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 USAA2014021700007Seal · leakingCREW REPORTED A STRONG ODOR OF FUEL NOTICED IN FWD & AFT GALLEYS. SINGLE ENG TAXI - ODOR COMING FROM ENG NR 1. FLIGHT RETURNED TO THE GATE. MX COMPLIED WITH JOB CARDS 26L00021001, 26L00021003 & 26L00021004. FOUND OIL COMING OUT OF NR 1 & NR 2 ENG BREATHER Feb 14, 2014 · N814AW · Airbus A319132 · Turbine Engine Oil SystemSDR GTIA201402141171Liner · damagedNR 2 ENGINE ATTRITION LINER HAS DAMAGE. MEASURED DAMAGED AREA AT APPROX .9" L X .8" W X .2500" D. ALSO, FOUND APPROXIMATELY 6" LANDING GEAR DEBONDED AREA WHICH PUTS ATTRITION LINER PANEL OUT OF LIMITS, REF AMM 72-32-85-200-010B AND 4.B.8, DAMAGE GREATER THAN Feb 14, 2014 · N532NK · Airbus A319132 · Engine (Turbine/Turboprop)SDR GTIA201402071159Eec · damagedENG 1 EPR MODE FAULT, FL 340, HIGH EGT, SHUTDOWN IN SHORT FINAL ABOUT 3 MIN TO TOUCHDOWN. ENG 1 EGT AND FUEL FLOW FLUCTUATED BUT STAYED IN OPERATING RANGE DURING DESCENT AT ABOUT 6000 FT, TEMP ROSE OVER 580 AND WE DECIDED TO LEAVE IT AT IDLE. TURNING FINAL EFeb 7, 2014 · N522NK · Airbus A319132 · Fuel Control/Reciprocating EnginesSDR USAA2014010800001Connector · unsecureAFTER TAKEOFF CREW REPORTED REVERSER NR 2 & ENG NR 2 THR INOPERATIVE ON SYS STATUS PAGE. FLIGHT RETURNED TO FIELD AT PHX & LANDED WITHOUT INCIDENT. UPON INSPECTION, FOUND OTBD LOCKING ACTUATOR CONNECTOR BACK SHELL BACKED OFF. SECURED BACK SHELL, RAN TEST ONJan 7, 2014 · N826AW · Airbus A319132 · Engine Exhaust System WiringSDR RJEF20131213013Indication Sys · oscillatesDURING CLIMB OF FLIGHT TA582 FROM SAL TO IAD THE PILOT REPORTED THAT THE ENG 2 OIL QUANTITY INDICATION SHOWED OSCILLATIONS AT HIGH THRUST SETTINGS. THE AIRCRAFT RETURNED TO SAL FOR MAINTENANCE. IT WAS VERIFIED THAT THE FAILURE IS DEFERRABLE IAW MEL 79-31-01 CDec 13, 2013 · N477TA · Airbus A319132 · Engine Oil QuantitySDR RJEF20131210011Anti-Ice System · malfunctionedDURING THE DISPATCH OF FLIGHT TA583 FROM IAD TO SAL, THE PILOT REPORTED THAT THE ACFT HAVE FAILURES, WING ANTI ICE SYS FAULT & ENG 1 FIRE LOOP B FAULT, DUE TO THOSE FAILURES THE ACFT RETURNED TO THE GATE FOR MAINTENANCE. ONCE AT THE GATE MAINTENANCE PERSONNELDec 8, 2013 · N478TA · Airbus A319132 · Airfoil Anti/De-ice SystemSDR GTIA201311091031Door · departedAIR RETURN DUE LOOSING RT ENGINE INBD AND OTBD COWLINGS, DECLARING EMERGENCY. LANDED SAFELY. INSPECTIONS REVEAL DAMAGES TO THE SECONDARY PYLON STRUCTURES AND IN THE VERTICAL L/E STABILIZER PANEL. REPAIR OF THE SECONDARY PYLON STRUCTURES IN PROCESS AND VERTINov 9, 2013 · N504NK · Airbus A319132 · Nacelle/Pylon, Main FrameSDR GTIA201310161005Engine · fireAIR RETURN DUE TO NR 1 ENGINE FIRE. ENGINE SHUTDOWN IN FLIGHT, SMOKE IN COCKPIT. NR 1 ENGINE CHANGED IAW AMM.Oct 15, 2013 · N516NK · Airbus A319132 · Engine (Turbine/Turboprop)SDR GTIA20131009994Connector · unsecureAFT CARGO DOOR OPEN WARNING IN FLT MAX CABIN PRESSURE CLIMB UP TO 500 FPM. IAW TSM 52-32-00-810-801-A. FOUND CONNECTOR TO