Airbus A321-271N

Service difficulty reports · 1,583

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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.

SDR HALA2019050900241Relay · faultyETOPS SIGNIFICANT SYSTEM - DURING EMER GEN TEST ECAM MESSAGE ELEC AC ESS BUS FAULT ON ECAM. FOLLOWED TSM 24-50-00-810-804-A. RELAY 12XE REPLACED AS REQUIRED. OPS CHECKS GOOD. OK FOR SVC.May 9, 2019 · N215HA · Airbus A321271N · AC Power Distribution SystemSDR HALA2019050400214Smoke Warning · false activationLAV C SMOKE WARNING WENT OFF FOR SEVERAL SECONDS AND FA'S VERIFIED OPS NORMAL WITH NO SMELL. T/S PER TSM 26-16-17-00-810-812-A. OPS CKS GOOD, OK TO CONTINUE.May 1, 2019 · N208HA · Airbus A321271N · Smoke DetectionSDR HALA2019042900205Warning Light · false indicationETOPS SIGNIFICANT SYSTEM - ENG 1 OIL CHIP DETECTED ON LANDING. T/S PER TSM 79-35-00-810-808-A. NO CONTAMINATION FOUND ON CHIP DETECTORS. INSPECTED OIL FILTER, NO CONTAMINANTS FOUND. INSPECTED W03 HARNESS AND PHMU CONNECTIONS P10 AND P36 ALL LOOKS NORMAL RANApr 28, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2019042900203Warning Light · false activationETOPS SIGNIFICANT SYSTEM - ENG 1 OIL CHIP ECAM ON TAXI IN - THEN EXTINGUISHED. // INSPECTED #1 ENG CHIP DETECTOR (NOTED NO SIGNS OF CONTAMINATION) PER AMM 79-00-00-281-802-A, VISUALLY INSPECTED, #1 ENG MAIN OIL FILTER (NOTED NO CONTAMINATION), RAN #1 ENG FOR 5Apr 28, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2019042900207Pressure Switch · failedETOPS SIGNIFICANT SYSTEM - ECAM HYD BLUE ELEC PUMP LO PR CAME ON IN FLIGHT. PERFORMED ECAM ACTIONS AND PROCEED FLIGHT WITH BLUE PUMP MANUALLY OFF. // REMOVED AND REPLACED BLUE ELECTRIC PUMP PRESSURE SWITCH IAW AMM 29-12-17-000-001-A. OPS CHECK GOOD OK FOR SERVApr 27, 2019 · N209HA · Airbus A321271N · Hydraulic Pump (Electric/Engine), MainSDR HALA2019042900204Chip Detector · false indicationETOPS SIGNIFICANT SYSTEM - ECAM: ENG1 OIL CHIP DETECTED. // REMOVED AND REPLACED OIL DEBRIS SENSOR PER AMM 79-35-21-400-801-A. OPS CHECK GOOD. MESSAGE EXTINGUISHED OK FOR SERVICE.Apr 27, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2019042900202Warning Light · false activationETOPS SIGNIFICANT SYSTEM - RECALL PAGE SHOWS ENGINE 1 CHIP DETECTOR FAULT. // PERFORMED INSPECTION OF THE MAGNETIC CHIP DETECTORS AMM 79-00-00-281-802-A (NOTED NO METAL PARTICLES). VISUAL INSPECTION OF #1 ENGINE OIL FILTER AMM 79-00-00-210-809-A, RUN #1 ENGINEApr 26, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2019042500201Outflow Valve · faultedATB - VENT SKIN VALVE FAULT. // FOUND MAIN SKIN AIR OUTLET VALVE IN PARTIALLY OPEN POSITION, MANUALLY OPENED VALVE TO FULL OPEN. ACCOMPLISHED AEVC TEST TWICE, BOTH PASSED. VALVE OPS OK.Apr 24, 2019 · N208HA · Airbus A321271N · Pressure Regulator/Outflow ValveSDR HALA201904230198Engine · making metalETOPS SIGNIFICATION - UPON