IAE V2524-A5

Service difficulty reports · 893

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 engine_model_key = 'V2524A5'
  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 AALA2020091429013Valve · defectiveAIRCRAFT WAS GROUNDED: ON TAKEOFF AT 1500 THE ECAM ENG2 BEARING 4 OIL SYS (PRESS HI) CAME ON FOR ABOUT TWO MINUTES, THEN WENT OUT. THE AIRCRAFT RETURNED TO DFW, WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. REPLACED NR 2 ENGINESep 11, 2020 · N812AW · Airbus A319132 · Turbine Engine Oil SystemSDR GTIA2020072735279Oil System · lowENROUTE WE HAD AN ADVISORY ON ECAM WARNING US OF LOW OIL LEVEL IT DROPPED TO 2.5 QTS ( OIL QUANTITY INDICATIONS )--Jul 26, 2020 · N524NK · Airbus A319132 · Turbine Engine Oil SystemSDR AALA202007279014Eec · inoperativeAIRCRAFT WAS GROUNDED: ON SHORT FINAL AUTOTHROTTLE OFF ECAM: #1 ENGGINE WENT TO IDLE #2 ENIGINE ENTERED THRUST LOCK: AUTOTHROTTLE DISCONNECTED, ENGINES RETURNED TO NORMAL OPERATION. REPLACED NR 2 EEC2 IAW AMM 73-22-34. GROUND OPERATIONAL CHECKED SATISFACTORY Jul 26, 2020 · N809AW · Airbus A319132 · Fuel Controlling SystemSDR AALA2020060429019Pin · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION AFT ENGINE MOUNT INNER PIN UPPER POSITION INBOARD SIDE ON ENGINE 1. REPLACED AFT ENGINE MOUNT INNER PIN PER CMM 71-22-11.May 31, 2020 · N828AW · Airbus A319132 · Engine Mount SectionSDR AALA202004219017Engine · power lossAIRCRAFT WAS GROUNDED: ON TAKEOFF, WHEN THRUST LEVERS WERE PLACED IN FLEX DETENT, THERE WAS A SIGNIFICANT DIFFERENCE IN ENGINE EPR. #1 EPR, WE BELIEVE ACHIEVED APPROX. 1.4, WHILE #2 ACHIEVED APPROX..1.2. REJECTED TAKEOFF APPROX. 70 KNOTS. REMOVED AND REPLACEDApr 20, 2020 · N839AW · Airbus A319132 · Fuel Controlling SystemSDR GTIA2020032335118Seal · damagedDIRTY SOCK SMELL ON DESCENT THROUGH 4000: PACK 2 ISOLATED AND SMELL DISSAPATED-ACCOMPLISHED AMM 21-00-00-615-803-A LEVEL B. DECONTAMINATION OF ECS. REMOVED, INSPECTED AND REINSTALLED ENG 1 AND 2 PRV IAW AMM 36-11-52. NO DEFECTS NOTED. REMOVED, INSPECTED AND REMar 21, 2020 · N522NK · Airbus A319132 · Turbine Engine Oil SystemSDR SOKF202002290001Switch · malfunctionedAFTER TAKE OFF FROM SAL TO TGU THE AIRCRAFT RETURNED TO SAL DUE TO THE ECAM SHOWED HYDRAULIC YELLOW RESERVOIR LOW LEVEL FOLLOWED BY HYDRAULIC YELLOW ENGINE 2 PUMP LOW PRESSURE THE ENGINE 2 DRIVEN PUMP WAS SHUTDOWN AFTER 1 MINUTE OF OPERATION. NO OVERWEIGHT LANFeb 26, 2020 · N703AV · Airbus A319132 · Hydraulic System, MainSDR AALA2020021759008Bleed Valve · defectiveAIRCRAFT WAS GROUNDED: REPEAT PRESSURIZATION WRITE-UP