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.

SDR 2008UALA05894Sill · corrodedR2 DOOR SILL HAS CORROSION AT FRAME 66 -Y1732. INSTALLED RE PAIR PER MT53-025 AND SRM53-41-14 ON NR K8545G.Sep 25, 2008 · N804UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR 2008UALA05895Lever · out of rigDOOR 2R, PER INBOARD CREW, OK ON GRD WHEN PRESSURIZED SLIDE ARMING HANDLE MOVES OUT APPROX ONE-HALF IN. RE-RIGGED DOOR ARMING LEVER. DOOR ARMS/DISARMS NORMALLY.Sep 25, 2008 · N826UA · Airbus A319131 · Escape SlideSDR 2008UALA05869Sill · corrodedCORROSION ON R2 DOOR SILL AT BOLT HOLE 6 IN FWD OF AFT GIRT BAR LATCH UNDER SCUFF PLATE. ACCOMPLISHED MAJOR REPAIR AT LCQ. MAJOR REPAIR. REPAIRED PER SRM 53-41-14 ON NR D8530Y BY 306924 AND INSPECTED BY LC5.Sep 23, 2008 · N804UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR 2008UALA05845Sill · corrodedCORROSION ON R2 DOOR SILL BETWEEN FR 67 AND 68. MAJOR REPAIR. CUT OUT DAMAGE AND INSTALLED REPAIR.Sep 22, 2008 · N804UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR 2008UALA05824Sill · corrodedCORROSION ON L2 DOOR SILL FWD OF FR 68. REPAIRED PER SRM 53-41-14 ON NR K8564G.Sep 20, 2008 · N804UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR 2008UALA05853Floorbeam · corrodedFLOORBEAM 70 CORRODED IN AREA OF FRAME 66 AFT OF LAV LOCATED FORWARD DOOR 2 LEFT. REMOVED CORROSION. VERIFIED CORROSION WAS REMOVED AND IS WITHIN LIMITS. TREATED PRIMED AND PAINTED. OK FOR SERVICE. Sep 20, 2008 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05771Line · looseY RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN - HYD. FOUND LOOSE LINE AT KEEL BEAM. SECURED HYD LINE AT KEEL BEAM, PUMP REPLACED FOR CAVITATION AND FILTERS DOWNLINE. SERVICED SYSTEM AND ALL LEAK CHECKS WERE GOOD. Sep 18, 2008 · N829UA · Airbus A319131 · Hydraulic System, MainSDR 2008UALA05769Shear Tie · corrodedSHEAR PLATE AFT OF DOOR 2R AND FRAME 69 DAMAGED BY CORROSION. MAJOR REPAIR ACCOMPLISHED, REPLACED SHEAR TIE. COMPLETED INSTALLING WIRES THROUGH SHEAR PLATE.Sep 17, 2008 · N817UA · Airbus A319131 · Fuselage Internal Mounting StructureSDR 2008UALA05759Floorbeam · corrodedFLOORBEAM 150 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. ASSEMBLED AND PICKED UP HOLES. ATTACHED TO BEAM 95 AND STARTED INSTALLATION. INSTALLED BEAM. Sep 17, 2008 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05760Floorbeam · corrodedFLOORBEAM 145 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED AND DISASSEMBLED FLOORBEAM. TRANSFERED HOLES TO NEW BEAM. INSTALLED SPLICE ANGLES TO ATTACH BEAM 145 TO BEAM 140. INSTALLED FLOORBEAM TO FRAME. INSTALLED SECURING FASTENERS. Sep 17, 2008 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05761Floorbeam · corrodedFLOORBEAM 140 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED AND DISASSEMBLED FLOORBEAM. TRANSFERED HOLES TO NEW BEAM. ATTACHED SPLICE ANGLES TO ATTACH BEAM 140 TO BEAM 145. BUILT AND INSTALLED 3 BEAM. Sep 17, 2008 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05762Floorbeam · corrodedFLOORBEAM 175 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM AND ANCHOR FITTINGS. INSTALLED ANCHOR FITTINGS AND FITTED BEAM 175 INTO ACFT. DRILLED HOLES FOR AFT END BRACKET. STARTED INSTALLATION OF BRACKET. STILL NEED TO ATTACH TO FRAME. INSTALLED FLSep 17, 