IAE V2527-A5

Service difficulty reports · 8,011

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 = 'V2527A5'
  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 2006UALA01331Slide · faultyCABIN EMERGENCY LTS FAILED TEST IND EPSU EXT LOAD AFT L. TROUBLE SHOT SYSTEM. 2L SLIDE REPLACED PER MM 25-23-45.Jul 5, 2006 · N491UA · Airbus A320232 · Escape SlideSDR 2006UALA01312Cabin Pressure · failedFLIGHT DIVERTED DUE TO LOSS OF CABIN PRESSURIZATION. AIRCRAFT TYPE I FERRIED FROM LAX TO SFO FOR REPAIR BY SFOMM. THIS WAS A DIAGNOSTIC TEST FLT WITH A MAX ALT OF FL230. AIRCRAFT DID NOT HOLD PRESSURE ON FERRY FLIGHT WITH OUTFLOW VALVE FULL CLOSED AT FL220. Jul 4, 2006 · N465UA · Airbus A320232 · Cabin Pressure Control SystemSDR 2006UALA01311Hydraulic System · reads lowRETURN TO FIELD DUE TO ALL HYDRAULIC QUANTITY INDICATIONS SHOWING ZERO. FOUND NO POWER AT 1834GQ IND RSVR HYD QTY AT REFILL BAY. CHECKED FOR 26VAC AT CIRCUIT BREAKER 1831GQ, NO POWER. FOUND CIRCUIT BREAKER 5XN1 BUS 1-131XP A SUPPLY POPPED ON 123VU. RESET BJul 3, 2006 · N439UA · Airbus A320232 · Hydraulic System, MainSDR 2006UALA01313Frame · damagedFOUND FRAME NR 6 IS DAMAGED AT LOWER CTR BTWN E/E DOOR AND POWER PANEL. REPLACED FRAME NR 6 PER SRM 53-11-12 FIG201. THIS IS A INTERIM REPAIR & MAY BE UPGRADED TO A PERMANENT REPAIR WITH SUPPLEMENTAL INSPECTIONS FOLLOWING DAMAGE TOLERANCE ANALYSIS. INSPECTEJul 3, 2006 · N461UA · Airbus A320232 · Fuselage Main, FrameSDR 2006UALA01314Skin · damagedFOUND FUSELAGE DAMAGE IN NOSE AREA AFT OF THE E/E DOOR FROM RAMP TRACTOR. HIT ANTENNA AND EXTERNAL POWER DOOR. INSTALLED DOUBLER PER SRM 53-00-11 FIG205. INTERIM REPAIR & MAY BE UPGRADED WITH SUPPLEMENTAL INSPECTIONS FOLLOWING DAMAGE TOLERANCE ANALYSIS. ACCJul 3, 2006 · N461UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2006UALA01332Light · inoperativeFOUND EMERGENCY LIGHT INOP AT SEAT 26C. REPLACED LIGHT ASSEMBLY, OPS CHECKS OK.Jul 3, 2006 · N431UA · Airbus A320232 · Emergency LightingSDR 2006UALA01333Light · inoperativeFOUND EMERGENCY LIGHT INOP AT SEAT 8C. REPLACED WIRE ASSEMBLY FROM SEAT ELECTRONIC BOX TO LIGHT ASSEMBLY, ALSO REPLACED LIGHT ASSEMBLY REF MM 33-51-19, OPS CHECK OK.Jul 3, 2006 · N431UA · Airbus A320232 · Emergency LightingSDR 2006UALA01334Charger · faultyDURING 3 SVC, FOUND EMERGENCY LIGHTS FAULTED INTERNAL. REPLACED FWD LEFT CHARGER, EMERGENCY TEST CHECKS OK.Jul 3, 2006 · N471UA · Airbus A320232 · Emergency LightingSDR 2006UALA01294Handle · failedDOOR 2R ARMING HANDLE RAISED UP APPROX ONE QUARTER OF TRAVEL IN FLIGHT AND SLIDE DISARMED INDICATION APPEARED MOMENTARILY. ADJUSTED DOOR 2R