ENG START WHEN START SWITCH TO IGN/START, ECAM ENG 1 OIL CHP DETECT ILLUMINATED. ABORTED START, ECAM CLEARED, MX CONTROL IN HNL SAID OK TO START. NEXT START NORMAL. // PERFORMED TSM 79-35-00-810-808-A, FOUND 2 "MAGNETIC FINE" PARTICLApr 22, 2019 · N202HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2019042320197Warning Message · false activationETOPS SIGNIFICATION - ENG 1 OIL CHIP DETECTED BTB ON ENGINE ONE START. MESSAGE HAPPENED WHEN MODE SELECTOR PUT TO IGN / START. // PERFORMED TSM 79-35-00-810-808 CHIP DETECTORS CLEAN. NO ECAM MSG DISPLAYED. IDLE RUN ENGINE #1 FOR 5 MIN. NO FAULT NOTED. OK FOR SApr 20, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil SystemSDR HALA2019042320196Warning Light · false activationETOPS SIGNIFICATION - ON ENGINE START UP ENG 1 OIL CHIP DETECTED CAME UP ON ECAM AND THEN SELF CLEARED. PERFORMED TSM 79-35-00-810-808-A NO EVIDENCE OF METAL FOUND ON CHIP DETECTORS, ALSO ACCOMPLISHED ENGINE RUN OF #1 ENGINE FOR 5 MINUTES REOPENED COWLS AND Apr 19, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil SystemSDR ASAA2019041508988Valve · failedENGINE 1 FUEL RETURN VALVE. VALVE NOT CLOSE ECAM AFTER # 1 ENGINE START GROUNDED - YES. R/R FUEL RETURN VALVE ON ENG 1 REF AMM 73-11-35 OPS CHK GOOD DURING ENGINE RUN. OK FOR SVC. PLACARD REMOVED, MEL LIST UPDATED, MCC YARED NOTIFIED. THIS CLEARS MEL 73-11-01-Apr 10, 2019 · N928VA · Airbus A321271N · Fuel Controlling SystemSDR 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 HALA2019040900184Light · inoperativeR1 DOOR EMERGENCY WALL LIGHT (90WL2) INOP. // REPLACED EMERGENCY LIGHT AS REQUIRED. OPS CHECKS GOOD. OK FOR SVCApr 5, 2019 · N204HA · Airbus A321271N · Emergency LightingSDR HALA2019040500179Light · inoperativeR1 DOOR EMERGENCY WALL LIGHT (90WL2) INOP. REPLACED EMERGENCY LIGHT AS REQUIRED. OPS CHECKS GOOD. OK FOR SVC.Apr 4, 2019 · N204HA · Airbus A321271N · Emergency LightingSDR HALA2019032800150Cable · out of adjustETOPS SIGNIFICANT SYSTEM - ENG 2 REVERSER FAULT ASSERTED AFTER SELECTION OF REVERSE THRUST ON LANDING. PERFORMED OPS TEST OF ENG 2 T/R PER AMM 78-31-00-710-805-A. TROUBLESHOOT PER TSM 78-31-00-810-982-A. FOUND CLEARANCE OF INHIBIT MECHANISM OUT OF LIMIT. ADJUSMar 27, 2019 · N212HA · Airbus A321271N · Engine Thrust ReverserSDR HALA2019032500143Unknown · odorDIRTY SOCK ODOR AT 0200 Z. RAN NR 1 AND NR 2 ENGINES SEPARATELY. RAN APU WITH NR 1 AND NR 2 PACKS SEPARATELY. NO ODOR NOTED. OK FOR SERVICE.Mar 22, 2019 · N217HA · Airbus A321271N · Air Distribution SystemSDR HALA2019032500142Transducer · defectiveATB - "F/CTL ELEV SERVO FAULT" ILLUMINATED ON CLIMB OUT. PERFORMED OPS TEST OF SIDE STICK ASSY PER AMM 27-96-00-710-020-A. PERFORMED WIRING CHK OF POS RVDT MON SIGNAL FROM ELAC 1 MON PART TO FIRST TERMINAL BLOCK REF 27-93-07. SWAP ELAC 1 AND ELAC 2 NO HELP SWAMar 22, 2019 · N216HA · Airbus A321271N · Elevator