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 CALA2016121696042Fitting · corrodedCORROSION FWD CARGO BAY RT CROSSBEAM END FITTING FRAME 27 STRINGER 39 - 42R. REMOVED CORROSION IAW SRM 51-24-00. REMOVED AND REPLACED THE END FITTING IAW SRM 51-72-11.Dec 15, 2016 · N891UA · Airbus A319132 · Fuselage Main, Attach FittingsSDR CALA2016121696043Door Sill · corrodedCORROSION ON THE L2 DOOR SILL FRAME 66. FABRICATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, TOPCOATED, AND INSTALLED THE REPAIR IAW SRM 53-41-14 PAR 2 FIG 001.Dec 15, 2016 · N891UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR 5TTY201611280001Actuator · vibrationDURING CLIMB, VIBRATION WAS FELT FROM THE AIRCRAFT REAR AREA AT SPEED BETWEEN 250KTS TO 300KTS CONSEQUENTLY, RETURNED DEPARTURE. AFTER AN UNEVENTFUL LANDING, A FAULT ANALYSIS WAS PERFORMED PER TSM 05-50-00-810-801-A AND FOUND THE RUDDER GREEN HYD SYSTEM SERVNov 28, 2016 · N479TA · Airbus A319132 · Rudder Control SystemSDR SOKF20161128011Oven · odorDURING FLIGHT, THE AIRCRAFT RETURN TO DEPARTURE DUE TO A STRONG ODOR OF BURNING IN FWD GALLEY. PERFORMED TSM 05-50-00-810-831-A AND FOUND THE ODOR CAME FROM FWD GALLEY NR 1 OVEN. REMOVED AND REPLACED THE FWD GALLEY OVEN IAW AMM 25-35-19 AND OPS CHECKED IAWNov 25, 2016 · N480TA · Airbus A319132 · Buffet/GalleysSDR AALA201611239024Seal · leakingCABIN CREW REPORTS DIRTY, MUSTY ODOR IN CABIN DURING CLIMB AND DESCENT. FOUND OIL LEAKING FROM DE-OILER VENT PIPE ON NR 1 ENGINE. R & R THE GEARBOX BREATHER OUTLET DUCT SEAL IAW AMM 72-60-31-400-010-A. RAN ENG. NO LEAKS NOTED. LEAK CHECKED GOOD. THE AIRCRAFT WNov 22, 2016 · N817AW · Airbus A319132 · Turbine Engine Oil SystemSDR GTIA2016111301662Seal · leakingDURING DESCENT EXPERIENCED DIRTY SOCKS SMELL COMPLIED WITH OS AFTER PACK 1 SHUTOFF SMELL DISSIPATED. PERFORMED INSPECTION AND PACK BURNOUT IAW AMM 21-00-00, FOUND THE NR 1 ENG DE-OILER CASING SEAL ASSEMBLY LEAKING OIL. REMOVED AND REPLACE THE DE-OILER CASING Nov 13, 2016 · N523NK · Airbus A319132 · Turbine Engine Accessory DriveSDR AALA201610249001Actuator · faultyAIRCRAFT WAS GROUNDED. IN FLIGHT NR 2 FUEL VALVE SHOWED IN TRANSIT ON FUEL PAGE, REMAINED SAME UNTIL ENGINE SHUTDOWN. ALL OTHER INDICATIONS NORMAL. MAINTENANCE REPLACED THE NR 2 ENGINE LOW PRESSURE FUEL VALVE ACTUATOR PER AMM 28-24-51-000-001-A AND 28-24-51Oct 23, 2016 · N832AW · Airbus A319132 · Aircraft Fuel Distribution SystemSDR GTIA2016091901594Seal · leakingDIRTY SOCK, OIL ODOR IN ALL PHASES OF FLIGHT. R & R DEOILER SEAL ASSEMBLY IAW AMM 72-60-31. DECONTAMINATION OF THE ECS ONLY LEFT PACK ACCOMPLISHED IAW AMM 21-00-00-615-004. R & R RECIRCULATION FILTERS AS PRECAUTION IAW AMM 71-00-00. NO ODOR AT THIS TIME WITHSep 19, 2016 · N503NK · Airbus A319132 · Turbine Engine Oil SystemSDR AALA201608199005Oil Cooler · leakingAIRCRAFT WAS GROUNDED, FLIGHT CREW REPORTED A CABIN ODOR, DIRTY SOCK, WHEN SWITCHING FROM GROUND AIR TO APU BLEED AIR. MAINTENANCE REPLACED THE APU OIL COOLER ASSY IAW AMM 49-91-44 AND ACCOMPLISHED A SATISFACTORY LEAK AND OPS CHECK.Aug 17, 2016 · N832AW · Airbus A319132 · APU Oil SystemSDR AALA201608089002Pump · failedFLIGHT CREW REPORTED RECIEVEING A NR 1 ENGINE FUEL CONTROL ECAM FAULT DURING TAKEOFF ROLL AND ABORTED THE TAKEOFF AT 60 KNOTS. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL PUMP AND FUEL METERING UNIT IAW AMM 73-12-41 & 73-22-52. A SATISFACTORAug 4, 2016 · N802AW · Airbus A319132 · Engine Fuel PumpSDR AALA201608089003Metering Unit · faultedFLIGHT CREW REPORTED RECIEVEING A NR 1 ENGINE FUEL CONTROL ECAM FAULT DURING TAKEOFF ROLL AND ABORTED THE TAKEOFF AT 60 KNOTS. AIRCRAFT WAS GROUNDED. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL PUMP AND FUEL METERING UNIT IAW AMM 73-12Aug 4, 2016 · N802AW · Airbus A319132 · Fuel Controlling SystemSDR AALA201607259008Terminal · brokenFLIGHT CREW REPORTED THAT THE NR 2 ENGINE EGT WAS ABNORMALLY LOW (160 DEGREES C) DURING TAKE OFF ROLL AND ABORTED THE TAKEOFF BELOW 60 KNOTS. IT WAS ALSO NOTED THAT THE EGT INDICATION WAS ERRATIC DURING ENGINE SHUTDOWN AT THE GATE. AIRCRAFT GROUNDED. MAINTENJul 22, 2016 · N801AW · Airbus A319132 · Engine Indicating System WiringSDR AALA201607269001Fmu · faultedFLIGHT CREW REPORTED THAT THE NR 1 ENGINE WAS SLOW TO SPOOL AND AN ECAM FUEL CONTROL FAULT DISPLAYED DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AROUND 60 KNOTS. THE AIRCRAFT RETURNED TO THE GATE AND WAS REMOVED FROM SERVICE. AIRCRAFT GROUNDED. MAINTENJul 22, 2016 · N823AW · Airbus A319132 · Fuel Controlling SystemSDR AALA201607119001Actuator · warning messageDURING TAKEOFF, FLIGHT CREW REPORTED THAT AN ECAM MESSAGE FOR A NR 2 ENGINE COMPRESSOR VANE FAULT OCCURRED AND THE TAKEOFF WAS ABORTED AROUND 80 KNOTS.THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER INCIDENT. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED Jul 10, 2016 · N822AW · Airbus A319132 · Engine Bleed Air SystemSDR AALA201606199013Actuator · faultyAIRCRAFT WAS GROUNDED, ON TAKEOFF FLEX EPR 1.33 FLIGHT CREW RECEIVED ECAM ENGINE 1 COMPRESSOR VANE FAULT AROUND 50 KNOTS. TAKEOFF WAS ABORTED AROUND 60 KNOTS. MAINTENANCE REPLACED THE NR 1 ENGINE VSV ACTUATOR AND ACCOMPLISHED A SATISFACTORY LEAK AND OPS CHECJun 15, 2016 · N822AW · Airbus A319132 · Compressor Bleed ControlSDR AALA201605169006Engine · slowABORTED TAKEOFF. ACFT WAS GNDED. NR 2 ENG SLOW TO SPOOL ON TAKEOFF ROLL, FLIGHT CREW ABORTED TAKEOFF, BETWEEN 25 & 30 KNOTS & RETURNED TO THE GATE. ACCOMPLISHED TSM TASK 73-00-00-810-881-A, NR 2 ENG ACCELERATION TESTED NORMAL, FADEC TESTED NORMAL, NO FAULTSMay 15, 2016 · N803AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR SOKF20160509002Warning Message · activatedDURING CLIMB, THE ACFT RETURNED TO DEPARTURE, DUE ECAM WARNING MESSAGE NAV GPWS FAULT, LANDED SPURIOUS INDICATION WAS SIGNALED, AT