A FAULT. REMOVED AND REPLACED ENG 2 IGN A PER AMM 74-21-01, IGNITER TEST GOOD ON CH A+B. OK FOR SVC.Oct 9, 2018 · N213HA · Airbus A321271N · Spark Plug/Igniter
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