LARGE FLUXUATIONS IN CABIN VERTICAL SPEED DURING DECENT (-1300 TO +300) SYSTEM 1. REPLACED # 2 ENGINE BLEED PRESSURE REGULATING VALVE PER AMM 36-11-52.Feb 14, 2020 · N802AW · Airbus A319132 · Compressor Bleed ValveSDR SOKF202001270001Flt Controls · malfunctionedDURING FLIGHT FROM SJO TO BOG THE AIRCRAFT DIVERTED TO PTY DUE TO ECAM WARNING LOST OF FLIGHT CONTROLS AT FL 370 DUE TO AIRBUS REFERENCE : 80742128/008 ACTION: PERFORMED AFS TEST IN ACCORDANCE WITH AMM TASK 22-96-00-710-001-A, TEST OK. DUE TO PFR AUTO FLT A/THJan 23, 2020 · N703AV · Airbus A319132 · Auto Flight SystemSDR AALA2019120189035Apu · leakingAIRCRAFT WAS GROUNDED: FLT. ATD REPORTED FUMES ODOR FUEL SMELL. SEVERITY MILD/MODERATE CATEGORY C. ONCE QUICK ACTIONS ITEMS COMPLETED SMELL GOT A LITTLE BETTER. MAINTENANCE TROUBLESHOT APU AND FOUND OIL LEAKING INTERNALLY FROM AIR INTAKE. INTERNAL IMPELLAR ANDDec 17, 2019 · N813AW · Airbus A319132 · APU Core EngineSDR CALA2019120702161Indication Sys · malfunctionedLOW OIL QTY AFTER T/ODISPLAYED/4.0 QT WITH A FACE TO FACE WITH PILOTS, THEY SAID THE OIL QTY IN BOTH ENGINES WERE 22.5 ON THEIR WALKAROUND/PREDEPARTURE CHECKS, WHILE ROLLING DOWN THE RUNWAY THE NUMBER 2 OIL QTY WENT DOWN TO 4.0 AND THE INDICATION WAS FLASHING.Dec 7, 2019 · N425UA · Airbus A320232 · Turbine Engine Oil SystemSDR AALA2019121099008Packing · leakingAIRCRAFT WAS GROUNDED: PILOT REPORTS SMALL HINT OF OIL SMELL FROM THE PACKS IN CRUISE. ON DESCENT ODOR INCREASED TO A VERY LARGE SMELL. MAINTENANCE FOUND OIL LEAKING FROM APU BEARING CAVITY LUBRICATION TUBES. MAINTENANCE REMOVED AND REPLACED APU TURBINE BEARINDec 7, 2019 · N826AW · Airbus A319132 · APU Oil SystemSDR AALA2019111169012Apu · leakingAIRCRAFT WAS GROUNDED: PILOT REPORTS DIRTY SOCK SMELL ON DECENT IN COCKPIT AND CABIN. MAINTENANCE FOUND SOURCE OF ODOR TO BE FROM APU. SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED THE APU IAW JOB CARD 26L31049005. (CLOSED)Nov 5, 2019 · N813AW · Airbus A319132 · APU Core EngineSDR SOKF20191104006Actuator · damagedDURING TO (20NTS) FROM LIM TO BOG, THE TO WAS REJECTED DUE TO ECAM WARNING MSG ENG 2 COMPRESSOR VANE, BRAKE TEMP 140 DEGREES AFTER REJECTED TAKEOFF AT LIM STA DUE TO TSM 75-30-00-810-844-A REMOVED AND REPLACED ACTUATOR-VSV (4022KS) IAW AMM 75-32-41-000-010 ANDNov 2, 2019 · N480TA · Airbus A319132 · Compressor Bleed ValveSDR GTIA2019102234720Seal · leakingDIRTY SOCK SMELL ON DESCENT FROM 6,000 TO THE GROUND AFT AND FLT DECK-DECONTAMINATED ECS PER AMM 21-00-00, NO SMELL NOTICED. R&R ENG 1 & ENG 2 DEOILER SEAL & MATING RING AS