SAL BS WAS INCLUDED AS MEL 34-48-01. THE ACFT WAS RETURNED TO NORMAL OPERATION.May 7, 2016 · N480TA · Airbus A319132 · Ground Proximity SystemSDR AALA201604209010Flow Divider · leakingAIRCRAFT WAS GNDED. SIGNIFICANT ODOR IN CABIN & COCKPIT SIMILAR TO DIRTY SOCKS OR OIL SMELL. FOUND SEVERAL FUEL LEAKS ON APU IGV ACTUATOR FUEL LINE & FUEL FLOW DIVIDER LEAKING FUEL AT DRAIN LINE DURING RUN OPERATION. TIGHTENED FUEL LINE & REPLACED FUEL FLOWApr 19, 2016 · N827AW · Airbus A319132 · APU Engine Fuel and ControlSDR AALA201604209011Fuel Line · leakingAIRCRAFT WAS GNDED. SIGNIFICANT ODOR IN CABIN & COCKPIT SIMILAR TO DIRTY SOCKS OR OIL SMELL. FOUND SEVERAL FUEL LEAKS ON APU IGV ACTUATOR FUEL LINE & FUEL FLOW DIVIDER LEAKING FUEL AT DRAIN LINE DURING RUN OPERATION. TIGHTENED FUEL LINE & REPLACED FUEL FLOWApr 19, 2016 · N827AW · Airbus A319132 · APU Engine Fuel and ControlSDR AALA20160407007Wire Harness · chafedAIRCRAFT WAS GNDED. DURING TAKEOFF ROLL NR 1 ENG EXCEEDED MAX EGT. TAKEOFF ABORTED AT APPROX 65 KNOTS. FOUND CHAFING ON EGT HARNESS. R & R HARNESS IAW AMM 71-21-23. ACCOMPLISHED LT ENG RUN IAW AMM 71-00-00. SYS CHECKED NORMAL.Apr 4, 2016 · N134AN · Airbus A321231 · Engine Indicating System WiringSDR GTIA2016032301509Drain Line · chafedTHE CONNECTOR THAT ATTACH THE FIRE BOTTLE AND FIRE BOTTLE DISTRIBUTION PIPE BECAME LOOSE, CONNECTOR NOT SAFETIED AND BACKED OFF FROM THE FIRE BOTTLE BACK AS FAR AS POSSIBLE, CONTACTING A DRAIN LINE AND CHAFED A HOLE IN THE DRAIN LINE.Mar 23, 2016 · N528NK · Airbus A319132 · Engine (Turbine/Turboprop)SDR GTIA2016032201508Union · chafedTHE CONNECTOR THAT ATTACHES THE FIRE BOTTLE AND FIRE BOTTLE DISTRIBUTION PIPE BECAMES LOOSE, CONNECTOR NOT SAFETIED AND BACKED OFF FROM THE FIRE BOTTLE, BACK AS FAR AS POSSIBLE, CONTACTING A DRAIN LINE AND CHAFED A HOLE IN THE DRAIN LINE AND VIBRATED AND CUT IMar 22, 2016 · N528NK · Airbus A319132 · Extinguishing SystemSDR AALA201603099015Actuator · defectiveAIRCRAFT WAS GNDED. DURING TAKEOFF THE CREW RECEIVED A COMPRESSOR VANE FAULT ON NR 1 ENG AT 60 KNOTS & THE TAKEOFF WAS ABORTED. REPLACED VSV ACTUATOR ON NR 1 ENG IAW TASK CARD 26T40075005.Mar 6, 2016 · N805AW · Airbus A319132 · Compressor Bleed ValveSDR AALA201602229006Apu · leakingAIRCRAFT WAS GNDED. VERY STRONG ODOR DIRTY SOCK SMELL IRRITATES NASAL PASSAGES BADLY. FOUND APU LEAKING OIL FROM TURBINE ACCESS PLATE AFT OF INLET & REPLACED THE APU IAW TASK CARD 26L31049003. A SATISFACTORY OPERATIONAL & LEAK CHECK WAS ACCOMPLISHED & NO ODFeb 21, 2016 · N836AW · Airbus A319132 · APU Core EngineSDR AALA201601099002Actuator · defectiveAIRCRAFT WAS GNDED. ECAM CLASS 1, ENG 2 COMPRESSOR VANE AT POWER UP FOR TAKEOFF. FLIGHT CREW ABORTED TAKEOFF, LESS THAN 80 KNOTS & RETURNED TO GATE. REPLACED NR 2 ENG VSV ACTUATOR & ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK IAW AMM 75-32-41.Jan 8, 2016 · N821AW · Airbus A319132 · Compressor Bleed