PROXIMITY SWITCH FIN NUMBER 7WN2 ARM DISARM AMM-52-71-00-820-002-01.Jul 2, 2006 · N430UA · Airbus A320232 · Escape SlideSDR 2006UALA01292Girt Bar · misinstalledDOOR 2 RT WILL NOT ARM. FOUND GIRT BAR FWD FLOOR MOUNT PLATE INSTALLED WITH TO MUCH SEALANT AFFECTING THE NORMAL HEIGHT OF GIRT BAR FLOOR MOUNT. REPOSITIONED FLOOR PLATE AND SEALED. OPS CHECKED GOOD.Jul 1, 2006 · N477UA · Airbus A320232 · Escape SlideSDR 2006UALA01293Warning Light · false activationON DESCENT INTO ORD, NR 1 ENGINE FIRE INDICATION LIGHT CAME ON FOLLOWED BY NR 2 ENGINE FIRE LIGHT. NR 1 ENGINE FIRE LIGHT WENT OUT. REPLACE NR 2 FDU PER AMM26-12-34, REF TSM 26-21-00-810-820.Jul 1, 2006 · N416UA · Airbus A320232 · Fire DetectionSDR 2006UALA01296Wire · burnedFOUND BURNED FEEDER WIRE. TERMINAL ON R3782 AND/OR HARNESS ON R4388. REPLACED APU GENERATOR REF MM 24-23-51.Jun 30, 2006 · N483UA · Airbus A320232 · Electrical Power System WiringSDR 2006UALA01277Battery Pack · dischargedLEFT EMERGENCY EXIT EMERGENCY LIGHT BATTERY INOPERATIVE. REPLACED LEFT EMERGENCY EXIT EMERGENCY LIGHT BATTERY.Jun 29, 2006 · N425UA · Airbus A320232 · Emergency LightingSDR 2006UALA01278Slide · failedDOOR 1R SLIDE FAILS EXT LOADS TEST IN EMERGENCY LIGHTS TEST. REPLACED SLIDE 1R PER AMM 25-62-44.Jun 29, 2006 · N428UA · Airbus A320232 · Escape SlideSDR 2006UALA01263Warning System · activatedRETURNED TO FIELD WITH NR 1 ENG BLEED FAULT MESSAGE. REPLACED BLEED PRESSURE REGULATOR VALVE PER AMM 36-11-52-000-010, OPERATIONAL CHECK OKAY.Jun 27, 2006 · N427UA · Airbus A320232 · Pneumatic Indicating SystemSDR 2006UALA01276Light · inoperativeEMERGENCY PATH LIGHTING IS INOP AT OVER WING EXT AND ALSO THE EXIT SIGNS ARE INOPERATIVE. REPLACED BATTERY CHARGER GROUND CHECKS NORMALJun 27, 2006 · N402UA · Airbus A320232 · Emergency LightingSDR 2006UALA01213Support · brokenCABIN - FWD RT PAX DR, EMERGENCY SLIDE FWD SUPPORT LUG BROKEN. FWD FLANGE BROKEN THROUGH PIN SUPPORT HOLE. AFT FLANGE BROKEN OFF AT BASE OF FLANGE. THIS OCCURRENCE ATTRIBUTED TO FAILURE OF ONE OF THE COMPONENTS SUPPORTING THE SLIDE, CAUSING A CHAIN OF ATTACJun 20, 2006 · N489UA · Airbus A320232 · Escape SlideSDR 2006UALA01202Power Supply · failedEMERGENCY LIGHT TEST FAILS. REPLACED 1L FORWARD EPSU, CHECKS OK.Jun 19, 2006 · N442UA · Airbus A320232 · Emergency LightingSDR 2006UALA01204Blades · damagedABORTED TAKEOFF FOR COMPRESSOR STALL AT 100-110 KTS. ALL INDICATIONS NORMAL UP TO THAT POINT. STOPPED THE ACFT WITH TWO BLOWN TIRES. NO INJURIES. BOROSCOPE INSPECTION FOUND 2 BLADES DAMAGED WITH PARTS OF THE MIDSPAN SHROUD MISSING, 1 ALSO HAS LEADING DAMAJun 19, 2006 · N467UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2006UALA01191Electrical Sys · multiple failRETURNED TO FIELD WITH MULTIPLE ELECTRICAL FAILURES. CONFIRMED PULLING CB 1PH CAUSES OTHER FAULTS. RAN WIRES AND REPLACED RELAYS 6XB [E0217XXY0080A], 21XE [E0245-28A0], 8PH [630CC01Y1] & 31XE [E0242A28A0]. CONDITION BEHIND 106VU LOOKED GOOD. RESISTER 32XE, Jun 18, 2006 · N445UA · Airbus A320232 · Electrical Power SystemSDR 2006UALA01200Battery · failedEMERGENCY LIGHT TEST FAILED. REPLACED LEFT MID EMERGENCY BATTERY, OF THE EPSU. OPS CHECK GOOD.Jun 16, 2006 · N409UA · Airbus A320232 · Emergency LightingSDR 2006UALA01201Battery · failedEMERGENCY LIGHT TEST GIVES MESSAGE OF "EMER COM RT". REPLACED BATTERY, CHECKS OK.Jun 16, 2006 · N425UA · Airbus A320232 · Emergency LightingSDR 2006UALA01199Power Supply · inoperativeLT AFT EMERGENCY ERROR MESSAGE DURING EMERGENCY LIGHT TEST. REPLACED LT AFT EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY. OPS CHECKS GOOD.Jun 13, 2006 · N415UA · Airbus A320232 · Emergency LightingSDR 2006UALA01152Structure · vibrationDIVERTED DUE TO AIRFRAME VIBRATION.Jun 12, 2006 · N432UA · Airbus A320232 · Fuselage Main, StructureSDR 2006UALA01129A/C Pack · malfunctionedLOST BOTH PACKS, FLIGHT DIVERTED. FOUND AIR LEAK AT RT WING LEADING EDGE, AT THE DUCT CONNECTION BETWEEN TRACK 2 AND 3. THERE WAS EVIDENCE OF BURN MARKS AT JOINT. REPLACED 4 SEALS FROM PNEUMATIC DUCTING LEADING TO AFT OF NR 1 PYLON HEAT EXCHANGER. REPLACED Jun 11, 2006 · N491UA · Airbus A320232 · Cabin Cooling SystemSDR 2006UALA01130Power Supply · failedEMERGENCY LIGHT SYSTEM TEST FAILS *L EMER UNIT*. REPLACED LIGHT EMER PWR SUPPLY MR33512 AND AD 3214-30 BATTERY PER MM 33-51-38. SYS TEST OKJun 10, 2006 · N437UA · Airbus A320232 · Emergency LightingSDR 2006UALA01131Epsu · faultyEPSU FAULT DISPLAYED ON CIDS. AFT L COMM EPSU ARMED AFT L. RESET LEFT AFT EPSU AND REPLACED LEFT EPSU AND BATTERY. EMERGENCY LIGHT TEST OK.Jun 10, 2006 · N445UA · Airbus A320232 · Emergency LightingSDR 2006UALA01198Power Supply · inoperativeEEL LIGHTS FAIL 3SVC TEST. REPLACED FORWARD LEFT EPSU AND BATTERY.Jun 10, 2006 · N442UA · Airbus A320232 · Emergency LightingSDR YENA200652Stator Vane · lack of lubeECAM WARNING -ENG 2 COMPRESSOR VANE- INITIATED AT THRUST REDUCTION FROM BUR. FOLLOWED FULL ECAM PROCEDURE (APPROXIMATELY 3 MINUTES) AND CLEARED ECAM. THE SAME ECAM APPEARED AGAIN AND CLEARED ITSELF WITHIN 1 MINUTE. DECLARED EMERGENCY AND LANDED AT LGB AND GJun 4, 2006 · N630JB · Airbus A320232 · Compressor Bleed ControlSDR 2006UALA01066Compressor · stalledCREW EXPERIENCED MOMENTARY ENG NR 2 STALL