PRECAUTIONARY PER AMM 72-60-31. OPS/LEAK CHK OKOct 22, 2019 · N510NK · Airbus A319132 · Engine Bleed Air SystemSDR AALA2019102539007Unknown · odorAIRCRAFT WAS GROUNDED: STRONG ODOR OF OIL WHEN APU BLEED AIR TURNED ON. MAINTENANCE PERFORMED JOB CARD 2600021001. ISOLATED ODOR TO APU. SUPPLEMENTAL INFORMATION: MAINTENANCE REPORTS ACCOMPLISHED JOB CARD 26L00021002 AND 26L00021004, FOUND NO DISCREPANCIES. NOOct 22, 2019 · N838AW · Airbus A319132 · Air Distribution SystemSDR AALA2019102319047Garlock Seal · leakingAIRCRAFT WAS GROUNDED: PILOT REPORTS WHILE AIRBORNE, THERE WAS A DIRTY GYM-SOCK SMELL IN THE COCKPIT, IT WAS EVIDENT THROUGHOUT THE FLIGHT, LOW LEVEL, BUT CONSISTANT, F/A IN AFT GALLEY SMELLED COOLANT/ANTIFREEZE BRIEFLY DURING GROUND OPS BEFORE T/O. MAINTENANCOct 21, 2019 · N807AW · Airbus A319132 · Turbine Engine Oil SystemSDR GTIA2019101074682Engine · smokePULLING INTO GATE, SHUT DOWN ENGINE #2 AND HAS A MASSIVE AMOUNT OF SMOKE CAME FROM ENGINE #2 AFTER SHUTDOWN NO ECAM MESSAGES DISPLAYED-VISUALLY INSPECTED AND PERFORMED ENGINE RUN/SHUTDOWN PER AMM 71-00-00 NO DEFECTS NOTEDOct 7, 2019 · N512NK · Airbus A319132 · Engine (Turbine/Turboprop)SDR GTIA2019091034613Solenoid Valve · faultyENG 1 O;TEMP WHILE CLIMING THROUGH 3000/FUEL FLOW 8200 ON #1 ENG AND 7200 ON ENG 2 ALL OTHER PARAMETERS NORMAL NORMAL LANDING UNDER WEIGHT LANDING FOB 11.9. R&R #1 ENG HPC 10TH STAGE IAW AMM 75-32-54, R&R SOLENOID VALVE IAW AMM 75-32-52 PENDING ENGINE RUN FOR Sep 10, 2019 · N532NK · Airbus A319132 · Compressor Bleed ControlSDR GTIA2019083134587Seal · damaged1 AIR CONDITIONING SMELL DIRTY SOCKS PASSING FLIGHT LEVEL 290-PERFORM TSM 05-50-00-810-831-A AND IDENTIFY THE APU LEAKING OIL AND FOUND ENGINE # 1 AND ENGINE # 2 LEAKING OIL FROM DE-OILER SEAL. PERFORM ACTION ON LOG PAGE 2547222-1. PERFORM ACTION ON LOG PAGEAug 31, 2019 · N524NK · Airbus A319132 · Turbine Engine Oil SystemSDR AALA2019082629016Engine · malfunctionedAIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO PHX ON ACCOUNT OF RIGHT ENGINE OIL QUANTITY DROPPING. EMERGENCY WAS DECLARED BY ATC. PILOT REPORTS RT ENGINE SUDDENLY LOST OIL QUANTITY FROM 19 TO 5, GRADUAL LOSS FROM 5 TO 2.5 THEN BACK TO 9.0, OIL PRESSURE THROUGHOUTAug 21, 2019 · N819AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR AALA2020080629016Oil System · low pressureAIRCRAFT WAS GROUNDED, FLIGHT RETURNED TO DEPARTURE ON ACCOUNT OF RIGHT ENGINE OIL QUANTITY DROPPING. EMERGENCY WAS DECLARED BY ATC. PILOT REPORTED RT ENGINE SUDDENLY LOST OIL QUANTITY FROM 19 TO 5, GRADUAL LOSS FROM 5 TO 2.5 THEN