ValveSDR GTIA2015010301444Engine · odorON APPROACH, AT ABOUT 10K FT, BOTH PILOTS DETECTED SIGNIFICANT ODOR OF DIRTY SOCKS OR SOUR MILK. SUSPECTING POSSIBLE PACK FUME EVENT, WE TURNED OFF PACK 1 TO ISOLATE AND ODOR INSTANTLY WENT AWAY. TROUBLESHOT IAW TSM 05-50-00-810-831A. IAW DECISION TABLE, ODOJan 3, 2016 · N528NK · Airbus A319132 · Engine (Turbine/Turboprop)SDR RJEF20151224001Outflow Valve · unserviceableDURING CLIMB OF THE ACFT AS FLIGHT TAI-593, THE PILOT REPORTED THAT THE OUTFLOW VLV BECAME UNCONTROLLABLE. THE SYS WAS RESET BY THE CREW, BUT NOT SUCCESS OBTAINED ON CONTROLLING CABIN V/S & HENCE, THE ACFT WAS RETURNED. AFTER AN UNEVENTFUL LANDING & IAW TSM Dec 24, 2015 · N479TA · Airbus A319132 · Pressure Regulator/Outflow ValveSDR AALA201512049001Pressure Switch · defectiveAIRCRAFT WAS GNDED. FLIGHT CREW REPORTED THAT THE GREEN HYD SYS HAD LOW PRESS LEVEL RESULTING IN LOW LEVEL WARNING & RAPID DEPLETION OF HYD FLUID. LT ENG PUMP WAS TURNED OFF WITHIN 1 MINUTE. AN EMER WAS DECLARED & THE ACFT LANDED WITH NO INCIDENTS. THE ACFDec 3, 2015 · N834AW · Airbus A319132 · Hydraulic Pressure SensorSDR AALA201512049012Hydraulic Line · defectiveAIRCRAFT WAS GNDED, FLIGHT CREW REPORTED THAT THE GREEN HYD SYS HAD LOW PRESS LEVEL, RESULTING IN LOW LEVEL WARNING & RAPID DEPLETION OF HYD FLUID. LT ENG PUMP WAS TURNED OFF WITHIN 1 MINUTE. AN EMER WAS DECLARED & THE ACFT LANDED WITH NO INCIDENTS. THE ACFTDec 3, 2015 · N834AW · Airbus A319132 · Hydraulic System, MainSDR AALA201512039001Actuator · faultyAIRCRAFT WAS GNDED. NR 1 COMPRESSOR VANE FAULT OCCURRED ON TAKEOFF ROLL & THE TAKEOFF WAS ABORTED AT 65 KTS. REPLACED THE NR 1 ENG VSV ACTUATOR. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW TASK CARD 26L00071014.Dec 2, 2015 · N823AW · Airbus A319132 · Compressor Bleed ControlSDR AALA201511159002Eec · defectiveAFTER NR 2 ENG START ONCE STABILIZED ENG NR 2 SHUTDOWN. REPLACED NR 2 ENG EEC IAW AMM 73-22-34.Nov 14, 2015 · N535UW · Airbus A321231 · Fuel Control/Turbine EnginesSDR AALA201511029014Seal · leakingON DESCENT OILY AIR SMELL IN COCKPIT, BUT NOT NOTICED IN CABIN. TROUBLE SHOT CABIN AIR QUALITY UTILIZING JC 26L00021001, 26L00021003 & FOUND NR 1 ENG DE-OILER SEAL LEAKING. R & R NR 1 ENG OIL BREATHER SEAL ASSEMBLY IAW AMM 72-60-31-001-010-A.Oct 29, 2015 · N804AW · Airbus A319132 · Turbine Engine Oil SystemSDR GTIA2015090401380Bleed Valve · failedNR 1 ENGINE FAILED, PRIOR HAD NR 1 ENGINE COMPRESSOR VANE ECAM. ACCOMPLISHED TROUBLESHOOTING IAW TSM 71-00-00-810-808-A. R & R ALL 7TH AND 10TH STAGE BLEED VALVES AND SOLENOIDS ON NR 1 ENGINE, REF LOG PAGES 71099-1, 71099-2, 71100-1, 71100-2, 99751-1, 99751-Sep 4, 2015 · N517NK · Airbus A319132 · Compressor Bleed ValveSDR AALA201508319007Actuator · defectiveTHE FLIGHT CREW ON FLIGHT 1894 ACFT 837, NOTED A NR 1 ENG COMPRESSOR VANE FAULT ON TAKEOFF ON RNWY 28R. PERFORMED A REJECTED TAKEOFF. THE ACFT WAS AT APPROX 