IAE V2522-A5
Service difficulty reports · 3,465
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 = 'V2522A5' 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.
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 = 'V2522A5' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2005UALA01167Warning Flag · illuminatedEXCESS CABIN ALT DISPLAYED ON UPPER ECAM SCREEN. CABIN ALTITUDE CLIMBED TO 10400 MSL. AIRCRAFT DESCENDED AND CABIN ALTITUDE CONTROLLER RETURNED TO NORMAL. NO FAULTS ON PFR. ACCOMPLISHED PRESSURE MONITOR AND CONTROL TEST PER MM 21-31-00, OP CHECK GOOD. FSDR 2005UALA01135Light · missingRED EEL LIGHT ASSY MISSING AT FWD CLOSET. REPLACED RED LIGHT ASSY.SDR 2005UALA01073Skin · bird strikeBIRD STRIKE DAMAGE AT FRAME 5 AT TO TOP OF RVSM AREA. *S/D* INST REPAIR DOUBLERS AND FRAME FLANGES PER SRM 53-11-11 AND UA-EVA-50672.SDR 2005UALA01050Mount Bracket · brokenDOOR 1L SLIDE AFT LWR MOUNT BRACKET BROKEN. THE STEP BRACKETS OF SLIDE (LH & RH) ARE THE TWO BOTTOM ATTACHMENT POINTS THAT HOLD THE SLIDE ASSEMBLY ONTO THE AIRCRAFT DOOR. THESE PARTS ARE STICKING OUT OF THE WHOLE ASSEMBLY AND ARE LIABLE TO DAMAGE ESPECIALLY SDR 2005UALA01012A/C Pack · inoperativeWHILE AT FL310, A/C EXPERIENCED SLOW DEPRESSURIZATION. NR 1 PACK WAS INOP. NR 2 PACK WAS ON HIGH. EMERGENCY DESCENT TO FL160. CHECKED CABIN PRESSURE CONTROLLER AND BLEED MONITORING COMPUTER, CHECKED OK. PERFORMED PRESSURE CHECK OF LEFT AND RIGHT PACKS ANDSDR 2005UALA01001Battery Pack · inoperativeCABIN EMERGENCY LIGHT TEST FAILS: EPSU INT LOADS AFT L AND EPSU BATTERY R. REPLACED AFT EPSU 13WL PER MM 33-51-38 AND BATTERY PACK FOR RIGHT MID POWER SUPPLY.SDR 2005UALA00989Warning Light · illuminatedCREW REPORTS SMOKE WARNING FOR AFT CARGO PIT. NTERROGATED SYSTEM AND UNABLE TO VERIFY FAULT FOR AFT CARGO COMPARTMENT SMOKE DETECTION. REPLACED SDU PER AMM 26-17-34. REPLACED AFT CARGO COMPARTMENT SMOKE DETECTOR PER AMM 26-16-15. REPLACED AFT CARGO FIRE SDR 2005UALA00980Oven · smokeF/A REPORTS SMOKE COMING OUT OF OVEN. SECURED IT AND DIVERTING FLIGHT. INITIAL INSPECTION REVEALED A DIRTY FILM ON INTERIOR OF OVEN WITH A DISTINCT ODOR THAT COULD HAVE CAUSED "SMOKING" CONDITION. THE OVEN WAS INSPECTED AND CHECKED/TESTED PER MANUFACTURER'SSDR 2005UALA00951Power Supply · failedFWD LT EMERGENCY POWER SUPPLY AND BATTERY FAILS TEST. REPLACED POWER SUPPLY AND BATTERY.SDR 2005UALA00940Battery · failedEMERGENCY LIGHT TEST FAILS. GRIPES 'EPSU AFT L'. REPLACED AFT LEFT BATTERY.SDR 2005UALA00929Lever · failedUNABLE TO RETRACT LANDING GEAR. ON TAKE OFF LANDING GEAR HANDLE WOULDN`T MOVE, GEAR STAYED DOWN. LANDING WT-140.8+SINK RATE-100FPM. REPLACED LANDING GEAR LEVER PER MM- 32-31-11, TESTS GOOD.SDR 2005UALA00939Battery · failedCABIN EMERGENCY LIGHT TEST FAILED WITH MESSAGE: EPSU INT