N205HA

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 = 'N205HA' 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 ASAA2026021663449Safety Pin · lack of lube3R DOOR SAFETY PIN IS DIFFICULT TO REMOVE. GROUNDED - YES. CLEANED AND LUBED 3R DOOR SAFTEY PIN. OPS CHECKS GOOD. OK FOR SERVICE.Feb 16, 2026 · N205HA · Airbus A321271N · DoorsSDR HALA20251009050Filter · odorLAV SMOKE INFLIGHT. PERFORMED TSM 26-17-00-810-804-A FOUND LAV D SMOKE DET. FILTER PLUGGED. REPLACED FILTER. TEST PASSED, MESSAGE CLEARED. OK FOR SVCOct 8, 2025 · N205HA · Airbus A321271N · Air Distribution SystemSDR HALA20250724230Oil Filter · warning messageETOPS - ECAM: ENG 2 OIL SENSOR FAULT OCCURED DURING FLIGHT, NO ACTIONS GIVEN. PER TSM 79-35-00-810-808-A, INSPECTED THE MAGNETIC CHIP COLLECTORS AND WITHIN LIMITS. INSPECTED AND REPLACED MAIN OIL FILTER ELEMENT PER AMM 79-21-06-960-801-A, OPS CHECKED GOOD. IDLJul 23, 2025 · N205HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA20250721223Door · openATB - IN FLIGHT PAX OBSERVED THRUST REVERSER FLIPPER DOOR OPEN. #2 ENGINE. DEFERRAL OF #2 THRUST REVERSER FLIPPER DOOR. #2 ENG INBD AFT FLIPPER DOOR SPEED TAPED (THRUST REVERSER FLIPPER DOOR). OK FOR SERVICE.Jul 20, 2025 · N205HA · Airbus A321271N · Engine Thrust ReverserSDR HALA20250721222Pump · failedETOPS - DURING T.O. ROLL HYD Y ENG 2 PUMP LOW PRESSURE INTERMITTENT. Y LEVEL FLUCTUATING DURING TAXI. PERFORMED TSM 29-13-00-810-804-A. OPS TEST OF YELLOW HYDRAULIC SYSTEM FAILED. REMOVED AND REPLACED ENG #2 YELLOW ENGINE DRIVEN PUMP. ENGINE IDLE RUN, LEAK CHEJul 20, 2025 · N205HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR 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 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 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 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 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 HALA20250205052None · noneATB - BIRDSTRIKE @ 1500' AGL ON DEPARTURE RWY 16L. ACCOMPLISHED BIRDSTRIKE INSPECTION IAW AMM 05-51-14-200-803-A, NO DAMAGE FOUND, CLEANED FUSELAGE OF ORGANIC MATTER, A/C OK FOR CONTINUED SERVICEFeb 5, 2025 · N205HA · Airbus A321271N · Standard Practices/StructuresSDR HALA20250203044Clamp · leakingETOPS - BTB: ECAM AIR R WING LEAK. REMOVED 621BT PANEL. LOOKED FOR LEAK. SUSPECT LEAK FROM CLAMP. REMOVED AND REPLACED CLAMP PER AMM 36-11-48. LEAK CHECK OK. REINSTALLED 621BT PER AMM 57-41-37. CLAMP REF IPC 36-11-85-01 #450. AS PRECAUTIONARY REMOVED AND REPLAJan 31, 2025 · N205HA · Airbus A321271N · Airfoil Anti/De-ice SystemSDR HALA20250127036Pump · leakingETOPS - FOUND BLUE ELEC PUMP LEAKING. REMOVED AND REPLACED ELEC PUMP PER AMM 29-12-51-400-001-A OPS CHK GOOD AND LEAK CHK GOOD A/C OK FOR SVC.Jan 26, 2025 · N205HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR HALA20241210355Fire Loop · faultedETOPS - ENG 2 FIRE LOOP A FAULT. REMOVED AND REPLACED PYLON FIRE