Control SystemSDR HALA2019032200141Connector · dirtyETOPS SIGNIFICANT SYSTEM - UPON ARRIVAL APU AUTO SHUTDOWN, APU INOP. PERFORMED TSM 49-00-81 CLEANED CONNECTOR P19. RE-SECURED CONNECTOR P19 TO FCU PERFORMED GROUND SCAN-NO FAULTS. PERFORMED APU BITE TEST PER MEL 49-00-00 TEST PASS. APU STARTED ON FIRST ATTEMPMar 21, 2019 · N212HA · Airbus A321271N · APU System WiringSDR HALA2019031900136Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER ENGINE SHUTDOWN. ENG 2 OIL CHIP DETECTED ECAM. PERFORMED INSPECTION OF NR 2 ENGINE MAGNETIC CHIP COLLECTORS PER AMM 79-00-00-281-802-A. NO CHIPS OR FLAKES NOTED. PERFORMED NR 2 ENGINE RUN. NO FAULTS NOTED. OK FOR CONTINUED SERMar 18, 2019 · N202HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2019031200114Warning System · false activationETOPS SIGNIFICANT SYSTEM - BTB. AFTER ENGINE START, STATUS PAGE ECAM MSG. INOP SYS: A/THR CAT 3 APPEARED. PERFORMED AMM 22-96-00 & AMM 22-30-00. OPS CK OK. OK FOR SERVICE.Mar 11, 2019 · N209HA · Airbus A321271N · Auto Throttle SystemSDR HALA2019031100111Rotor · damagedATB - NR 2 ENGINE SHUTDOWN DUE TO HIGH ENGINE OIL TEMPERATURE. IAW ENGINEERING, INSPECTED NR 2 ENGINE MAGNETIC CHIP DETECTORS AND MAIN OIL FILTER. FOUND SHAVINGS ON THE (1,1.5,2) BEARING CHIP DETECTOR. IAW AMM 79-00-00-281-802A. INSPECTED NR 2 ENGINE PMA ROTOMar 10, 2019 · N212HA · Airbus A321271N · Engine (Turbine/Turboprop)SDR HALA2019031100112Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG NR 1 CHIP DETECT ON START FOR ~2-3 MINS BEFORE DISAPPEARING. INSPECTED CHIP DETECTOR AND MAIN OIL FILTER ON NR 1 ENG. NO METAL OR DEBRIS NOTED. PER TSM 79-35-00-810-808-A. RAN NR 1 ENG. NO MSG DISPLAYED. FADEC 1 GROUND REPORMar 10, 2019 · N202HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2019031200113Filter · odorOIL SMELL DETECTED AFTER TAXI IN FROM HIGH POWER RUN. PERFORMED DECONTAMINATION OF ECS PER AMM 21-00-00-615-002-A WITH APU BLEED UP TO STEP W(STAGE 2 CLEANING). ACCOMPLISHED AMM 21-00-00-615-002-A STEP W, STILL HAD OIL SMELL DETECTED, REMOVED AND REPLACED RECIMar 9, 2019 · N202HA · Airbus A321271N · Air Distribution SystemSDR HALA2019030500086Unknown · odorSTRONG ODOR IN CABIN ON POWER UP FROM IDLE DECENT @3000' MSL. ODOR LASTED 5 MIN IN BACK CABIN AND 5 SEC IN COCKPIT. PERFORMED TSM 05-50-00-810-831. RAN BOTH NR 1/2 ENGINES. RAN AND ISOLATED EACH PACK WITH EACH ENGINE AND APU. COULD NOT DUPLICATE PROBLEM. NO ODMar 4, 2019 · N202HA · Airbus A321271N · Air Distribution SystemSDR HALA2019030400083Fire Loop · faultyETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP B FAULT ILLUMINATED 3 TIMES, STAYED ON FOR 15 SEC TO 1.5 MIN. REMOVED AND REPLACED NR 1 ENGINE PYLON FIRE LOOP B IAW AMM 26-12-16-04 CONF 21. NO ECAM MESSAGES DISPLAYED, OPS TEST GOOD PER AMM 26-12-00-710-002-A. OK FOMar 4, 2019 · N202HA · Airbus A321271N · Fire DetectionSDR