LOAD EMER L. REPLACED BATTERY 11WL.SDR 2005UALA00928Fan · failedRETURN TO FIELD DUE TO AN EXTRACT FAN FAULT. ECAM EXTRACT FAN FAULT DISPLAYED AFTER TAKEOFF. REPLACED BLOWER FAN AND AVIONICS FILTER. OPS. TEST PER 21-26-00. OPS CHECKS GOOD.SDR 2005UALA00922Battery · failedFWD EMERGENCY BATTERY FAILED 3SVC CK. REPLACED FWD EMERGENCY LIGHT BATTERY.SDR 2005UALA00924Window · crackedFIRST OFFICER'S FWD OUTER PANE WINDOW CRACKED. REPLACED RT WINDSHIELD REF MM56-11-11. ALSO REPLACED RT WINDOW HEAT CONTROLLER.SDR 2005UALA00921Battery Pack · dischargedLT FWD EMERG LIGHT BATTERY PACK LOW. FAILED 3SVC LIGHT TEST. REPLACED FWD EMERG LIGHT BATTERY.SDR 2005UALA00740Epsu · faultyEMERGENCY LIGHT TEST FAULTED. REPLACED EPSU.SDR 2005UALA00733Bottle · lowESCAPE SLIDE HAS LOW BOTTLE PRESSURE. SLIDES BEING REMOVED DUE TO LOW BOTTLE PRESSURE IS NOT TOTALLY AN UNCOMMON EVENT. THE OPERATING ENVIRONMENT OF SLIDES (VIBRATION, DOOR OPENING/CLOSING, CARTS IMPACTING DOORS, TEMPERATURE & PRESSURE CHANGES) ARE AMONG TSDR 2005UALA00730Pin · bentCREW REPORTED R ENGINE OVERTEMP. THE 2.5 BLEED VALVE MASTER ACTUATOR WAS FOUND TO HAVE A BENT CONNECTOR PIN. THIS DEFECT LEAD TO THE 2.5 BLEED VALVE BEING INTERMITTENTLY SET TO THE FAIL-SAFE (OPEN) POSITION LEADING TO AN EGT OVER-TEMP.SDR 2005UALA00743Steering Sys · inoperativeON ROLLOUT GOT LANDING GEAR NOT DOWN ECAM , THEN GOT NW STEER FAULT. NWS DID NOT WORK.SDR 2005UALA00690Motor · failedRETURN TO FIELD WITH A BLUE HYDRAULIC OVERHEAT INDICATION. BLUE HYD ELECT OVERHEAT. SHUTDOWN BLUE PUMP. WARNING CLEARED AFTER 5 MINS. CYCLED CB C12 PER SAMC AND RESTARTED BLUE PUMP. FAULT THEN RETURNED. QTY NORMAL. PUMP JUST REPLACED DUE TO POPPED CB ABSDR 2005UALA00671Epsu · failed"INTERNAL LOAD FAULT FWD L" DISPLAYED ON PTP DURING EMER LIGHT SYS TEST. SWAPPED FWD AND AFT EPSU'S AND ALL TESTED OK. INTERNAL LOAD FAULTS WILL APPEAR IF THE LOAD ON THE EPSU IS DIFFERENT THAN WHAT THE UNIT "LEARNED" AT IT'S ORIGINAL LOCATION DURING "TEACH-SDR 2005UALA00668Bottle · dischargedDOOR 2L PRESSURE LOW. SERVICED DOOR CYLINDER TO 1800 PSI. NO HISTORY EXCEPT ROUTINE SERVICING AT A-CHECK.SDR 2005UALA00729Warning Light · illuminatedLOST GREEN SYSTEM HYDRAULIC QTY INDICATION. CREW HAS SHUTDOWN EDP AND PTU. WILL REQUIRE TOW OFF RUNWAY. GREEN HYD QTY LOSS, CREW HAS SHUTDOWN EDP AND PTU. NO SIGNS TH AT PUMP WAS RUN DRY. WILL REQUIRE TOW OFF RUNWAY. INDLM/AFTER MEETING ACFT ON RUNW AY FOSDR 2005UALA00626Slide · lowDOOR 1L SLIDE PRESS JUST OUTSIDE GREEN ARC. SLIDES BEING REMOVED DUE TO LOW BOTTLE PRESSURE IS NOT TOTALLY AN UNCOMMON EVENT. THE OPERATING ENVIRONMENT OF SLIDES (VIBRATION, DOOR OPENING/CLOSING, CARTS IMPACTING DOORS, TEMPERATURE & PRESSURE CHANGES) ARESDR 2005UALA00617Bulkhead · cutDAMAGE CUT THROUGH SKIN FWD OF PRESSURE BULKHEAD