DETECTOR RAMP ASSY PER AMM 26-12-16 BITE TESTS GOOD OPS CHECK GOOD OK FOR SERVICEDec 9, 2024 · N205HA · Airbus A321271N · Fire DetectionSDR HALA20241121330Engine · odorETOPS - STRONG DIRTY SOCK SMELL DURING DESCENT. CONCENTRATION FROM ROW 46 TO COCKPIT. SMELL DISSIPATED WHEN APU BLEED WAS SELECTED. ACCOMPLISED REMOVAL AND INSTALLATION OF #2 ENG PER TASK CARD J321-72-HWI-01 AND 321-72-HWI-02 AND LEVEL C DECON PER TASK CARD E1Nov 21, 2024 · N205HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA20241118326Packing · leakingETOPS - STRONG DIRTY SOCK SMELL AT TOD IN MAIN CABIN. NO VISIBLE SMOKE. CONCENTRATION FROM ROW 46 TO COCKPIT. LASTED INTERMITTENTLY. ODOR WAS NOTICED AFT FIRST AT TOD, THEN MOVED FORWARD TO THE FORWARD FLIGHT ATTENDENT SEATS. DID NOT NOTICE SMELL IN THE FLIGHTNov 17, 2024 · N205HA · Airbus A321271N · Turbine Engine Air Inlet SectionSDR HALA20241106316Oil System · overservicedATB - DIRTY SOCK SMELL IN CABIN. UPON ARRIVAL, NO SMELL NOTED PACKS 1& 2 W/APU BLEED, FOUND #1 & #2 ENGINES OVERSERVICED. REMOVED FROM (2) QTS FROM #1 AND (1) QT FROM #2. PERFORMED #1 & #2 ENG IDLE RUN PER AMM 71-00-00. ENG OIL QTY STILL HIGH, REMOVED (1) QNov 5, 2024 · N205HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA20241101064Smoke Detector · no discrepancyRECEIVED RED "SMOKE LAVATORY SMOKE" ECAM DUE TO PAX VAPING IN LAV APPROX 90 MINS INTO FLIGHT. PERFORMED BITE OF SMOKE DETECTION SYSTEM PER AMM 26-10-00-740-801-A. NO FAULTS, OK FOR SERVICE.Oct 31, 2024 · N205HA · Airbus A321271N · Smoke DetectionSDR HALA20240920261Fadec · faultedETOPS - ON WAKE UP, FOUND ENG 2 FADEC SYS FAULT AND ENG 2 MINOR FAULT: OIL SENSOR FAULT. REMOVED AND REPLACED EEC #2 PER AMM 73-21-01-400-801-A. OPS CHECK GOOD OK FOR SERVICE. VERIFICATION FLIGHT SATISFACTORY, NO FAULTS OR WARNING UPON AIRCRAFT ARRIVAL.Sep 19, 2024 · N205HA · Airbus A321271N · Fuel Controlling SystemSDR HALA20240816227Pump · faultedETOPS - FUEL L TK PUMP 2 LO PR ECAM IN CRUISE - NO CB POPPED. REMOVED AND REPLACED LEFT WING FUEL PUMP 2 PER AMM 28-21-51. OPS CHECK GOOD, OK TO CONTINUE.Aug 15, 2024 · N205HA · Airbus A321271N · Fuel Boost PumpSDR HALA20240520136Fuel Filter · damagedETOPS - UNABLE TO REMOVE FUEL FILTER PER T/C E1128-321-73-002. RH ENG FUEL FILTER FLANGE AND BOWL DAMAGED. REMOVED AND REPLACED FUEL FILTER ASSEMBLY PER AMM 73-11-07. PERFORMED ENGINE AND LEAK CHECK, NO DEFECTS NOTED. OK FOR SERVICE.May 18, 2024 · N205HA · Airbus A321271N · Engine Fuel DistributionSDR HALA20240415019Smoke Warning · false activationINFO TO MX INFLIGHT LAV SMOKE DETECTED FA CHECKED AND NO SMOKE. INFO NOTED BY MAINTENANCE LAST LEG SHOWS NO FAULTS RAN OPS CHECK OF LAVATORY SMOKE DTECTION ALL LAVS TEST OK REF AMM 26-17-00 OK TO CONTINUE.Apr 14, 2024 · N205HA · Airbus A321271N · Smoke DetectionSDR HALA20240223008Engine · odorDIRTY SOCK SMELL ON TAKEOFF AND LANDING. T/S PER E1128-321-49-04 PERFORMED BORESCOPE OF # 1 ENGINE