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 2008UALA03114Transducer · malfunctionedCABIN TEMPERATURE PROBLEM. RTFL. *S/D* FOUND PRESS BLEED TRANSDUCER ON NR 2 ENG BAD. REPLACED PRESS BLEED TRANSDUCER, RAN ENGS. PACK TEMPS AND CONDITION AIR OPS NORMAL. ALSO REPLACED AFT CABIN TRIM VALVE.Jun 2, 2008 · N470UA · Airbus A320232 · Engine Bleed Air SystemSDR 2008UALA03159Sign · looseAT DOOR 1L - EXIT LIGHT AT LOWER LEFT SIDE IS LOOSE. *S/D* SIGN IS BROKEN. REPLACED EMERGENCY EXIT SIGN AT LEFT LOWER DOOR 1L.Jun 2, 2008 · N444UA · Airbus A320232 · Emergency LightingSDR 2008UALA03194Oxygen System · low pressureCREW 02 NEEDS SERVICE. SERVICED CREW O2 TO FULL, NO LEAKS NOTED.Jun 2, 2008 · N461UA · Airbus A320232 · Crew Oxygen SystemSDR 2008UALA03134Power Supply · failedEPSU UNIT R FAILED ON 3 SVC CK. *S/D* EPSU FAILURE. REPLACED EPSU, ALL TESTS GOOD.May 30, 2008 · N432UA · Airbus A320232 · Emergency LightingSDR 2008UALA03092Bottle · reads lowDOOR 1R DOOR PRESSURE AT 500. SERVICED DOOR 1R ASSIST BOTTLE TO 1750 PSI. NO LEAKS WERE NOTED AT TIME OF SERVICE.May 29, 2008 · N471UA · Airbus A320232 · Passenger/Crew DoorsSDR 2008UALA03093Skin · dentedLEFT INBOARD FLAP DENT AND ABRASION ON TRAILING EDGE, CENTER AFT OF NR 2 TIRE. FOUND AND REPORTED BY RAMP DURING WALKAROUND. *S/D* IDENTIFIED BY SRM 57-50-00- 001 PG 7 INBOARD FLAP. DAMAGE AREA PER SRM 57-52-00-101 PG 4 AS ZONE 2, PER TABLE 101 PG 2. DENTMay 29, 2008 · N497UA · Airbus A320232 · Trailing Edge FlapsSDR 2008UALA03071Shear Plate · corrodedRIGHT SHEAR PLATE BETWEEN FRAMES 69 AND 70 HAS EVIDENCE OF SURFACE CORROSION ON UPPER SURFACE AND FASTENER HOLES. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED SHEAR PLATE, DRILLED NEW PLATE AND INSTALLED.May 28, 2008 · N447UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA03072Sill · corrodedDOOR SILL 2L HAS CORROSION AT APPROX FRAME 68. CORROSION - ACP'ED REWORK, PRIMER AND TOP COAT REF SRM 53-00-14.May 28, 2008 · N447UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA03053Floorbeam · corrodedFLOORBEAM ITEM 235 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED FLOORBEAM AND RE-INSTALLED NEW.May 27, 2008 · N447UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA03054Floorbeam · corrodedFLOORBEAM ITEM 250 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM, BEAM ON WORK TABLE. CONT OF AMIS ITEM 0912010: PICKED UP HOLES FOR BARREL NUT FITTINGS AND SPLICE ANGLES ON NEW BEAM. CONT OF AMIS ITEM 0912017: CONTINUED WORKING BEAM PARTMay 27, 2008 · N447UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA03055Floorbeam · corrodedFLOORBEAM ITEM 255 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. FLOORBEAM ITEM 255 HAS CORROSION. (MARKED) REF SRM 53-41-14 FIG 1 ITEM 255. REMOVED BEAM 255, ON WORK TABLE. CONT OF AMIS ITEM 0912011: PICKED UP HOLES FOR SPLICE ANGLE ON NEW BEAM. CONMay 27, 2008 · N447UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA03056Floorbeam · corrodedFLOORBEAM ITEM 165 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM 165 FOR CORROSION WORK CONT OF AMIS ITEM 0912012. REPLACED BEAM REF SRM 53-41-14.May 27, 2008 · N447UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA03057Floorbeam · corrodedFLOORBEAM ITEM 200 HAS CORROSION. UPDATE ACCOMPLISHED MAJOR REPAIR AT DEN. REF SRM 53-41-14 FIG 1 ITEM 200. BEAM REMOVED CONT OF AMIS ITEM 0912013. REPLACED BEAM, REF SRM 53-41-14.May 27, 2008 · N447UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA03058Floorbeam · corrodedFLOORBEAM ITEM 175 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM 175 TRANSFERRED CLIPS AND SPLICES TO NEW BEAM PARTS.May 27, 2008 · N447UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA03059Floorbeam · corrodedFLOORBEAM ITEM 205 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. BEAM REMOVED. REPLACED BEAM, REF SRM 53-41-14.May 27, 2008 · N447UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA03060Floorbeam · corrodedFLOORBEAM ITEM 210 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM 210 TRANSFERRED ALL CLIPS, AND INSTALLED SPLICES.May 27, 2008 · N447UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA03061Sill · corrodedDOOR SILL 2R HAS CORROSION AT FRAME 66 AND 68 AT NUT PLATE (MARKED). ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED DAMAGE, MFG REPAIR PARTS, TREATED PRIMED AND TOP COATED WITH PAINT.May 27, 2008 · N447UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA03062Shear Plate · corrodedLEFT SHEAR PLATE BETWEEN FRAME 69 AND 70 HAS EVIDENCE OF SURFACE CORROSION ON UPPER SURFACE AND AT FASTENER HOLES. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED LT SHEAR PLATE AND DRILLED NEW PLATE TO FIT, CLEANED AND TOP COATED AREA.May 27, 2008 · N447UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02997Seal · damagedLANDING GEAR FAILED TO RETRACT. RTFL. FOUND NOSE STRUT SEALS DAMAGED. REPLACED NOSE STRUT SEALS, SERVICED STRUT. NO REPEATS.May 26, 2008 · N441UA · Airbus A320232 · Nose/Tail Landing Gear Strut/AxleSDR 2008UALA02999O-Ring · failedLOSS OF PRESSURE IN YELLOW HYD SYSTEM. FLT RTFL. YELLOW ELECTRIC HYD PUMP IS LEAKING. REPLACED O-RING ON PTU CHECK VALVE.May 26, 2008 · N416UA · Airbus A320232 · Hydraulic System, MainSDR 2008UALA03007Connector · unsecureNR 3 SERVICE CABIN EMER LIGHT CHECK FAILED. INT LOADS EMER R AND EXT LOADS AFT L. REMOVED AFT LT SLIDE AND RESET CONNECTOR AND RE-INSTALLED AND TEST NOW OK.May 26, 2008 · N417UA · Airbus A320232 · Light System WiringSDR 2008UALA02996Smoke Warning · malfunctionedAVIONIC SMOKE ECAM, NO SMOKE PERCEPTIBLE. FLIGHT DIVERTED. FOUND NO EVIDENCE OF SMOKE OR ODORS ON MAIN DECK OR E&E COMPARTMENT, ECAM HAD CLEARED UPON ARRIVAL, SUCCESSFULLY TESTED AEVC AND SCDU REF AMM 21-26-00. CHECK PFR REPORT FOR FAILURE MESSAGES, NONE FOMay 25, 2008 · N467UA · Airbus A320232 · Smoke DetectionSDR 2008UALA02966Slide · out of positionDOOR 1L SLIDE OUT OF PACK. UNKNOWN. REMOVED SLIDE AND REPLACED.May 22, 2008 · N425UA · Airbus A320232 · Escape SlideSDR 2008UALA02857Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM ITEM 210. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED FLOORBEAM, FLOOR BEAM INSTALLED. NEED TO SECURE AFT OUTBOARD BOLT, AND WIRE CLAMPS.May 19, 2008 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02858Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM ITEM 175. ACCOMPLISHED MAJOR REPAIR AT DEN. INSTALLED FLOORBEAM. REQUIRES INSTALLATION OF WIRE CLAMPS AND BLOWER FAN BOLTS. HARDWARE IS ATTACHED TO FLOORBEAM.May 19, 2008 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02859Skin · gougedGOUGE FOUND JUST BELOW AND FWD OF O2 SVC ACCESS DOOR ON LEFT SIDE OF FUSELAGE AT FRAME 13, BETWEEN STRINGERS 21 AND 27, 3 INCHES LONG AND .015 INCH DEEP. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.May 18, 2008 · N494UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA02860Skin · dentedDENT IN FWD LOWER FUSELAGE JUST LEFT OF GROUND COMMUNICATION ACCESS DOOR FWD OF E/E DOOR. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.May 18, 2008 · N494UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA02861Skin · dentedFOUND DENT ON BOTTOM OF FUSELAGE JUST FWD OF THE FRONT E-E DOOR. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.May 18, 2008 · N494UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA02873Unknown · malfunctionedELAC 2 PITCH FAULT AFTER FIRST ENG START ON GROUND SWITCH CYCLE. RESET ECAM. May 18, 2008 · N477UA · Airbus A320232 · Elevator Control SystemSDR 2008UALA02872Oxygen Bottle · lowFOUND PORTABLE OXYGEN BOTTLE LOW AT SEAT ROW 26 ABC. REPLACED O2 BOTTLE.May 17, 2008 · N469UA · Airbus A320232 · Portable Oxygen SystemSDR 2008UALA02813Shear Plate · corrodedFOUND SHEAR PLATE NR 15 CORRODED.May 16, 2008 · N446UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02814Floorbeam · corrodedFOUND CORROSION ON FLOOR BEAM NR 215. May 16, 2008 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02838Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM ITEM 235. MAJOR REPAIR ACCOMPLISHED, REPLACED FLOORBEAM 235.May 16, 2008 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02811Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM 200. MAJOR REPAIR ACCOMPLISHED: REPLACED BEAM.May 16, 2008 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02812Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM 205. MAJOR REPAIR ACCOMPLISHED: REPLACED BEAM.May 16, 2008 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02793Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM NR 255.May 15, 2008 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02794Sill · corrodedDOOR SILL 2R CORRODED AROUND FLOOR PANEL ATTACH NUTPLATE HOLES IN AREA OF FR66.May 15, 2008 · N446UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02797Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM NR 250. May 15, 2008 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02798Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM NR 165. MAJOR REPAIR ACCOMPLISHED: REPLACED BEAM.May 15, 2008 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02796Beam · corrodedLT AFT PASSENGER-CREW DOOR SILL BEAM HAS CORROSION AROUND FLOOR PANEL ATTACH NUTPLATE HOLE LOCATED AT INBD MOST FLANGE APPROX 4 INCHES FWD OF FR68. MAJOR REPAIR ACCOMPLISHED: MFG AND INSTALLED ANGLE REPAIR WET.May 14, 2008 · N446UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02772Light · inoperative15C EMERGENCY LIGHT INOP. RELAMPED. OP CK GOOD.May 13, 2008 · N416UA · Airbus A320232 · Emergency LightingSDR 2008UALA02773Bleed Valve · malfunctionedNR 1 ENGINE HIGH PRESSURE BLEED VALVE PROBLEM CAUSED A DIVERSION.May 13, 2008 · N427UA · Airbus A320232 · Compressor Bleed ValveSDR 2008UALA02780Unknown · odorIN FLIGHT HAD NOISE AND VIBRATION BELOW FLT DECK (RUDDER PEDAL AREA) WITH BURNING RUBBER (ELECT) SMELL FOLLOWED BY AEVC VENT BLOWER FAULT.May 13, 2008 · N436UA · Airbus A320232 · Air Distribution SystemSDR 2008UALA02730Warning System · activatedELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. FCDC FAILED---NO SHOP FINDINGS. REPLACED FCDC-2. SYSTEM CKS NORMAL, NO MSG'S DISPLAYED. ACCOMPLISHED AFS & LAND TESTS. CHECKS OK. May 12, 2008 · N478UA · Airbus A320232 · Elevator Control SystemSDR 2008UALA02756Power Supply · failedEMERGENCY LIGHT TEST FAILS PER "A" CHECK JOB CARD. "EPSU BATTERY EMER R" DISPLAYED.May 12, 2008 · N464UA · Airbus A320232 · Emergency LightingSDR 2008UALA02757Light · faultyDURING TAKEOFF, THE EMERGENCY LIGHTS IN THE CABIN CAME ON FOR ABOUT 4 MINUTES.May 12, 2008 · N497UA · Airbus A320232 · Emergency LightingSDR 2008UALA02705Blade · failedNR 2 ENGINE STALL. AMBER DECLARED, FLIGHT DIVERTED. ENGINE REPLACED. FOUND HPC 6TH STAGE BLADE FAILURE.May 11, 2008 · N441UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2008UALA02731Lens · missingEMERGENCY AISLE LIGHT AT SEAT 18C IS MISSING LENS. REPLACED SEAT LIGHT. OP CHECKS OKAY.May 11, 2008 · N463UA · Airbus A320232 · Emergency LightingSDR 2008UALA02725Control Unit · faultyAIL SERVO FAULT, LAF DEGRADED L AIL AMBER HALF BOX B, R AIL AMBER HALF BOX G. REPLACED ELAC 1, ALL OPS TESTS WERE NORMAL. May 10, 2008 · N408UA · Airbus A320232 · Flight Control SystemSDR 2008UALA02733Oxygen System · low pressureFOUND CREW OXYGEN LOW ON ECAM. SERVICED O2 TO FULL. NO LEAKS NOTED AT TIME OF SERVICE.May 10, 2008 · N469UA · Airbus A320232 · Crew Oxygen System
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