APPROX 6 INCHES LONG AND 8-9 INCHES WIDE. INSTALLED DOUBLER REPAIR AND SPLICED STRINGER SECTION REF UA EVA-50432 AND SRM53-00-11 FI G 227.SDR 2005UALA00594Door · openPILOTS REPORTED LT OVERWING DOOR OPEN ECAM MESSAGE. LATCH COVER (PLASTIC PART) FELL OFF IN FLIGHT (REMOVED?). PART SHOULD HAVE BEEN REINSTALLED AND WARNING WOULD HAVE GONE OUT. COVER HAS PROXIMITY SWITCH TO ENSURE CLOSED. THIS PROXIMITY SWITCH, IN ADDITIONSDR 2005UALA00595Wire · chafedLOST NR 2 GENERATOR AND APU AUTO SHUTDOWN. REPAIRED 4 CHAFED WIRES BEHIND NR 2 GCU BENCH PLUG, LOCATED AT FIRST TIE WRAP.SDR 2005UALA00571Connector · looseAFT CARGO DOOR OPEN DISPLAYED ON UPPER ECAM SCREEN. CONNECTOR TO 32WV PROXIMITY SENSOR CAME LOOSE. COA 404692 WAS PERFORMED INCORRECTLY. FIRST INCIDENT SINCE INCORPORATION IN MAY 2004. EG4352.SDR 2005UALA00541Clamp · failedNR 2 ENGINE BLEED FAULT. RIGHT WING BLEED LEAK DISPLAYED AFTER TAKEOFF. FOUND LEAK ABOVE NR 2 ENG PYLON AT DUCT CLAMP (REF IPC 36-11-05 FIG 02 ITEM 20). REPLACED CLAMP. LEAK WAS 2 INCHES IN FRONT OF RT WING LOOP -A- ELEMENTS 43HF AND 44HF.SDR 2005UALA00540Fan · failedCREW REPORTED SMOKE IN FLIGHT DECK. REPLACED THE AVIONICS BLOWER FAN. TESTED OK. REPLACED THE AVIONICS BLOWER FAN. TESTED OK.SDR 2005UALA00539A/C Pack · failedECAM NR 1 ENG EIU DISPLAYED DURING CRUISE. LOST BOTH AIR CONDITIONING PACKS. EIU REMOVED TO SFO HOME SHOP. UNIT TESTED NO FAULTS FOUND. CCOA 0-4499 ACCOMPLISHED 1/29/2004 PER SB 395798-73-004 AS RECOMMENDED BY AIRBUS TFU 73.25.00.019. FLEET ENGINEERING SETTISDR 2005UALA00498Epsu · dischargedEEL LIGHTS INOPERABLE AT ROWS 15,16,19, 20, 23 & 24. THE EMERGENCY POWER SUPPLY UNIT (EPSU) WAS REPLACED AT DOOR 2R.SDR 2005UALA00443Engine · flamed outNR 1 ENGINE FLAMED OUT AT FL360. ALL PARAMETERS ROLLED BACK TOGETHER. RESTARTED AT FL 200. THE PMA S/N FAAG6915FL03 ARRIVED AT SFOEP ON 5/26/2005. THE PMA SHAFT WAS IN ONE PIECE, THE NUT P/N NAS1291C7 WAS STILL IN PLACE, HOWEVER, P/N 4B0286 HAD A FREE RUNSDR 2005UALA00448Slide · damagedSLIDE HAD BEEN DEPLOYED CAUSING HOLES IN INFLATION TUBE AND HEAVY SEAM DEGRADATION. PROBABLE CAUSE OF HOLES IN THE INFLATABLE IS FOREIGN OBJECT DAMAGE (FOD) DURING DEPLOYMENT OR PERHAPS DUE TO HANDLING DURING TRANSPORTATION. SINCE THE DAMAGE WAS BEYOND THE CSDR 2005UALA00409Fan · failedFUMES IN COCKPIT WITH VIBRATIONS. REPLACED THE AVIONICS BLOWER FAN. TESTED OK.SDR 2005UALA00366Proximity Sensor · disconnectedFWD CARGO DOOR OPEN INDICATED ON ECAM. CONNECTOR CAME OFF OF THE PROXIMITY SENSOR 28WV. REINSTALLED CONNECTOR ON THE DOOR PROXIMITY SENSOR.SDR 2005UALA00340Proximity Sensor · failedGEAR NOT DOWN AND LOCKED ECAM DISPLAYED. MANUAL EXTENSION WAS SUCCESSFUL. FAULTY SENSOR FIN 34GA. GEAR EXTENDED MANUALLY. REPLACED PROX SENSOR 34GA.SDR 2005UALA00316Fairing · contaminatedSMOKE