PROXIMITY SENSOR 32WV UNSEATED. SECURED CONNECTOR, PERFORMED OPS CHECK OF CARGO DOOR AMM 52-30-00-860-001/52-30-00-860-002. OPS CHECKEOct 9, 2013 · N519NK · Airbus A319132 · Air Conditioning System WiringSDR USAA2013091300018Actuator · faultyENROUTE, CREW REPORTED AN ENGINE NR 2 COMPRESSOR VANE STALL. SHUTDOWN ENGINE, DECLARED AN EMERGENCY AND DIVERTED. MX R & R NR 2 ENGINE VSV ACTUATOR IAW AMM 75-32-41 AND COMPLETED BOROSCOPE OF HPC, LPC IAW 72-00-20-017 AND -016.Sep 10, 2013 · N817AW · Airbus A319132 · Compressor Bleed ValveSDR RJEF20130909007Unknown · odorON ARRIVAL, PILOT REPORTED THAT DURING DESCENT, "IN IDLE, SMELLED FUEL VAPORS", ACFT WAS HELD ON GROUND FOR MX. PERFORMED ANALISYS IAW "TSM 28-00-00-810-801-A, PERFORMED A VISUAL INSPECTION FOR ANY FUEL LEAKING EVIDENCE AT THE CENTER OF THE PASSENGER CABIN BSep 6, 2013 · N477TA · Airbus A319132 · Air Distribution SystemSDR USAA2013081600002Eec · faultyDURING CRUISE, STS PAGE SHOWED INOPERATIVE SYSTEMS REVERSER 2 AND ENG 2 THRUST. ENGINE PARAMETERS NORMAL WITH AUTO THRUST ENGAGED. AT LANDING, NR 2 THRUST REVERSER WORKED AND ENGINE RESPONDED NORMAL. AN EMERGENCY WAS DECLARED BY THE CAPTAIN. MX R & R THE NR Aug 14, 2013 · N819AW · Airbus A319132 · Fuel Controlling SystemSDR RJEF20130719003Outflow Valve · failedDURING CLIMBOUT, AN ECAM MESSAGE "VENT SKIN VALVE FAULT", ACFT RETURNED TO DEPARTURE. AFTER AN UNEVENTFUL LANDING AT DEPARTURE, MX PERFORMED FAULT ANALYSIS IAW TSM 21-26-00-810-804-A AND DETERMINED THAT THE CAUSE OF SUCH FAILURE IS THE SKIN AIR OULTLET VALVE.Jul 18, 2013 · N479TA · Airbus A319132 · Pressure Regulator/Outflow ValveSDR USAA2013060700004Uplock · faultyAFTER TAKEOFF, RETRACTED LANDING GEAR AND RECEIVED LANDING GEAR SYS DISAGREE. NOSE DOOR SHOWING NOT CLOSED. RECYCLED GEAR AND PROBLEM REPEATED. ON AIR TURNBACK, PROBLEM REPEATED AGAIN. FLIGHT LANDED WITHOUT INCIDENT. MX R & R NOSE DOOR UPLOCK REF 32-31-14Jun 6, 2013 · N806AW · Airbus A319132 · Landing Gear Retraction/Extension SystemSDR SOKF20130424002Thermocouple · erraticENGINE NR 1 EGT OVER LIMIT AFTER TAKEOFF, NO OVERWEIGH LANDING. ACCORDING TO TSM TASK CARD 77-00-00-810-817-B WAS REMOVED AND REPLACED THERMOCOUPLE NR 1, 2, 3, 4 AS PER AMM 77-21-43 PB 401 AND AMM 77-21-15 PB401. ADDITIONALLY BOROSCOPE INSPECTION WAS PERFORMApr 24, 2013 · N520TA · Airbus A319132 · Engine EGT/TIT Indicating SystemSDR RJEF2013032747901Sensor · faultyDURING THE TAKEOFF RUN OF FLIGHT LR691 FROM BOG TO BSB THE PILOT REPORTED THAT PFD1 INDICATES 15 KNOTS MORE THAN PFD2, DUE TO THAT REASON THE AIRCRAFT RETURNED TO THE GATE FOR MAINTENANCE. IN ORDER TO RETURN THE AIRCRAFT TO SERVICE PERFORMED A FAULT ISOLATIONMar 27, 2013 · N479TA · Airbus A319132 · Outside Air Temperature Indicator/SensorSDR USAA2013031100005Engine · overservicedCREW REPORTED A CHEMICAL ODOR IN CABIN WITH PACKS ON (AIRCRAFT PARKED AT GATE). SMOKE WAS ALSO PRESENT. MAINTENANCE ACCOMPLISHED JOB CARDS. FOUND NR 1 ENGINE OVERSERVICED. DRAINED 1 QUART OF OIL