70 KTS WHEN THE FAULT WAS RECEIVED. REPLACED THE VSV ACTUATOR & ACCOMPLISHED A SATISFACTORY OPERATIOAug 27, 2015 · N837AW · Airbus A319132 · Compressor Bleed ValveSDR RJEF20150514001Transceiver · unserviceableDURING THE FLIGHT TAI 457, THE PILOT REPORTED THE WEATHER RADAR INOPERATIVE DURING CRUISE. CONSEQUENTLY, THE ACFT WAS RETURNED FOR MX. THE ACFT WAS LANDED WITH NO INCIDENTS & AS REPORTED BY THE PILOT, WITH A LANDING WEIGHT OF 55.3 TONS. THE WEATHER RADAR TRMay 14, 2015 · N479TA · Airbus A319132 · Weather Radar SystemSDR RJEF20150416001Skin · dentedDURING ACFT PREPARATION, PRIOR TO DEPART , FOUND A DENT ON THE SKIN OF NR 2 INLET COWL. WAS DETERMINED IS OUT OF LIMITS FOR ACFT OPERATIONS IAW AMM 71-11-11 PB 601. PERFORMED ENG 2 INSPECTION AFTER BIRD STRIKE IAW AMM 05-51-19-200-001-A WITH NO ADDITIONAL DApr 15, 2015 · N522TA · Airbus A319132 · Nacelle/Pylon, Plate/SkinSDR USAA2015032500001Pressure Switch · faultyNUMBER 2 ENG FUEL FILTER CLOG INDICATION. TROUBLE SHOT IAW TSM 73-00-00-810-858A & FOUND FUEL DIFFERENTIAL PRESS SWITCH INOPERATIVE. REPLACED PRESS SWITCH IAW AMM 73-34-15-000-010 & 73-34-15-400-010.Mar 24, 2015 · N827AW · Airbus A319132 · Fuel Pressure SensorSDR USAA2015010900003Engine · making metalEMERGENCY DECLARED DURING CRUISE, NR 2 ENGINE ECAM OIL FILTER CLOG LIGHT ILLUMINATED. OIL PRESSURE OK 31 QTS, NO SURGE. AT 1426Z THE FLIGHT CREW HEARD A SMALL GROWLING NOISE. PULLED NR 2 ENGINE TO IDLE. ON FINAL APPROACH RECEIVED A RED ECAM LOW OIL QTY.Jan 8, 2015 · N840AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR CALA2014122392850Skin · damagedRIGHT ELEVATOR UPPER SURFACE HAS A TRAPPED WATER INDICATION. 113 INCHES FROM INBD, 12 INCHES FROM TE & 6 INCHES IN DIAMETER & THE LOWER SURFACE 80 INCHES FROM INBD, 5 INCHES FROM TE & 2 INCHES IN DIAMETER. CUT OUT TRAPPED WATER & APPLIED REPAIR CONFIG 1 & REDec 15, 2014 · N811UA · Airbus A319131 · Elevator, Plate/SkinSDR RJEF20141024001Actuator · malfunctionedDURING TAKEOFF RUN THE ACFT HAD THE FAILURE MSG ENG 2 FADEC ENG 2 COMPRESSOR VANE. THE TAKEOFF WAS ABORTED & RETURNED TO THE GATE FOR MX. THE ACFT WAS HELD ON GND & PERFORMED FAULT ANALYSIS IAW TSM 75-30-00-810-844-A, REPLACING THE VSV ACTUATOR OF ENG 2 IAW Oct 23, 2014 · N479TA · Airbus A319132 · Compressor Bleed ControlSDR SOKF20141019007Acm · damagedDURING CRUISE FLIGHT, SMOKE ODOR WAS FELT VERY STRONG IN THE COCKPIT, ALSO STRONG NOISE & FELT VIBRATION LT SIDE ACFT. DEVIATION & EMER DESCENT WAS DONE. PERFORMED INSPECTION IAW TSM 05-50-00-810-831-A, COS REPORTING SHEET WAS FILLED UP & FOUND ONE OF THE CAOct 17, 2014 · N520TA · Airbus A319132 · Cabin Cooling SystemSDR USAA2014091700007Engine · leakingCABIN ODOR REPORTED, MOC TECHNICAL SERVICE ITEM. MX FOUND OIL BEHIND SPINNER OF NR 1 ENG. R & R NR 1 ENG IAW JOB CARD 26L40071004.Sep 14, 2014 · N810AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR RJEF20140829001Apu · faultyDURING