NOTICED EMANATING FROM LEFT WING AREA. INSPECTED LT IB FLAP TRACK FAIRING. FOUND NO SIGNS OF HYD LEAKS. HYD QTY CHECKED OK. RAN NR 1 ENGINE AND OPERATED FLAPS. ALL OPS NORMAL NO SMOKE OR VAPORS FOUND. FLIGHT CREW REPORTED THAT IT HAD RAINED HARD IN GSDR 2005UALA00265Warning Light · malfunctionedENGINE 2 PUMP LO PRESSURE DISPLAYED ON UPPER ECAM. REPLACED NR 2 ENG. HYDRAULIC PRESS. SWITCH, RAN ENG. LEAK CHECKS GOOD.SDR 2005UALA00304Cell · separatedAFTER INFLATION AND PRESSURIZING TO 2.5 PSI FOR AR, CHAMBERS SEPARATED. ADHESIVE FAILURE, RESULTED IN AIR CHAMBERS TO SEPARATE DURING PRESSURIZATION OF ASSEMBLY. UNIT WAS SENT TO OEM FOR REPAIR/DISPOSITION.SDR 2005UALA00068Odor · detectedELECTRICAL SMELL OBSERVED IN THE FLIGHT DECK. NSPECTED GALLEY AREAS AS WELL AS AVIONICS COOLING FANS. FLIGHT CREW HAD NO OTHER ABNORMAL INDICATIONS OR SYSTEM MALFUNCTIONS. ACCOMPLISHED POWER RUNS AND REPLACED AEVC FILTER CARTRIDGE AS PRECAUTINARY MEASURES. NOSDR 2004UALA01242Computer · malfunctionedALL FMGC 1 FUNCTIONS LOST. AUTOPILOTS DISENGAGED. SUPPLEMENTAL DATA UPDATE FMGC 1 WAS FAULTED BY THE CFDS TEST. REPLACED THE NR 1 FMGC. SHOP TEST FOUND SOLDER CRACKS ON THE U10 OF A51 CARD.SDR 2004UALA01233Pump · leakingGREEN SYSTEM LOW LEVEL ECAM MSG AND ECAM SHOWING LOW LEVEL. AMBER ALERT DECLARED. FOUND NR 1 ENG EDP HYD PUMP LEAKING, REPLACED EDP PUMP AND REPLACED CASE DRAIN FILTER.SDR 2004UALA01177Light · damagedDURING OVERHAUL EMERGENCY EXIT SLIDE LIGHT WERE FOUND TO BE DAMAGED. SUPPLEMENTAL DATA UPDATE THE LIGHT ASSEMBLY WAS REPLACED.SDR 2004UALA01152Bolt · misalignedAFTER DIFFICULTY RAISING GEAR HANDLE, GEAR DID NOT INDICATE RETRACTED. LOUD AIR NOISE FURTHER INDICATED THAT GEAR WAS NOT UP. MLG SHOCK ABSORBER MESSAGE DISPLAYED. AIRCRAFT ARRIVED WITH LARGE AMOUNT OF ICE ON NLG AND SENSORS. CFDS SHOWS NLG FAULTS. CLEANESDR 2004UALA01148Blade · crackedNR 2 ENGINE COMPRESSOR STALL AND SHUTDOWN ON DECENT. THIRD STAGE COMPRESSOR BLADE FAILED. BLADE RE-DESIGN IS IN PROCESS TO ADDRESS THIS PROBLEM.SDR 2004UALA01140O-Ring · leakingYELLOW SYSTEM LOW LEVEL ECAM MESSAGE. CREW FOLLOWED ECAM, EDP SELECTED OFF. YELLOW SYSTEM PRESSURE ZERO, WITH QUANTITY IN AMBER ZONE. REPLACED O-RING ON YELLOW SYSTEM MANIFOLD.SDR 2004UALA01028Spoiler · vibrationNR 2 SPOILERS APPEAR TO BE FULLY UP INTO THE AIRSTREAM CAUSING AIRFRAME VIBRATION DURING FLIGHT. THE LT AND RT NR 2 SPOILER SERVO CONTROLS WERE PREVIOUSLY DEFERRED. DEFERRAL PROCEDURE USING A SPECIAL MAINTENANCE KEY FOR SPOILER DEACTIVATION WAS FOUND NOT CORRSDR 2004UALA01026Tape · separatedSLIDE RAMP HINGE TAPE SEPARATED DURING OVER PRESSURE TEST. THE TAPE SEPARATION COULD BE ATTRIBUTED TO ADHESIVE FAILURE. THE UNIT WAS SENT TO OEM (AIRCRUISERS) FOR REPAIR.
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