FROM NR 1 ENGINE. MAINTENANCE ALSO ACCOMPLISHED THE FOLLOWINMar 9, 2013 · N839AW · Airbus A319132 · Turbine Engine Oil SystemSDR USAA2013021900007Eec · faultyAPPROXIMATELY 30 MINUTES INTO FLIGHT, CREW REPORTED AN ENGINE 1 EPR MODE FAULT. FLIGHT RETURNED TO FIELD AT PHX AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. FADEC 1A FLT DATA "EPRINI" P/F P5/EEC1. INSPECTED NR 1 EPR TUBES FOR VISIBLE DAMAGE. NONFeb 17, 2013 · N802AW · Airbus A319132 · Fuel Control/Turbine EnginesSDR USAA2013020400023Oil System · overservicedCREW REPORTED ENGINE 1 OIL QUANTITY INDICATOR SHOWS XX. FLIGHT RETURNED TO FIELD AT PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED CONNECTOR WIRING AND PINS. NO DEFECTS NOTED. FOUND ENGINE 1 OVERSERVICED WITH OIL. REMOVED 2 GALLONS OF OIL. REMOVEFeb 3, 2013 · N827AW · Airbus A319132 · Turbine Engine Oil SystemSDR GTIA20130104518Engine · fluctuatesPOWER FLUCTUATION DURING TAKEOFF. DURING CLIMB AT F 50 ACFT SUDDENLY YAWED ENGINE NR 1 EPR DROPPED TO ZERO ALONG WITH N1 THEN RECOVERED IT APPEARS THE ENGINE LOST POWER THIS OCCURRED THREE TO FOUR TIMES THROUGH FL 70 WHERE DESCISION TO TURN BACK WAS MADE, DURJan 4, 2013 · N514NK · Airbus A319132 · Engine (Turbine/Turboprop)SDR USAA2012122100003Engine · malfunctionedON TAXI IN, CREW REPORTED A NR 1 ENGINE OVERTEMP AND AUTO SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW J/C 26L40071004. OPS GROUND CHECK IAW 26L00071015 GOOD AT THIS TIME.Dec 20, 2012 · N837AW · Airbus A319132 · Engine (Turbine/Turboprop)SDR GTIA20121129514Lamp · inoperativeEMERGENCY CEILING LAMP AT 9DEF INOPERATIVE. R & R EMERGENCY CEILING LAMP AT 9DEF. OPS CHECK OK IAW AMM 33-51-11-000-001 AND 33-51-11-400-001.Nov 29, 2012 · N531NK · Airbus A319132 · Emergency LightingSDR GTIA20121126513Cylinder · low pressureL2 PAX DOOR LOW PRESSURE. SERVICED L2 PAX DOOR TO PROPER PRESSURE IAW AMM 52-10-00-614-001.Nov 26, 2012 · N512NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121124512Cylinder · low pressureR2 DOOR ASSIST BOTTLE RES READING 1100 PSI. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-PB 301. SERVICED TO 1750 PSI.Nov 24, 2012 · N532NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121115510Cylinder · low pressureR2 DOOR ASSIST CYLINDER AT 1650 PSIG AT 20C. SERVICED CYLINDER IAW AMM 52-10-00-614-001-A. LEAK CHECKED GOOD.Nov 15, 2012 · N533NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121113509Slide · failedON FAP AFTER WHEELS UP "CHECK SLIDE PRESSURE ON OVERWING EXIT RT SIDE DOOR IS ALSO AMBER. R & R INFLATION RESERVOIR OFFWING SLIDE RT IAW AMM 25-62-46-000-001A/25-62-46-400-001A. OPS TEST OK.Nov 13, 2012 · N531NK · Airbus A319132 · Escape SlideSDR RJEF2012111347901Computer · malfunctionedDURING FLIGHT TAI-457 FROM SAL TO UIO, THE PILOT IN COMMAND REPORTED: "NAV GPWS TERRAIN DETECTION FAULT, NO OVERWEIGHT LANDING", THEREFORE, THE FLIGHT ATB. ONCE THE AIRCRAFT WAS POSITIONED AT THE MAINTENANCE RAMP, AND AS PER TSM 34-38-00-810-825-A, THE GPWC WNov 