HALA2019030400082Warning System · false activationETOPS SIGNIFICANT SYSTEM - ECAM MESSAGE: ENG 1 FIRE LOOP B FAULT ILLUMINATED TWICE IN 5 MINUTE,1.5 HRS PRIOR TO TOD THEN OPS NORMAL. PERFORMED OPERATIONAL TEST OF ENGINE FIRE AND OVERHEAT DETECTION SYSTEMS PER AMM 26-12-00-710-002A. ALL TEST PASSED, AIRCRAFT OMar 3, 2019 · N202HA · Airbus A321271N · Fire DetectionSDR HALA2019030400081Warning System · false activationETOPS SIGNIFICANT SYSTEM - ECAM MESSAGE: ENG1 FIRE LOOP B FAULT ILLUMINATED 4 DIFFERENT TIMES WITHIN 10 MINUTES AND THEN OPS NORMAL. PERFORMED TSM 26-12-00-810-804, PERFORMED GVI OF ENG 1 LOOP B FIRE DETECTORS (4WD1)(4001WD2)(4002WD2)(41WD1)AND (42WD1). NO DEFMar 3, 2019 · N202HA · Airbus A321271N · Fire DetectionSDR HALA2019030100076Unknown · odorDESCENDING THROUGH 3,000 FT A MILD ODOR THAT SMELLED LIKE DIRTY WET SOCKS WAS OBSERVED IN THE COCKPIT AND 1L JUMPSEAT. THE ODOR WAS GONE BY 1,000 FT. PERFORMED INSPECTION OF ENG 1&2 & PACKS 1&2 PER TSM TASK 05-50-00-810-831A. NO LEAKS OR ODOR PRESENT. OK TO COFeb 28, 2019 · N202HA · Airbus A321271N · Air Distribution SystemSDR HALA2019030100077Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 1 LOOP B ECAM ILLUMINATED FOR 2-3 MINUTES THEN WENT AWAY. PERFORMED OPERATIONAL TEST IAW AMM 26-12-00, NO FAULT AND DEFECT NOTED, OK TO CONTINUE.Feb 27, 2019 · N202HA · Airbus A321271N · Fire DetectionSDR HALA2019022800074Unknown · odorSTRONG ODOR OF BURNING/MELTING PLASTIC/OIL THROUGHOUT COCKPIT LAST 15 MIN OF FLT. NO SMELL IN CABIN REPORTED. STRONGEST SMELL AT 8000FT.STRONG ODOR OF BURNING/MELTING PLASTIC/OIL THROUGHOUT COCKPIT LAST 15 MIN OF FLT. NO SMELL IN CABIN REPORTED. STRONGEST SMELFeb 27, 2019 · N202HA · Airbus A321271N · Air Distribution SystemSDR HALA2019022700072Unknown · odorFUMES/ODORS LIKE DIRTY WET SOCKS DURING DESCENT THRU 14000, ALL THE WAY TO THE GATE. // PERFORMED TSM 05-50-00-810-831-A. RAN #1 AND #2 ENGINES AND ISOLATED APU BLEED AND RAN EACH PACK INDIVIDUAL. NO ODOR NOTED IN CABIN OR COCKPIT. OK TO CONTINUE.Feb 26, 2019 · N209HA · Airbus A321271N · Air Distribution SystemSDR HALA2019022600070Unknown · odorSTRONG ODOR OF BURNING/MELTING PLASTIC THOUGHT OUT THE CABIN LAST 10 MIN OF FLIGHT.// COMPLIED WITH TSM 05-50-00-810-831-A. RAN PACK ON ENG 1 ENG 2 AND APU SEPARATELY. CONFIRMED WITH HA MAINTENANCE CONTROL. NO SMELL RE-PRODUCIBLE THRU SUGGESTED PROCEDURES.Feb 25, 2019 · N202HA · Airbus A321271N · Air Distribution SystemSDR HALA2019022600069Chip Detector · false indicationETOPS SIGNIFICANT SYSTEM - ENG 2 OIL CHIP DETECTED ECAM. // PERFORMED #2 ENG OIL CHIP DETECTOR INSPECTION PER TSM 79-35-00-810-808A. NO CHIP NOTED, RUN AND LEAKED CHK GOOD, MESSAGE ERASED OK TO CONTINUE.Feb 25, 2019 · N202HA · Airbus A321271N · Engine Oil Indicating SystemSDR HALA2019022500062Compressor · leakingSOCKS SMELL ON DESCENT OUT OF 8000' ODOR STRONGEST OVER WING INTENSIFYING AT LANDING.