BACK TO 9.0, OIL PRESSURE TAug 21, 2019 · N819AW · Airbus A319132 · Engine Oil PressureSDR AALA201908129016Actuator · intermittentAIRCRAFT WAS GROUNDED: PILOT REJECTED TAKEOFF DUE TO ECAM "ENGINE 1 COMPRESSOR VANE". MAINTENANCE TROUBLESHOT IAW TSM 75-30-00-810-852-A. VSV SYSTEM INTERACTION ISSUE ON ENG 1. FOUND THE VSV ACTUATOR INTERMITTENTLY FAULTY. REMOVED AND REPLACED THE VSV ACTUATORAug 11, 2019 · N827AW · Airbus A319132 · Turbine Engine Compressor SectionSDR SOKF20190814005Actuator · damagedDURING TAKE OFF FROM LIM TO CZC THE AIRCRAFT REJECTED THE TO DUE TO WHEN SELECT TAKE OFF POWER ECAM: ENG 2 COMPRESSOR VANE, AT LIM STATION AS PER TSM 75-30-00-810-844-A ENG 2 VARIABLE STATOR VANE (VSV) ACTUATOR (4022KS), WAS REMOVED AND REPLACED AS PER AMM 75Aug 11, 2019 · N520TA · Airbus A319132 · Compressor Bleed ControlSDR AALA201907269035Turbine Blades · damagedAIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO PHX ON ACCOUNT OF NUMBER 1 ENGINE ISSUE. ENG 1 FAIL ENG 1 COMPRESSOR AND OVER LIMIT EGT REVESER DEPLOYED AFTER LANDING. EMERGENCY DECLARED. MAINTENANCE ACCOMPLISHED BORESCOPE INSPECTION, FOUND EXTREME DAMAGE TO THE 6THJul 26, 2019 · N837AW · Airbus A319132 · Turbine SectionSDR AALA201907229021Actuator · faultyAIRCRAFT WAS GROUNDED: PILOT REPORTS AT OR ABOUT 80 KIAS ON TAKE-OFF ROLL, AMBER ECAM ENG 1 COMPRESSOR VANE MEMO, NO OTHER ECAM ACTIONS NOTED. CONTINUED T/O. ECAM CLEARED IN LESS THAN 5 SEC. (CONT'D) ON LANDING ECAM ENG. 1 COMPRESSOR VANE WITH ACCOMPANIED ECAMJul 18, 2019 · N820AW · Airbus A319132 · Turbine Engine Compressor SectionSDR SOKF20190716004Sensor · out of adjustDURING CLIMB FORM MDE TO SAL THE AIRCRAFT RETURN TO MDE DUE TO L/G NO UP LOCKED AND LANDING GEARS DOOR NOT CLOSED AT MDE STATION PERFORMED TSM 32-31-00-810-808-A REV 48 DATE 01-MAY-2019 L/G AND DOORS WILL NOT OPERATE AFTER SELECTION WAS PERFORMED TEST OK PASSEJul 12, 2019 · N520TA · Airbus A319132 · Landing Gear Position and WarningSDR GTIA2019060303377Engine · leakingMUSTY ODOR EXPERIENCED DESENDING THROUGH 7/6000 PRIOR TO LANDING-PERFORMED TMS 05-50-00.INSPECTED APU ENG 1 + 2 LE LEAKS FOUND. PERFORMED ECS DECONTAMINATION WITH # 1 + 2 ENG IAW AMM 21-00-00-615-001. NO SMELL NOTICED WITH ENG RUN. FOUND APU TO BE THE COUSE OMay 30, 2019 · N504NK · Airbus A319132 · Engine (Turbine/Turboprop)SDR SOKF20190517003Adiru · damagedDURING CLIMB FROM LIM TO CZC THE AIRCRAFT RETURNED TO LIM DUE TO ECAM WARNING, ADR 1 FAULT AND GPWS INOP, AT LIM STATION PERFORMED TSM 34-14-00-810-808-A REMOVED AND REPLACED THE ADIRU 1 (1FP) AS PER AMM 