PER T/C E1128-321-72-019, CONFIRMED # 1 ENG CAUSE OF DIRTY SOCK SMELL. DUE TO BORESCOPE RESULTS NEED TO REMOVE #1 ENGINE, REMOVED #1 ESN: P771072 PER AMM 71-00-5Feb 22, 2024 · N205HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA20240108005Unknown · unknownATB - ENG2 COMPRESSOR VANE. PERFORMED WIRE CHECKS PER TSM 75-31-00-810-816-A STEP 4.A(4) 1 & 2 & 3. ALL CHECKS GOOD. NO SHORTS. CONTINUING TSM 75-31-00-810-816-A REMOVED AND REPLACED EEC #2 ENG IAW AMM 73-21-01. TEST OK. REMOVED AND REPLACED LPC-SVA PER AMM 75Jan 6, 2024 · N205HA · Airbus A321271N · Turbine Engine Compressor SectionSDR HALA20230905187Unknown · unknownENG 1 FIRE LOOP A FAULT INTERMTTENT DURING FLIGHT. FOUND CHAFFED WIRES (GREEN/WHITE) ON ENG #1 LOOP "A" HARNESS FIN 4165KS. REMOVED AND REPLACED LOOP "A" HARNESS 4165KS PER AMM 26-12-61. OPS CHECK AND SECURITY CHECK BOTH GOOD. CLOSED #1 ENGINE COWLS. SECURITY Sep 2, 2023 · N205HA · Airbus A321271N · Fire DetectionSDR HALA2023051200026Unknown · unknownENG 1 FIRE LOOP B FAULT ECAM MESSAGE DURING CLIMB THROUGH 10,000 FEET. MESSAGE CLEARED WITHOUT ANY ACTION AFTER ABOUT 1 MINUTE. PERFORMED INSPECTION OF ENG 1 FIRE LOOP B. NO DAMAGE NOTED. TEST OF THE FDU 1 PER AMM 26-12-00-710-002-B OK. NO FAULTS DETECTED. A/CMay 11, 2023 · N205HA · Airbus A321271N · Fire DetectionSDR HALA2023022700027Wire Harness · usedETOPS- ON CLIMBOUT "ENG 1 FIRE LOOP A FAULT, OFF & ON ECAM DURING ENTIRE FLT. FOUND INTERMITTENT ON 4036VC(BLUE) OF 4165KS. REMOVED AND REPLACED WIRE HARNESS 4165KS PER AMM 26-12-61. CONTINUITY CHECK, SHORT TO GROUND GOOD. PERFORMED FDU 1 BITETEST PER AMM 26-Feb 25, 2023 · N205HA · Airbus A321271N · Fire DetectionSDR HALA2023022400004None · noneENG 1 FIRE LOOP A FAULT ILLUMINATED BRIEFLY MULTIPLE TIMES IN CRUISE. PER TSM 26-12-00-810-912-A ALL WIRE CHECK GOOD. REMOVED AND REPLACED FDU PER AMM 26-12-34. OPS CHECK GOOD. OK FOR SERVICE.Feb 23, 2023 · N205HA · Airbus A321271N · Detection SystemSDR HALA2023012700016Pump · inoperativeETOPS - BTB: DURING TAXI OUT ECAM MESSAGE HYD ENG2 PUMP LO PR FOLLOWED ECAM ACTIONS. STATUS HYD ENG2 Y PUMP INOP. REMOVED AND REPLACED ENG 2 YELLOW HYD PUMP PER AMM 29-13-51 OPS AND LEAK CHECK GOOD OK FOR SVC.Jan 26, 2023 · N205HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR HALA2022112800302Pressure Switch · faultedETOPS- APU AUTOSHUTDOWN APPROX 5 MINUTES AFTER REACHING THE GATE. USING TSM 49-00-81-810-849-A, FOUND OIL PRESSURE SWITCH FAULTING. REMOVED AND REPLACED 8070KM & 8071KM PER AMM 49-91-14, AND CHANGED FILTER ELEMENTS PER AMM 49-91-41. OPS AND LEAK CHECKS, BOTNov 27, 2022 · N205HA · Airbus A321271N · APU Oil SystemSDR HALA2022111800006Smoke Detector · malfunctionedIN CRUISE ECAM SMOKE FWD CRG DET FAULT AND AFT CRG DET FAULT AND LAVATORY DET FAULT. FOLLOWED ECAM PROCEDURE THEN PERFORMED CIDS RESET FOR SMOKE DET FAULT WHICH CLEARED ALL FAULT MESSAGES. INFO NOTED BY MAINTENANCE PERFORMED BITE TEST