ECAM, COMPRESSOR STALL, CLIMBING THRU FL290. NO DEFECTS FOUND DURING TROUBLESHOOTING.Jun 4, 2006 · N472UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2006UALA01017Ram Air Turb · leakingIN PROCESS OF RAT CHECK, DROPPED THE RAT, ABOUT ONE QUART OF HYDRULIC FLUID SPILLED OUT ON THE GROUND. FAULTY RAM AIR TURBINE. REPLACED RAM AIR TURBINE.May 24, 2006 · N489UA · Airbus A320232 · Hydraulic System, AuxiliarySDR 2006UALA01002Connector · disconnectedFOUND LOWER EXIT LIGHTS WERE INOPERATIVE AT THE LT AND RT FWD OVERWING EMERGENCY EXITS. FOUND LT & RT CONNECTORS TO THESE LIGHTS DISCONNECTED, RECONNECT AND TESTED GOOD.May 23, 2006 · N444UA · Airbus A320232 · Light System WiringSDR 2006UALA00990Sill · corrodedFOUND R-2 DOOR SILL HAS CORROSION FWD OF AFT GIRT BAR MOUNT. REPLACED DOOR SILL.May 22, 2006 · N436UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2006UALA00978Slide · faultyFOUND DOOR 2L ESCAPE SLIDE IS DEPLOYED BUT NOT INFLATED. THIS ESCAPE SLIDE SLIPPED OUT OF ITS POSITION BUT DID NOT DEPLOY. ON SITE INVESTIGATION REVEALED SAFETY PIN WAS IN PLACE, HOWEVER, SAFETY PIN FELL DOWN ON GRD AFTER HANGING FROM A/C FOR ABOUT 30 MINUTEMay 21, 2006 · N403UA · Airbus A320232 · Escape SlideSDR 2006UALA00975Skin · buckledEXTERNAL FUSELAGE SKIN BUCKLED SURROUNDING JACK PAD AREA APPROX FRAME 71 THRU FRAME 76, BETWEEN STR 31L THRU STR 31R. REPAIR WAS ACCOMPLISHED BY AIRBUS ON WORK ORDER M-300742-EMBOD.May 20, 2006 · N446UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR AWXA200600875Bleed Valve · malfunctionedLAS - ENGINE SHUTDOWN - FLT 714 - CREW REPORTED THAT AFTER CLEARING RUNWAY, EGT ON NR 2 ENGINE WENT TO 610 WITH NORMAL READINGS ON N1 AND N2. ENGINE WAS AT IDLE. CREW SHUT ENGINE DOWN WITH NO EXCEEDENCES NOTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGIMay 19, 2006 · N663AW · Airbus A320232 · Compressor Bleed ValveSDR 2006UALA00943Slide · failedEXT LOADS FWD L, SHOWS ON PTP AFTER EMERGENCY SYSTEM TEST. REPLACED BOTH RIGHT HAND AND LEFT HAND FORWARD SLIDES. BOTH REMOVED SLIDES DID NOT RING-OUT CORRECTLY AT THE CONNECTOR. OPS TESTED NORMAL WITH NEW SLIDES.May 14, 2006 · N428UA · Airbus A320232 · Escape SlideSDR 2006UALA00920Light · no test"FWD L UNIT" DISPLAYED AFTER EMERGENCY LIGHTS TEST. REPLACED EPSU AND BATTERY AT 1L "TEST OK".May 10, 2006 · N411UA · Airbus A320232 · Emergency LightingSDR 2006UALA00918Fan · failedAN ACRID HAZE FILLED THE CABIN ON DESCENT. FOUND RECIRCULATION FAN FAULTY.REPLACED RECIRCULATION FAN.May 9, 2006 · N487UA · Airbus A320232 · Air Distribution FanSDR 2006UALA01005Light · damagedAT ROW 26 RT EMERGENCY ESCAPE PATH LIGHT