34-12-34-000-001-A AND AMM 34-12-34-400-001-A, PERFORMEDMay 15, 2019 · N520TA · Airbus A319132 · Inertial Guidance SystemSDR AALA201905159017Compressor Blade · damagedAIRCRAFT WAS GROUNDED: PILOT REJECTED TAKEOFF AT 40-60 KNOTS DUE TO ENGINE ONE COMPRESSOR STALL. NO INJURIES REPORTED. FLIGHT RETURNED TO GATE FOR MAINTENANCE INSPECTION. MAINTENANCE ACCOMPLISHED BORESCOPE OF THE ENGINE AND FOUND DAMAGE TO THE 6TH AND 7TH STAGMay 14, 2019 · N824AW · Airbus A319132 · Turbine Engine Compressor SectionSDR SOKF20190502002Flow Valve · damagedDURING CLIMB FROM SAL TO MCO THE AIRCRAFT RETURNED TO SAL DUE TO ECAM WARNING "CAB PR EXCESS CAB ALT & CAB PR SAFETY VALVE OPEN & CAB PR LO DIFF PR & PILOT REPORT CABIN DEPREZURIZATION IN FLIGHT” AT SAL STATION PERFORMED TSM IAW 21.31.00.810..809 REMOVED AND RApr 28, 2019 · N520TA · Airbus A319132 · Cabin Cooling SystemSDR AALA2019041509021Blade · damagedAIRCRAFT WAS GROUNDED, PILOT REPORTS THE #1 ENG SN# V11099 OBSERVED SYMPTOMS INDICATING A LOSS IN HPC PERFORMANCE, INCREASE IN EGT, WF, LPR, CET, N2, ICT2, DECREASE IN TER3. DECREASE IN TAKEOFF EGT MARGIN. MAINTENANCE ACCOMPLISHED BORESCOPE INSPECTION ON STAApr 9, 2019 · N818AW · Airbus A319132 · Turbine Engine Compressor SectionSDR AALA201903279033Plug · leakingA STRONG MUSTY ODOR FOR THE LAST 5 MINUTES OF FLIGHT IN COCKPIT AND CABIN. APU WAS OFF AT THE TIME. THE AIRCRAFT WAS GROUNDED. APU FACTORY GEAR BOX PLUG LEAKING OIL DOWN ON INLET AND INGESTED, IN INTAKE. MAINTENANCE REMOVED AND REPLACED THE APU IAW CARD 26LMar 24, 2019 · N839AW · Airbus A319132 · APU Oil SystemSDR RJEF20190327001Hydraulic Line · leakingDURING CLIMB OF FLIGHT LRC697 (SJO-BOG) THE AIRCRAFT TRIGGERED MESSAGE RELATED WITH LOW PRESSURE ON HYDRAULIC RESERVOIR OF GREEN SYSTEM AND RETURNED TO SJO FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE FOLLOWING TWO ITEMS: 1) "COCKPIT DOOMar 23, 2019 · N479TA · Airbus A319132 · Hydraulic System, MainSDR AALA201902189010Compressor · stalledAT FL360, NR 2 ENGINE COMPRESSOR STALL AND EGT OVERTEMP. NR 2 ENGINE AUTO SHUTDOWN, FOLLOWED ECAM PROCEEDURES, NR 2 ENGINE MASTER SWITCH OFF AND LANDED. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED NR 2 ENGINE IAW 26L40071004 AND 26L00071015.Feb 15, 2019 · N821AW · Airbus A319132 · Turbine Engine Compressor SectionSDR AALA201902159006Engine · stalledNUMBER 2 ENGINE HIGH EGT WITH COMPRESSOR VANE FAULT. ENGINE SHUTDOWN WITH A SINGLE ENGINE TIME 15 MINUTES. DIVERTED, EMERGENCY WAS DECLARED. FLIGHT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE IAW JC 26L40071004,Feb 12, 