// CONFIRMED ODOR COMING FROM #2 ENG WITH BOTH PACKS RUNNING REF. TSM 71-00-00-810-847 ACP'D TO STEP 5. NO CONTAMINATION FOUND. NEXT STEP BORESCOPE. ACCOMPLISHED TSM 71-00-00-Feb 22, 2019 · N202HA · Airbus A321271N · Turbine Engine Compressor SectionSDR HALA2019021100055Starter · faultyATB / AFTER TAKEOFF ECAM ENG 1 START VALVE FAULT. START VALVE NOT CLOSED PERFORMED ECAM ACTIONS. REPLACED STARTER.Feb 11, 2019 · N204HA · Airbus A321271N · Engine StarterSDR HALA2019020800053Start Valve · failedAIR TURN BACK ECAM FOR ENGINE NR 1 START VALVE FAULT. SAV (STUCK) FAILED OPEN. REMOVED AND REPLACED STARTER AIR CONTROL VALVE.Feb 8, 2019 · N204HA · Airbus A321271N · Engine Start Valves/ControlsSDR HALA2019020500045Smoke Warning · false activationDURING FLIGHT LAV SMOKE WARNING, FA PANEL INDICATED LAV 1, NO SMOKE FOUND.// NO SMOKE DETECTED, NO SMOKE INDICATED. OK FOR SERVICE PER AMM26-17-01.Feb 4, 2019 · N208HA · Airbus A321271N · Smoke DetectionSDR HALA2019020400043Connector · brokenJUST BEFORE LANDING, STRONG ELECTRICAL BURNING SMELL IN THE AFT GALLEY. THE SMELL WENT AWAY AFTER LANDING. // TROUBLESHOT ELECTRICAL ODOR IN AFT GALLEY PER TSM 05-50-00-810-831-A. FOUND MOST LIKELY CAUSE TO BE MISCELLANEOUS. OPERATED ALL EQUIPMENT IN AFT GALLEFeb 3, 2019 · N209HA · Airbus A321271N · Equipment/Furnishings WiringSDR 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 HALA2019020100035Smoke Detector · false activationLAV E MOMENTARY SMOKE DETECTED ON ECAM W/ PAX INSIDE. // PERFORMED TSM 26-17-00-810-804-A. NO DEFECTS NOTED. PERFORMED OP'S TEST OF THE LAVATORY SMOKE DETECTION SYSTEM PER AMM 26-17-00. OP'S TEST GOOD. OK FOR SERVICE.Jan 31, 2019 · N217HA · Airbus A321271N · Smoke DetectionSDR HALA2019011700029Warning System · false activationSUP - MX STATUS MSG SMOKE DISPLAYED (CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY SMOKE (WITH MOD 30354 OR WITH MOD 33100). PERFORMED TSM 26-16-00-810-821-A, NO FAULTS DETECTED. MAINT STATUS "SMOKE" GJan 16, 2019 · N202HA · Airbus A321271N · Smoke DetectionSDR HALA2019011410024Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG. 1 A.ICE. PERFORMED BITE ON ENG NR 1. TEST PASSED NO FAULTS NOTED NO PREVIOUS FAULTS IN HISTORY. OK FOR SVC.Jan 11, 2019 · N212HA · Airbus A321271N · Air Intake Anti/De-Ice SystemSDR HALA2019010700008Smoke Warning · false activationMOMENTARY SMOKE LAV SMOKE ECAM IN CRUISE TWO HOURS PRIOR TO LANDING. NO SMOKE NOTED BY FAS. AND AGAIN ON HOUR PRIOR. PERFORMED LAV SMOKE BITE PER AMM 26-17-00-710-001-A. TEST PASS NO DEFECTS NOTED. OK FOR SVC.Jan 5, 2019 · N217HA · Airbus A321271N · Smoke DetectionSDR 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 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 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 System
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