CLIMB THE PILOT REPORTED F/CONTROL FLAPS LOCKED, DUE THAT SITUATION THE ACFT RETURNED FOR MX, ADDITIONALLY REPORTED ANTI-ICE L WINDOW FAULT & APU AUTO SHUTDOWN. IT WAS PERFORMED A FAULT ANALYSIS IAW TSM 27-51-00-810-808-A FINDING THAT APU LT HAS A DIFFAug 27, 2014 · N564TA · Airbus A321231 · APU Core EngineSDR RJEF20140820001Transceiver · faultyPREVIOUS TO DISPATCH OF FLIGHT THE PILOT REPORTED TERRAIN ON NAVIGATION DISPLAY WAS SELECTED ON ACCORDING WITH OPERATIONAL PROCEDURE OF MEL 24-48-01, TERRAIN ON ND DISPLAY WAS INOPERATIVE IN THAT CONFIGURATION. DUE SUCH SITUATION THE ACFT WAS HELD ON GND FOR Aug 18, 2014 · N524TA · Airbus A319132 · Ground Proximity SystemSDR RJEF20140815001Valve · defectiveAT THE ARRIVAL OF THE ACFT THE PILOT REPORTED ENG 1 BEARING 4 OIL SYS HIGH PRESS. CONSEQUENTLY, THE ACFT WAS DECLARED AOG FOR MX. IAW TSM 79-20-00-810-809A, BEARING NR 4 SCAVENGE VLV ON ENG 1 WAS REPLACED IAW AMM & ALL REQUIRED OPERATIONAL TEST PERFORMED WITAug 14, 2014 · N478TA · Airbus A319132 · Turbine Engine Oil SystemSDR USAA2014070800001Sensor · faultyON TAKEOFF AT APPROX 80 KNOTS, CREW RECEIVED AN AMBER EPR MODE FAULT. AN AMBER N1 DEGRADED MODE MSG AS WELL AS AURAL ALERT & CAUTION LIGHT. CREW REJECTED TAKEOFF & RETURNED TO GATE. AMBER AUTO THRUST OFF MSG DISPLAYED. PERFORMED TSM TASK 73-22-00-810-817-Jul 7, 2014 · N804AW · Airbus A319132 · Fuel Controlling SystemSDR USAA2014051200003Blade · damagedCREW REPORTED A BIRD STRIKE ON TO AT ABOUT 800 FEET AGL. ONLY ONE BIRD WENT INTO LT ENG. ENG CONTINUES TO RUN WITH NORMAL INDICATIONS. CREW DECLARED AN EMERGENCY & RETURNED TO FIELD AT LGA. AFTER LANDING, CREW SHUT ENG DOWN. ACCOMPLISHED BIRD STRIKE INSPECMay 10, 2014 · N828AW · Airbus A319132 · Turbine Engine Compressor SectionSDR RJEF20140409003Windshield · damagedDURING CLIMB OF THE ACFT FLIGHT TAI-383 FROM SAL TO BOG, THE PIC REPORTED LEFT WINDSHIELD BIRD STRIKE THEREFORE, THE ACFT WAS RETURNED TO SAL AIRPORT. PERFORMED AN ACFT INSPECTION FOR BIRD STRIKE IAW AMM 05-51-14-00 PB 601 AS A RESULT OF THAT INSPECTION 3 DAMApr 9, 2014 · N522TA · Airbus A319132 · Flight Compartment WindowsSDR RJEF20140309001Cable · damagedDURING THE FLIGHT TAI 450 FROM SAL TO HAV, THE PILOT REPORTED THE ELEC GEN ON ENG 2 INOPERATIVE. THE PLANE RETURNED TO AIRPORT. ONCE THE AIRPLANE WAS AT THE MX BASE IN SAL, TSM 24-00-00-810-869 WAS ACCOMPLISHED & FOUND DAMAGES ON THE IDG'S CABLES INSULATOR. Mar 5, 2014 · N479TA · Airbus A319132 · Electrical Power System WiringSDR USAA2014021700004Line · unsecureCREW REPORTED AN ENG NR 1 EPR MODE FAULT & A/T INOPERATIVE. FLIGHT RETURNED TO FIELD AT PHX & LANDED WITHOUT INCIDENT. ON ENG NR 1, THEY FOUND FLEX LINE AT INLET TORQUED BUT LINE 707667-1 WAS NOT SECURED. INSTALLED NEW LINE IAW MM 77-22-48, PB401. RAN ENG,Feb 14, 2014 · N834AW · Airbus A319132 · Engine Pressure Ratio (EPR)
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