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 2008UALA05547Regulator · leakingCREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. FOUND O2 REGULATOR - TRANSMITTER LEAKING AT FILL PORT. REPLACED REGULATOR - TRANSMITTER. FOUND LOOSE B-NUT AT 1ST OBSERVER'S 02 BOX. SECURED LINE. SERVICED O2 TO 1890 PRIOR TO DEPARTURE. Sep 1, 2008 · N441UA · Airbus A320232 · Crew Oxygen SystemSDR 2008UALA05563Fire Detector · inoperativeENG NR 1 FIRE TEST DOES NOT WORK. NO BELL OR LIGHT. SQUIB LIGHTS DO ILLUMINATE. NO ECAM. FOUND FAULTY FIRE DETECTION UNIT. REPLACED APU FDU. OP CHECKS GOOD.Sep 1, 2008 · N468UA · Airbus A320232 · Fire DetectionSDR 2008UALA05546Floorbeam · corrodedBEAM 255 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. BEGAN INSTALLING FLOORBEAM 255 IN A/C. COMPLETED INSTALLATION OF FLOORBEAM 255. INSPECTED INSTALLATION OF BEAM 255 FOR SAFETY AND SECURITY.Aug 31, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05539Power Supply · faultyEMERGENCY LIGHT SYS TEST FAULTS "UNIT EMER R". *S/D* REPLACED POWER SUPPLY, OP CHECKS OKAY.Aug 30, 2008 · N406UA · Airbus A320232 · Emergency LightingSDR 2008UALA05531Sill · corrodedDOOR SILL 2R HAS CORROSION (MARKED). DOOR SILL 2R HAS CORROSION (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED DOOR SILL. PICKED UP HOLES IN NEW SILL PAN. STARTED INSTALLING HI-LOKS THRU EXTERNAL SKIN COMMON TO DOOR 2R SILL BEAM ONLY. CONTINUED INSTALLING FAug 29, 2008 · N451UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA05532Floorbeam · corrodedFLOORBEAM 250 CORRODED (MARKED). ALSO HAS 8 EA SHEARED FASTENERS ON OUTBOARD SIDE OF BEAM (MARKED). MAJOR REPAIR ACCOMPLISHED. BEAM REMOVED, TRANSFERRED FASTENER HOLES TO NEW BEAM. BEGAN INSTALLING FLOORBEAM 250 IN AC. COMPLETED INSTALLATION OF FLOORBEAM Aug 29, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05521Smoke Detector · inoperativeLAV SMOKE DETECTOR INOP. REPLACED LAV 'D' SMOKE DETECTOR. AC OK FOR SERVICE.Aug 29, 2008 · N483UA · Airbus A320232 · Smoke DetectionSDR 2008UALA05601Valve · inoperativeLANDING GEAR EXT DELAY T-S: REPLACE LANDING GEAR SAFTEY VALVE 49GA. REPLACED LANDING GEAR SAFTEY VALVE 49GA PER MM32-31-17 THRU STEP 3.C. PG 411. NEED TO COMPLETE INSTALLATION FROM STEP 4.D. PG 412 THRU TO END. CONT OF AMIS ITEM 7342001.Aug 28, 2008 · N437UA · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR 2008UALA05502Floorbeam · corrodedFLOORBEAM 225 CORRODED AROUND FWD NUT PLATE HOLE (MARKED). MAJOR REPAIR ACCOMPLISHED: REMOVED BEAM, DRILLED BEAM AND ATTACH ANGLES. INSTALLED FLOORBEAM 225 IN A/C.Aug 27, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05500Unknown · unknownLOSS OF FMGC1 & GPWS. RTFL. Aug 27, 2008 · N454UA · Airbus A320232 · Standard Practices/StructuresSDR 2008UALA05492Battery · faultyESPU UNIT EMERGENCY LEFT MSG ON CIDS PANEL. REPLACED ESPU BATTERY 11WL. EMERGENCY LIGHT TEST NORMAL.Aug 27, 2008 · N498UA · Airbus A320232 · Emergency LightingSDR 2008UALA05491O-Ring · leakingDOOR 2R SLIDE PRESSURE BOTTLE LOOKS LOW. O-RING LEAKING FROM CENTER BALL SHAFT. REMOVED & REPLACED O-RING.Aug 27, 2008 · N498UA · Airbus A320232 · Escape SlideSDR 2008UALA05484Sill · corrodedDOOR 2L SILL IS CORRODED (MARKED).Aug 26, 2008 · N451UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA05482Unknown · unknownMECHANICAL PROBLEM INCURRED. FLIGHT DIVERTED.Aug 26, 2008 · N472UA · Airbus A320232 · Standard Practices/StructuresSDR 2008UALA05475Shear Plate · corrodedRIGHT SHEAR PLATE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED RT SHEAR PLATE. INSTALLED NEW RT SHEAR PLATE.Aug 26, 2008 · N451UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA05485Floorbeam · corrodedFLOORBEAM 245 CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. TRANSFERRED ATTACHING PARTS AND IS READY FOR FIT INTO AC. BEAM INSTALLED. INSPECTED THE INSTALLATION OF BEAM 245 FOR SECURITY AND FOUND SECURE.Aug 26, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05474Floorbeam · corrodedFLOORBEAM 235 CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. INSTALLED TIE DOWN FITTINGS FOR LAV AND GALLEY MODULES ONTO NEW FLOORBEAM 235. FITTED BEAM 235 TO ACFT (PICKED UP HOLES) AND FITTED 2EA. NEW SPLICES AT FWD END OF BEAM 235. INSTALLED FLOORBEAM 23Aug 25, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05464Unknown · unknownNR 2 ENGINE EPR FAULT. RTFL.Aug 24, 2008 · N402UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2008UALA05444Floorbeam · corrodedFLOORBEAM 175 IS CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 175. TRANSFERRED CABLE ATTACH BRACKETS AND STARTED ASSEMBLY WITH BEAM 210. BEAM 175 AND 210 ARE TOGETHER AND NEED FWD END OF BEAM PUT INTO AC AND DRILL FWD ATTACH HOLES. PICAug 24, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05445Floorbeam · corrodedFLOORBEAM 210 IS CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 210. TRANSFERRED ATTACH BRACKETS AND STARTED ATTACHING TO BEAM 175. BEAMS 210 AND 175 ARE TOGETHER AND NEED THE FWD END DRILLED TO BRACKETS IN A/C. PICKED UP REMAINING HOLESAug 24, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05446Floorbeam · corrodedFLOORBEAM 165 CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 165. REMOVED ANGLES. TRANSFERRED BRACKETS AND ATTACHED BEAM 165 AND 200 WITH SPLICE ANGLES WORKING ON BENCH. COMPLETED INSTALLATION.Aug 24, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05447Floorbeam · corrodedFLOORBEAM 200 IS CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 200. REMOVED ANGLES ATTACHED TO BEAM 165, DRILLED SPLICE ANGLES FOR BEAM 200 TO 205. COMPLETED INSTALLATION. Aug 24, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05448Floorbeam · corrodedFLOOR BEAM 205 IS CORRODED (MARKED). *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 205. REMOVED ANGLES, WORKING ON BENCH. INSTALLED GALLEY ATTACH POINTS, DRILLED NEW SPLICE ANGLES. INSTALLED NEW SPLICE ANGLES.Aug 24, 2008 · N451UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA05463Hydraulic System · failedYELLOW HYD SYSTEM FAILURE. FLIGHT DIVERTED.Aug 23, 2008 · N419UA · Airbus A320232 · Hydraulic System, MainSDR 2008UALA05477Smoke Detector · faultySMOKE LAVATORY DETECTOR FAULT AT FL350. FOUND DEFECTIVE SMOKE DETECTOR. REPLACED SMOKE DETECTOR. TESTS OKAY ON CFDS TEST & CIDS.Aug 23, 2008 · N491UA · Airbus A320232 · Smoke DetectionSDR 2008UALA05397Controller · malfunctionedCABIN EMERGENCY CALL GOES OFF BY ITSELF. REPLACED NR 1 CIDS DIRECTOR PER MM 23-73-00, TESTS OK.Aug 22, 2008 · N408UA · Airbus A320232 · Communications SystemSDR 2008UALA05398Unknown · odorF/A AND CPT CREW SMELLED AN ELECTRIC ODOR UPON LANDING ALSO ON APPROACH. ACCOMPLISHED POWER RUNS ON BOTH ENGINES, COMPARING BLEEDS FOR ODOR AT POWER AND AT IDLE, CHECKING COMBINATIONS OF BLEEDS AND PACKS. NO UNUSUAL ODORS NOTED, NO ELECTRICAL ODORS NOTED. PAug 22, 2008 · N476UA · Airbus A320232 · Air Distribution SystemSDR 2008UALA05416Unknown · unknownCABIN EMERGENCY CALL GOING OFF BY ITSELF.Aug 22, 2008 · N408UA · Airbus A320232 · Communications SystemSDR 2008UALA04365Attach Bracket · brokenLEFT NR 3 FLAP TRACK AFT END STAY ASSY ATTACH BRACKET I/B LUG BROKEN.Aug 21, 2008 · N423UA · Airbus A320232 · Wing, Attach FittingsSDR YENA2008081Bleed Valve · failedFLT 785, MCO-BON, DIVERTED TO FLL, ENG NR 2 BLEED FAULT. ACCOMPLISHED ECAM QRH, NO PRESSURIZATION IN CABIN. LOST BOTH (1&2) EMERGENCY DESCENT REQUIRED. REMOVED AND REPLACED NR 2 ENG PRESSURE REGULATING VALVE 4001HA PER AMM 36-11-52. OPS CHECK OK.Aug 21, 2008 · N569JB · Airbus A320232 · Compressor Bleed ValveSDR 2008UALA04355Wire · crossedCREW REPORT: EMERGENCY EXIT SIGN AT LEFT OVERWING EXIT INOP.Aug 20, 2008 · N494UA · Airbus A320232 · Light System WiringSDR 2008UALA04352Bottle · lowLARGE O2 BOTTLE AT 2R PRESS IS LOW. Aug 19, 2008 · N422UA · Airbus A320232 · Crew Oxygen SystemSDR USAA920081539Pump · inoperativeFLT 438 TPA-LAS - EMERGENCY LANDING - CREW REPORTED `HYD G RSVR LO LVL` AND `HYD G ENG 1 PUMP LOW PR` INDICATIONS. AN EMERGENCY WAS DECLARED DUE TO POSSIBLE LOSS OF NOSE WHEEL STEERING ON LANDING. THE ACFT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. Aug 18, 2008 · N664AW · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR 2008UALA04324Battery Pack · faultyLEFT UNIT DISPLAYED ON 3SV EMERGENCY LIGHT TEST. FOUND FAULTY BATTERY PACK. REPLACED EMERGENCY LIGHT BATTERY PACK & UNIT AT LT OVERWING. MESSAGE NO LONGER DISPLAYED. OK FOR SERVICE.Aug 16, 2008 · N403UA · Airbus A320232 · Emergency LightingSDR YENA2008080Thermostat · failedFLT 640, SFO-JFK, DIVERTED TO LGB, ENG 1 AND ENG 2 BLEED FAULTS DURING TAKEOFF DEPARTURE PHASE, ENG 2 BLEED FAULT OCCURRED FIRST. REPLACED NR 2 ENG THERMOSTAT FIN7170HM2. LEAK CHECK GOOD. REF AMM 36-11-06. REMOVED AND REPLACED NR 1 ENG FAN AIR VALVE THERMOAug 16, 2008 · N535JB · Airbus A320232 · Pneumatic Distribution SystemSDR 2008UALA04323Power Supply · failedFAILURE OF THE EMERGENCY LIGHT TEST. *S/D* REPLACED POWER SUPPLY.Aug 16, 2008 · N484UA · Airbus A320232 · Emergency LightingSDR 2008UALA04309Actuator · faultedELAC 1 & 2 PITCH FAULT. RTFL. REPLACED THS ACTUATOR. ACCOMPLISHED SUCCESSFUL TEST FLIGHT. A/C OKAY FOR SERVICE. Aug 15, 2008 · N460UA · Airbus A320232 · Flight Control SystemSDR YENA2008079Powerplant · flamed outFLT 354, BUR-JFK, UPON LANDING NR 1 ENG FLAMED OUT ON ROLL OUT, AFTER ENG 1 COMP FAIL ECAM FOLLOWED BY ENG 1 FAIL ECAM. DVDR ANALYSIS DETERMINED NR1 ENG REQUIRES ENG REPLACEMENT DUE TO EGT OVERLIMIT. REMOVED AND REPLACED NR1 ENG PER TC A320-71-00-20-400-040.Aug 14, 2008 · N715JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2008UALA04264Oxygen System · leakingCREW O2 LEAKS 10 PSI EVERY 8 MINUTES.Aug 13, 2008 · N403UA · Airbus A320232 · Crew Oxygen SystemSDR YENA2008078Powerplant · stalledFLT 489, BOS-LGB, AIR RETURN TO BOS, ENG NR1 STALL ON DEPARTURE AT APPROX 100FT ALT. WITH THRUST REDUCTION ECAM INDICATION WENT AWAY AND CONTINUED TO CLIMB TO FL230. PERFORMED QRH 6-26 ITEMS AND STALL OCCURRED AGAIN. WITH NUMBER 1 THRUST LEVER TO IDLE WENT Aug 12, 2008 · N510JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2008UALA04242B-Nut · leakingHYDRAULIC PROBLEM. RTFL. FOUND LT MLG DOOR UPLOCK ASSY B-NUT ON FWD SIDE LEAKING AND 3-4'S OF THE WAY BACKED OFF AND LOOSE. SECURED B-NUT ON ON FWD SIDE OF LT MLG DOOR UPLOCK ASSY. SERVICED GREEN SYSTEM & LEAK CHECK ACCOMPLISHED. Aug 12, 2008 · N443UA · Airbus A320232 · Hydraulic System, MainSDR 2008UALA04252Oxygen System · lowCREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: OXYGEN NEEDS SERVICING. LEAK CHECKED WITH NO LEAKS NOTED. SERVICED TO FULL. Aug 11, 2008 · N430UA · Airbus A320232 · Crew Oxygen SystemSDR USAA920081499Idg · inoperativeFLT 98 -LAS-DTW- AIR TURNBACK - CREW REPORTED TR1 AND ELEC GEN 1 FAULT ON CLIMBOUT AND "ELEC AC BUS 1 FAULT." MAINTENANCE REMOVED AND REPLACED THE NR 1 ENG INTEGRATED DRIVE GENERATOR PER AIRBUS MAINTENANCE MANUAL 24-21-51. OPERATIONAL CHECK GOOD. (S)Aug 10, 2008 · N648AW · Airbus A320232 · AC Generator-AlternatorSDR YENA2008076Computer · failedFLT 233, SLC-LGB, AFTER TAKEOFF ACFT SUFFERED A L&R AIL FAULT WITH ACFT ONLY ABLE TO FLY IN ALTERNATE LAW. PER PFR MSGS ELAC AIL ORDER DISAGREE & ELAC 2 AIL ORDER DISAGREE WERE FOUND. PER TSM 27-93-00-810-949 STEP 4A. ELAC (2CE1) NEEDS REPLACING. PERFORMED Aug 10, 2008 · N603JB · Airbus A320232 · Flight Control SystemSDR 2008UALA04191Smoke Detector · inoperativeLAV F SMOKE DETECTOR INOP. FOUND FAULTY SMOKE DETECTOR. REPLACED SMOKE DETECTOR, OP CHECKED GOOD. AC OK FOR SERVICE. Aug 9, 2008 · N407UA · Airbus A320232 · Smoke DetectionSDR 2008UALA04192Light · faultyDURING 3 SVC CHECK EMERGENCY SYSTEM TEST FAILED. MSG 33-51-38 "INT. LOADS AFT L" + "EXT. LOADS AFT L. T-S DOWN TO ROW 20ABC EGRESS LIGHTING, REMOVED BULB. OPERATION NORMAL. ALL OTHER EGRESS LIGHTING WORKING NORMALLY. REPLACED 20ABC SEAT MOUNTED EMERGENCY LIAug 9, 2008 · N432UA · Airbus A320232 · Emergency LightingSDR 2008UALA04170Outflow Valve · malfunctionedPRESSURIZATION PROBLEMS. FLIGHT DIVERTED. FOUND PFR FAULTING OUTFLOW VALVE 81. REPLACED OUTFLOW VALVE. OPS CHECKED GOOD.Aug 8, 2008 · N411UA · Airbus A320232 · Pressure Regulator/Outflow ValveSDR 2008UALA04172Smoke Detector · false activationAVIONICS SMOKE ECAM DISPLAYED AFTER TAKEOFF, NO PERCEPTIBLE SMOKE DETECTED. RAN SUCCESSFUL TEST OF AEVC & RESET BOTH FLIGHT WARNING COMPUTERS (PRECAUTIONARY). INSTALLED NEW SMOKE DETECTOR 2WA. OPS CHECK SATISFACTORY.Aug 8, 2008 · N439UA · Airbus A320232 · Smoke DetectionSDR 2008UALA04187Packing · leakingHYDRAULIC PROBLEM. FLIGHT DIVERTED. FOUND MANIFOLD ASSY LEAKING BELOW PRIORITY VALVE. REPLACED PACKING. NO LEAKS FOUND.Aug 8, 2008 · N415UA · Airbus A320232 · Hydraulic System, MainSDR 2008UALA04159Drain Valve · leakingHYDRAULIC GREEN SYSTEM LOW LEVEL DISPLAYED. FOUND DRAIN VALVE LEAKING. REPLACED DRAIN VALVE AND SERVICED HYD SYSTEM. OP CHECKS NORMAL. Aug 7, 2008 · N427UA · Airbus A320232 · Hydraulic System, Main
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