DAMAGED. REPLACED ASSEMBLY LIGHT.May 9, 2006 · N418UA · Airbus A320232 · Emergency LightingSDR 2006UALA00883Warning Message · illuminatedEMAC NR 2 COMPRESSOR VANE MESSAGE RECEIVED ON TAKEOFF.May 4, 2006 · N454UA · Airbus A320232 · Central WarningSDR 2006UALA00854Connector · disconnectedEMERGENCY LIGHTS TEST SHOWS EPSU EXT LOAD FWD L. REPLACED FWD EPSU BATTERY, NO HELP. RESECURED CONNETOR ON FWD LT DOOR SLIDE, OPS CHECKS GOOD.Apr 28, 2006 · N481UA · Airbus A320232 · Light System WiringSDR 2006UALA00823Electrical Box · failedELECTRICAL ODOR REPORTED ON FINAL APPROACH NEAR 12ABC. FOUND LT SIDE OF ENTERTAINMENT SYS INOP. FOUND FAULTY SEAT TO SEAT CABLE BETWEEN SEAT ROWS 12ABC AND 13ABC. FOUND BURNED SEAT ELECTRONIC BOX BENEATH SEAT ROW 13ABC. REPLACED SEAT TO SEAT CABLE AND SEAT EApr 26, 2006 · N437UA · Airbus A320232 · Entertainment SystemSDR 2006UALA00785Lanyard · damagedFOUND LANYARD IS DAMAGED AT L2 DOOR SLIDE. REPLACED SLIDE/RAFT ASSY.Apr 24, 2006 · N406UA · Airbus A320232 · Escape SlideSDR 2006UALA00772Epsu · no testAFTER THE EMERGENCY LIGHT TEST, 'AT 33-31-38 EPSU INT LOAD EMER L' MESSAGE SHOWED ON CIDS PANEL. REPLACED EPSU AT 11WL, SYSTEM TESTS NORMAL.Apr 23, 2006 · N439UA · Airbus A320232 · Emergency LightingSDR 2006UALA00802Cylinder · low pressureFOUND DOOR 2L SLIDE PACK INFLATION CYLINDER PRESSURE LOW. REPLACED DOOR 2L SLIDE/RAFT. SLIDE/RAFT REMOVED DID NOT FULLY DEPLOY DUE TO A LEAK FROM ONE OF THE SEAMS. FIRST REPLACEMENT SLIDE/RAFT REJECTED DUE TO LOW PRESSURE. SECOND REPLACEMENT INSTALLED.Apr 22, 2006 · N402UA · Airbus A320232 · Escape SlideSDR 2006UALA00748Computer · malfunctionedBOTH FMGC DUMPED ALL DATA ON DEPARTURE CLIMBING THRU FL180 PROMPTING RTFL. TROUBLESHOOTING CHECKS RETURNED NO DEFECTS.Apr 20, 2006 · N420UA · Airbus A320232 · Flight Management Computing Software SystemSDR 2006UALA00704Light · no testEMERGENCY LIGHTING CHECK FAILS 3 SERVICE TESTS. REPLACED LEFT FRONT BATTERY PACK. SYSTEM TESTED GOOD.Apr 17, 2006 · N416UA · Airbus A320232 · Emergency LightingSDR AWXA200600689Bleed Valve · malfunctionedPHX - ENGINE ANOMALY - FLT 0091 - CREW REPORTED THAT THE NR 1 ENGINE STALLED WHEN CREW LEVELED OFF AT 370. ENGINE RECOVERED AND OPERATED NORMALLY THE REMAINDER OF THE FLT. MX PERFORMED BOROSCOPE INSPECTION OF THE HPC STAGES 3 AND 6 IAW AWA TASK CARD I5M72308Apr 16, 2006 · N649AW · Airbus A320232 · Compressor Bleed ValveSDR 2006UALA00701Battery · faultedEPSU BATTERY AFT LT FAULT DISPLAYED AFTER PERFORMING CABIN EMERGENCY LIGHT TEST.Apr 16, 2006 · N487UA · Airbus A320232 · Emergency Lighting
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