13, 2012 · N479TA · Airbus A319132 · Ground Proximity SystemSDR USAA2012111400020Blade · damagedBIRD STRIKE SHORTLY AFTER GEAR RETRACTION. LOUD BUZZING FROM NR 2 ENGINE THAT BENT 4 BLADES ON THE N1 FAN. ENGINE DID NOT SHUTDOWN. PERFORMED BIRD STRIKE INSPECTION - REMOVED AND REPLACED A FULL SHIP SET OF FAN BLADES AND ANNULUS FILLERS PER 72-31-11-000-01Nov 4, 2012 · N826AW · Airbus A319132 · Turbine Engine Compressor SectionSDR GTIA20121102505Diaphragm · puncturedR2 DOOR CYLINDER DAMPER DIAPHRAGM PUNCTURED. REPLACED R2 DOOR CYLINDER DAMPER DIAPHRAGM IAW AMM TASK 52-10-00-610-001-A.Nov 2, 2012 · N534NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121102506Bottle · dischargedR2 DOOR EMERGENCY ASSIST DAMPER NITROGEN BOTTLE NEEDS TO BE SERVICED. SERVICED WITH FLL NITROGEN TO CORRECT PRESSURE R2 DOOR ASSIST DAMPER NITROGEN BOTTLE IAW AMM TASK 52-10-00-614-001-A.Nov 2, 2012 · N534NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121031504Bottle · low pressureRT AFT DOOR EMERGENCY BOTTLE LOW. SERVICED DOOR EMERGENCY BOTTLE RT AFT IAW AMM 52-10-00-614-001-A.Oct 31, 2012 · N502NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121030503Lamp · inoperativeWHILE PERF STOP C 33-51-00-710-001A. R & R OWL SLIDE. RECEIVED FAULT (ESCAPE SLIDE LT/ EPSU (12WL). LAMPED RT EMERGENCY OVERWING LIGHT IAW AMM 33-51-PB401. OPS CHECK GOOD PASED EPSU SYS TEST 33-51-00-710-001A TEST.Oct 30, 2012 · N532NK · Airbus A319132 · Emergency LightingSDR GTIA20121029500Cylinder · low pressureL1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED L1 DOOR PAMBER/EMERGENCY OPERATION CYLINDER IAW AMM 52-10-00-614-051-A. NO LEAKS NOTED.Oct 29, 2012 · N516NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121029501Cylinder · low pressureFOUND R2 DOOR, DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-22-00-614-002.Oct 29, 2012 · N534NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121026499Control Unit · failedNR 2 THRUST LEVER DISAGREE POSITION. R & R THROTTLE CONTROL UNIT IAW AMM 76-11-19-000-041A. OPS CHECKED IAW AMM 76-11-00-710-040-A. OPS CHECKED OK.Oct 26, 2012 · N534NK · Airbus A319132 · Power LeverSDR GTIA20121025498Eec · failedNR 2 ENGINE THROTTLE SETTING ERRATIC. PULLED BACK TO FLIGHT IDLE. NR 1 MAINTAINED FULL POWER. CREW ADVISED THEY ARE UNABLE FLL AND DIVERTED. DECLARED AN EMERGENCY. R & R EEC NR 2 IAW AMM 73-22-34-000-010-A & 73-22-34-400-010-A. OPS CHECKED OK.Oct 25, 2012 · N534NK · Airbus A319132 · Fuel Controlling SystemSDR GTIA20121024496Cylinder · low pressureR1 DOOR PSI (PASSENGER-ASSIST CYLINDER) APPROX 1100 PSI REQ'S SERVICING. SERVICED R1 DOOR ASSIST CYLINDER W/ NITROGEN TO REQ'D LEVEL IAW AMM 52-10-00-614-001-A. LEAK CK OK AT THIS TIME.Oct 24, 2012 · N506NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121024497Cylinder · low pressureL-1 DOOR ASSIST ACTUATOR PRESSURE LOW. CORRECTIVE ACTION: REMOVED AND REPLACED L-1 DOOR CYLINDER DAMPER IAW AMM 52-11-14-000-001-B/52-11-14-400-001-B OPERATIONAL CHECK