2019 · N821AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR RJEF20190215001Actuator · failedUPON ARRIVAL OF FLIGHT TAI422, THE PILOT REPORTED: "ENG 2 COMPRESSOR VANE", THE AIRCRAFT WAS HELD ON GROUND TO PERFORM FAULT ANALYSIS IN ACCORDANCE WITH TSM 75-30-00-810-848-A; REPLACED THE MASTER ACTUATOR OF LPC BLEED SYSTEM OF ENGINE 2 IN ACCORDANCE WITH AMMFeb 11, 2019 · N524TA · Airbus A319132 · Compressor Bleed ControlSDR ANCF201902150601Bleed Valve · malfunctionedIN FLIGHT DURING INITIAL CLIMB, WITH PACK # 2 INOPERATIVE, (ENG) AIR PACK 2 REGULATOR FAULT + ENG 1 BLEED ABNORMAL PR APPEARED ON ECAM, AS RESULT PRESSURIZATION FAILURE, INMIDIATE RETURN PERFORMED // CORRECTIVE ACTION: FEB 6. IN ACCORDANCE WITH TSM 36-11-00-81Feb 6, 2019 · N690AV · Airbus A319132 · Compressor Bleed ValveSDR GTIA2019020403137Hinge · damagedENG #2 INBD THRUST REVERSER HINGE #1 DAMAGED. DIMENSIONS:- L=8.0MM, W=6.0MM, D=7.5MM. RAF01 235085302 OPENED.-REVIEWED LTPR NRI 5000839597-0010 AND HAS BEEN ACCOMPLISHED. REPAIR IS PERMANENT CAT A NO FURTHER ACTION REQ.Feb 4, 2019 · N531NK · Airbus A319132 · Engine Thrust ReverserSDR AALA201901029004Actuator · faultedNR 2 ENGINE COMPRESSOR VANE ECAM MESSAGE DISPLAYED DURING TAKEOFF. WARNING REMAINED FOR MORE THAN 60 SECONDS, FLIGHT REJECTED TAKEOFF AT 90 KIAS. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED VSV ACTUATOR ON THE NR 2 ENGINE IAW JC 26T40075005, AND PERFORMDec 31, 2018 · N826AW · Airbus A319132 · Turbine Engine Compressor SectionSDR RJEF20181207001Outflow Valve · unserviceableDURING CLIMB OF FLIGHT TP9963 FROM MCO TO LIM, THE AICRAFT HAD ABNORMAL FUNCTIONING OF PRESSURIZATION SYSTEM AND DIVERTED TO MIA FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED: 1) "OUTFLOW VALVE OPENS AND CLOSES CONSTANTLY WITH CPC1 AND CPC2 CDec 4, 2018 · N479TA · Airbus A319132 · Pressure Regulator/Outflow ValveSDR GTIA2018120632988Seal · leaking"DIRTY SOCK SMELL WHILE DESCENDING THROUGH 15,000 FT. TURNED OFF PACK 1 PER ODOR/FUMES CHECKLIST AND SMELL DISSIPATED-PERFORMED TSM 05-50-00-810-831-A PREF LP 241559102 FOR R&R # 1 ENG DE-OILER SEAL. PERFORMED ENG # 1 RUN IAW AMM 71-00-00 WITH PACKS ON. NODec 3, 2018 · N504NK · Airbus A319132 · Engine (Turbine/Turboprop)SDR GTIA2018111292957Engine · failedON APPROACH ENG 2 FAIL. DID NOT RESTART. DID NOT RESTART DURING THE AUTOMATIC RESTART. ENGINE WAS SHUT DOWN-BORESCOPED HP COMPRESSOR AND HPT IAW AMM 72-00-00. NO DEFECTS FOUND. PERFORMED FUNCTIONAL TEST OF THE HPC STAGE 7 BLEED VALVE AND SOLENIODS IAW AMM 75-3Nov 9, 2018 · N502NK · Airbus A319132 · Engine (Turbine/Turboprop)SDR AALA2018101209013Pump · faultedCAPTAIN REPORTED ACARS MESSAGE AT 2126Z ON THE NR 1 ENGINE COMPRESSOR VANE. THE QRH WAS CHECKED AND IT STATED TO AVOID RAPID THRUST CHANGES AND THERE WERE NO RESTRICTIONS ON CONTINUING INTO CLT. WHEN AC WAS WITHIN 30 MINUTES OF DESTINATION, THE CAPTAIN REPORTOct 9, 2018 · N807AW · Airbus A319132 · Engine Fuel PumpSDR AALA201810129005Fmu · faultedCAPTAIN REPORTED ACARS MESSAGE AT 2126Z ON THE NR 1 ENGINE COMPRESSOR VANE ECAM MESSAGE. THE QRH WAS CHECKED AND IT STATED TO AVOID RAPID THRUST CHANGES AND THERE WERE NO RESTRICTIONS ON CONTINUING TO DESTINATION. WHEN ACFT WAS WITHIN 30 MINUTES OF THE DESTIOct 9, 2018 · N807AW · Airbus A319132 · Fuel Controlling SystemSDR AALA2018083079057Bleed Valve · failedDURING DECENT, WITH IDLE THRUST HIGH PRESSURE VALVE ON THE NR 2 ENGINE INTERMITTENTLY FAILED. FOUND HP VALVE CONNECTOR & BACKSHELL DAMAGED. REPLACED THE NR 2 ENGINE BLEED HIGH PRESSURE VALVE IAW AMM 36-11-51.Aug 25, 2018 · N808AW · Airbus A319132 · Compressor Bleed ValveSDR RJEF201808068001Computer · failedDURING CLIMB, THE AIRCRAFT HAD A FAILURE MESSAGE OF FLAP SYSTEM, RETURNED TO DEPARTURE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED A F/CTL FLAP LEVER NOT ZERO, AND A F/CTL FLAP SYS 2 FAULT, MAINTENANCE PERFORMED A FAULT ANALYSIS IAW TSM 27-51-00-810-805-AAug 1, 2018 · N479TA · Airbus A319132 · Trailing Edge Flap Control SystemSDR AALA2018073109021B-Nut · looseDURING CLIMB, THE FLIGHT ATTENDANTS REPORTED FUMES IN THE CABIN. FIRST CALL RECEIVED WHILE CLIMBED THROUGH 9,000 FT. PERFORMED QRC FOR SMOKE, AVIONICS SMOKE, FUMES TRANSITION TO QRH, AIRCRAFT ODOR, TOXIC SUB, VOL LIQ CHECKLIST. THE FUMES NEVER FULLY DISAPATEDJul 29, 2018 · N822AW · Airbus A319132 · Turbine Engine Oil SystemSDR AALA2018071219012Engine · stalledAT 12,000 FEET, IDLE THRUST, THE NR 2 ENGINE HAD A COMPRESSOR STALL WITH ECAM. DURING CRUISE, RECEIVED AN ECAM MESSAGE FOR THE NR 1 ENGINE COMPRESSOR VANE, MESSAGE CLEARED AFTER APPROXIMATELY TWO MINUTES. AFTER LANDING, RECEIVED SAME ECAM MESSAGE, MESSAGE CLJul 9, 2018 · N816AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR RJEF20180529001Fcu · malfunctionedDURING CLIMB, THE AIRCRAFT HAD A FAILURE OF THE KNOB SELECTORS SPEED AND HEADING OF THE FCU, LATER, THE AIRCRAFT DIVERTED, AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE FCU SPEED AND HEADING KNOBS BECAME INOPERATIVE WITH NO ECAM MESSAGE OR ANY APPARENT May 27, 2018 · N499TA · Airbus A320233 · Autopilot System
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