PER AMM 25-17-00-710-001-Nov 17, 2022 · N205HA · Airbus A321271N · Smoke DetectionSDR HALA2022082700249None · noneETOPS - WHILE IN CRUISE WE RECIEVED THE "ENG 1 FADEC SYS FAULT" ECAM MESSAGE. REMOVED N2 SPEED TRANSDUCER PER AMM 77-11-23-000-801-A #022348. INSTALLED N2 SPEED XDUCER CONDITION WAS SAME. SWAPPED ENG 1 EEC AND ENG 2 EEC POSITION FOR T/S MSG DID NOT FOLLOW. CAug 27, 2022 · N205HA · Airbus A321271N · Engine Indicating SystemSDR HALA2022080500250None · noneETOPS - WHILE IN CRUISE WE RECIEVED THE "ENG 1 FADEC SYS FAULT" ECAM MESSAGE. REMOVED N2 SPEED TRANSDUCER PER AMM 77-11-23-000-801-A #022348. INSTALLED N2 SPEED XDUCER CONDITION WAS SAME. SWAPPED ENG 1 EEC AND ENG 2 EEC POSITION FOR T/S MSG DID NOT FOLLOW. CAug 27, 2022 · N205HA · Airbus A321271N · Engine Indicating SystemSDR HALA2022081800147None · noneETOPS - FUEL DRIPPING FROM #2 ENGINE COWLING FOUND FUEL DRIP FROM "PYLON FUEL" DRAIN MAST PORT. PERFORMED TSM 28-11-00-810-817. CHECKED FWD AND AFT PYLON DRAIN PORTS WITH ENG 2 LP FUEL VALVE OPEN AND FUEL PUMPS RUNNING, NO LEAKS NOTED. PERFORMED ENG IDLE RUAug 18, 2022 · N205HA · Airbus A300* · Powerplant SystemSDR HALA2022012500025Filter · abnormalETOPS - ENG 2 OIL CHIP DETECTED MSG ON LANDING // PERFORMED INSPECTION OF CHIP DETECTOR AND OIL FILTER ELEMENT PER TSM 79-35-00-810-808-A. CHANGED OIL FILTER PER AMM 79-21-06-960-801-A. NO DEBRIS FOUND. ENGINE RUN PERFORMED PER AMM 71-00-00, NO DEFECTS. COWLS Jan 24, 2022 · N205HA · Airbus A321271N · Engine Oil System (Airframe Furnished)SDR HALA2022011200011O-Ring · defectiveETOPS - DURING BLOCK IN NOTICE #2 ENG DRAIN MAST LEAKING FUEL FROM PYLON FUEL PORT. // REMOVED G36-5812-501 AND UNCLOGGED PYLON TUBE ASSY. FUEL LEAK STOPPED BUT FURTHER TROUBLE SHOOTING REQUIRED. 21996. 01/08/22 CONT TO LOG 861518-1. CAPPED DRAIN UNION FROM DJan 10, 2022 · N205HA · Airbus A321271N · Aircraft Fuel SystemSDR HALA2021121400187Seal · damagedETOPS - FUEL DRIP NOTED ON #2 ENGINE DRAIN MAST // PERFORMED ENGINE RUN NO LEAKS NOTED DURING ENGINE RUN. FUEL LEAK NOTED 5 MIN AFTER ENGINE SHUTDOWN FROM PYLON FUEL DRAIN INBD SIDE OF DRAINMAST. DISCONNECTED PYLON/WING JUNCTION HOSE OF PYLON FUEL DRAIN. NO LEDec 13, 2021 · N205HA · Airbus A321271N · Aircraft Fuel SystemSDR HALA2021102500142None · noneETOPS - ENG 2 OIL CHIP DETECTED ECAM AFTER LANDING // PERFORMED INSPECTION OF MAG CHIP COLLECTORS FOR OIL CONTAMINATION PER AMM 79-00-281-802-A, NO FINDINGS ALSO DID PRECAUTIONARY OIL FILTER CHANGE REF AMM72-21-00-960-281-802-A ENG RUN &LEAK CK OK #2 ENG GOOD Oct 21, 2021 · N205HA · Airbus A321271N · Engine Oil System (Airframe Furnished)SDR HALA2021091200113Fire Loop · faultedETOPS - ECAM ENG 2 FIRE LOOP A FAULT OCCURRED MULTIPLE TIMES DURING FLIGHT // REMOVED AND REPLACED ENG 2 CORE VENT LOOP A AND CORE AGB LOOP A PER AMM 26-12-17-400-802A AND AMM 26-12-17-400-803A. OPS CHECK OK. OK FOR SERVICESep 12, 2021 · N205HA · Airbus A321271N · Fire DetectionSDR HALA2021091100112Fire Loop · faultedETOPS - INFO TO MAINTENANCE: ENG 2 LOOP A FAULT // CHECKED RESISTENCE ON ENG 2 LOOP A CORE AGB AND CORE VENT FIRE LOOP. RESISTENCE CHECK OK. CLEANED AND REPLACED HARDWARE ON CORE AGB AND CORE VENT FIRE LOOP A OF ENG 2 PER AMM 26-12-17. ACCOMPLISHED #2 ENGINE ISep 11, 2021 · N205HA · Airbus A321271N · Fire DetectionSDR HALA2021091000111Fire Loop · faultedETOPS - INFO TO MAINTENANCE: ENG 2 LOOP A FAULT DURING CRUISE // PERFORMED TSM 26-12-00-810-805-A BITE TEST OF FDU 1+2 OK. PERFORMED INSP OF FIRE LOOPS AND NO PHYSICAL DAMAGES NOTED. NO FAULTS PRESENT AT THIS TIME. PER TSM R/R PYLON LOOP A ENG 2 (3WD2) IAW AMMSep 10, 2021 · N205HA · Airbus A321271N · Fire DetectionSDR HALA2021061400069Fdu · faultedETOPS - ENG 2 FIRE LOOP A ON CLIMB OUT. WENT AWAY AFTER ABOUT 5 MINUTES. REMOVED AND REPLACED FDU PER AMM 26-12-34-400-001-A OPS CHECK GOOD OK FOR SERVICE.Jun 13, 2021 · N205HA · Airbus A321271N · Fire DetectionSDR HALA2021060900065Detection Sys · malfunctionedETOPS - ENG 2 FIRE LOOP B FAULT INTERMITTENT ON CLIMB OUT. PER PFR SHOWS ENG 2 FIRE LOOP A + B AGC FAIL, PERFORMED 26-12-00-810-894-A. ALL WIRING CK INSULATION CK OK ON BOTH LOOP A AND B. RESISTANCE CK WITHIN LIMIT. VISUAL CK OK. REMOVED AND REPLACED #2 FDU PEJun 8, 2021 · N205HA · Airbus A321271N · Fire DetectionSDR HALA2021060700083Fire Loop · faultedETOPS - BTB ENG 2 FIRE LOOP A FAULT ALERT ILLUMINATED ON TAXI OUT, REPLACED ENG 2 AGB LOOP A PER AMM 26-12-17-400-802-A. OPS TEST OK. OK FOR SVC.Jun 5, 2021 · N205HA · Airbus A321271N · Fire DetectionSDR HALA2020111600206Lanyard · inoperativeEMER EQUIPMENT 2L DOOR SAFETY PIN TETHER IS INOPERABLE. REATTACHED TETHER, OK FOR SERVICE.Nov 14, 2020 · N205HA · Airbus A321271N · Emergency EquipmentSDR HALA2020081100171Priority Valve · not reportedETOPS SIGNIFICANT SYSTEM. ENG 1 BLEED ABN PR RESET CB'S PER MAINTENANCE "AIR PACK 1 REGUL FAULT" ISSUE PERSISTED. PFR INDICATED PRV 1 FAULTING. INSPECTED VALVE & FOUND DIFFICULT TO OPERATE BY HAND. REMOVED & REPLACED PRV 1 PER AMM 36-11-52. LEAK CHE3CK OK. OAug 9, 2020 · N205HA · Airbus A321271N · Pneumatic Distribution SystemSDR 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,#1Aug 9, 2020 · N205HA · Airbus A321271N · Engine Bleed Air SystemSDR HALA2019020100037Smoke Detector · false activationECAM MOMENTARILY DISPLAYED "SMOKE LAVATORY SMOKE". FAS INSPECTED LAD D. NO SMOKE OR DEFECTS WERE OBSERVED. // PERFORMED OPERATIONAL CHECK OF LAVATORY SMOKE DEFECTOR SYSTEM PER AMM 26-17-00-710-00104 NO FAULTS NOTED.Jan 31, 2019 · N205HA · Airbus A321271N · Smoke DetectionSDR 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 Aug 20, 2018 · N205HA · Airbus A321271N · Air Distribution SystemSDR 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.Aug 20, 2018 · N205HA · Airbus A321271N · Turbine Engine Oil System
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