NORMALOct 24, 2012 · N506NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121017495Cylinder · low pressureL1 DOOR ASSIST LOW . SERVICED L1 DOOR ASSIST IAW AMM 52-10-00-614-001-A.Oct 17, 2012 · N522NK · Airbus A319132 · Passenger/Crew DoorsSDR EE4Y2012101100295Attach Fitting · wornDURING STRUCTURE INSPECTION, FOUND THE LT WING AILERON INBD SERVO CONTROL ATTACH FITTING WORN.Oct 11, 2012 · N527NK · Airbus A319132 · AileronsSDR GTIA20121010493Cylinder · low pressureL1 DOOR LOW ACCUMULATOR DOOR PRESSURE. SERVICED L1 DOOR CYLINDER IAW AMM 52-10-00-614-001-A TO PROPER LEVEL.Oct 10, 2012 · N531NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20121010494Cylinder · low pressureR2 DOOR DAMPER CYLINDER PRESSURE LOW. SERVICED R2 DOOR DAMPER CYLINDER IAW AMM 52-10-00-614-050-A. LEAK CHECKS GOOD.Oct 10, 2012 · N532NK · Airbus A319132 · Service DoorsSDR EE4Y2012100900293Fitting · corrodedDURING INSPECTION, FOUND THE RT AND LT MLG RETRACTION JACK ANCHORAGE FITTING CORRODED. THE FITTING WAS REPAIRED IAW 70567813/007.Oct 9, 2012 · N527NK · Airbus A319132 · Wing, Attach FittingsSDR EE4Y2012101000294Skin · corrodedDURING INSPECTION, FOUND VERTICAL STABILIZER, RUDDER RT EXTERNAL SKIN BULGED AT NR 7 POSITION HINGE. THE SKIN WAS REPAIRED IAW 70567897/006 .Oct 2, 2012 · N527NK · Airbus A319132 · Rudder, Plate/SkinSDR GTIA20121001489Latch · lack of lubeL2 DOOR WILL NOT LATCH TO OPEN POSITION. LUBRICATED DOOR GUST LOCK. PERFORMED OPS CHECK IAW AMM 52-10-00-010-001 AND 52-10-00-410-001. OPS CHECKED OK, NO DEFECTS.Oct 1, 2012 · N523NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20120928491Skin · corrodedRT WING LOWER SURFACE BETWEEN RIBS 25-&26 HAS CORROSION DAMAGE. PERFORMED PERMANENT BLEND OUT REPAIR OF CORROSION DAMAGE IAW EA 57-20-1219 REV ORIGINAL DATE 9-26-2012.Sep 28, 2012 · N503NK · Airbus A319132 · Wing, Plate/SkinSDR GTIA20120926487Epsu · failedPFR SHOWS EPSU FWD LIGHT. R & R EPSU (10WL) IAW AMM 33-51-38-000-001/400-001. OPS CHECKED GOOD IAW AMM 33-51-38-710-052-B.Sep 26, 2012 · N504NK · Airbus A319132 · Emergency LightingSDR GTIA20120923485Cylinder · low pressureR2 DOOR ASSIST BOTTLE AT 1550 PSIG. SERVICED IAW AMM 52-10-00-614-050-A. NO LEAKS NOTED. ACFT OK FOR SERVICE.Sep 23, 2012 · N526NK · Airbus A319132 · Passenger/Crew DoorsSDR GTIA20120923486Bottle · low pressureCIDS MESSAGE FAULT, FWD F/A PANEL CHECK SLIDE PRESSURE RT INDICATING EMERGENCY ROW. FOUND PRESSURE ON BOTTLE ON LOW SIDE. R & R RESERVOIR (7507MM) RT IAW AMM 25-62-46-000-001-A/25-62-46-400-001-A. OPS CK GOOD.Sep 23, 2012 · N522NK · Airbus A319132 · Escape SlideSDR EE4Y2012092000286Rudder · contaminatedVERTICAL STABILIZER RUDDER HOISTING POINTS 1LT, 2LT, 3LT AND 3RT WITH TRAPPED FLUID. DAMAGED AREAS WERE REPAIRED IAW MESSAGE 70567288/006 DTD SEP 19, 2012 AND TD-K4-S2-39630-2012, ISSUE A, UNDER THE NON ROUTINE ITEM, WO: A1A232, SUBJOB: 3, ITEM: 1.Sep 16, 2012 · N503NK · Airbus A319132 · Rudder Structure
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