2008 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05757Floorbeam · corrodedFLOORBEAM 95 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED BOLTS AT FWD END OF BEAM. REMOVED BEAM AND SPLICE. INSTALLED ALL BRACKETS. ATTACHED TO BEAM 95, INSTALLED AND MOUNTED TO FRAME 65 AND 66. INSTALLED FORWARD SPLICE AT FRAME 64. INSTALLED BEAM. Sep 16, 2008 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05758Floorbeam · corrodedFLOORBEAM 80 CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED BOLTS AT FWD END OF BEAM. REMOVED AND DISASSEMBLED FLOORBEAM. TRANSFERRED HOLES TO NEW BEAM. PICKED UP HOLES ON FWD SPLICE. INSTALLED AFT SPLICE. INSTALLED BEAM. Sep 16, 2008 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05740Cylinder · low pressureDOOR 1 RIGHT EMERGENCY OPERATION CYLINDER PRESSURE IS LOW. SERVICED CYLINDER. SERVICED CYLINDER, NO LEAKS NOTED AT TIME OF SERVICE.Sep 15, 2008 · N834UA · Airbus A319131 · Passenger/Crew DoorsSDR 2008UALA05743Floorbeam · corrodedBEAM UNDER FLOORBOARD AT DOOR 1 RIGHT HAS CORROSION ON IT. FIRST BEAM INBOARD OF SILL. MAJOR REPAIR ACCOMPLISHED. INSTALLED BEAM JUST INBOARD OF 2R SILL. BEAM IS B-BEAM.Sep 15, 2008 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05723Cover · missingEMERGENCY EXIT LIGHT COVER MISSING FROM FWD CLOSET BULKHEAD AT DOOR 1L. DISCOVERED COVER IS MISSING. REPLACED LIGHT ASSY. OP CHECKS GOOD.Sep 14, 2008 · N845UA · Airbus A319131 · Emergency LightingSDR 2008UALA05733Floorbeam · corrodedFWD GALLEY FLOORBEAM "A" HAS CORROSION AT FR16. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE.Sep 14, 2008 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05710Sensor · faultyDOOR 2R SLIDE ARMED INDICATION READS DISARMED WITH DOOR CLOSED AND SLIDE ARMED IN FLIGHT. REPLACED DOOR HOOK PROXIMITY SENSOR. ADJUSTED DOOR HANDLE SENSOR 17WV2. ALL SYSTEMS TEST NORMAL. Sep 13, 2008 · N815UA · Airbus A319131 · Escape SlideSDR 2008UALA05668Floorbeam · corrodedFLOORBEAM - Y765 HAS CORROSION FWD OF FR68. MAJOR REPAIR ACCOMPLISHED. BEAMS REMOVED AND BRACKETS TRANSFERRED (BEAM 95 AND 150) BEAMS NEED TO BE SPLICED TOGETHER AND INSTALLED. SPLICE INSTALLED AND BEAMS 95 AND 150 INSTALLED.Sep 11, 2008 · N816UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05742Floorbeam · corrodedFWD GALLEY OUTBOARD "B" FLOORBEAM HAS ONE FOOT SECTION WITH CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED BRACKETS. INSTALLED MFG'ED BEAM. INSTALLED ALL WIRE BUNDLES AND SECURED ALL CLAMPS BEAM. FINAL INSTALLATION IS COMPLETE.Sep 11, 2008 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05667Stiffener · crackedSTIFFENER IN NOSE WHEEL WELL LEFT SIDE IS CRACKED ON THE RISER. REPAIRED STIFFENER PER SRM 57-11-16.Sep 10, 2008 · N816UA · Airbus A319131 · Wing SparSDR UALA2013031301498Skin · corrodedLEFT & RIGHT OUTER WING TOP SKIN AT REFUEL PORT CUTOUT FLANGE HAVE PITTING CORROSION. REPAIR PER EVA-71896 AND REO-L01103.Sep 10, 2008 · N815UA · Airbus A319131 · Wing, Plate/SkinSDR 2008UALA05663Floorbeam · corrodedFLOORBEAM -Y1292 HAS CORROSION JUST AFT OF FR66. MAJOR REPAIR ACCOMPLISHED. REPLACED BEAM & SECURED WITH FASTENERS. ACP BEAM INSTALLATION FOR Y1292 FWD OF BEAM 140.Sep 9, 2008 · N816UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05665Floorbeam · corrodedFLOORBEAM 145 HAS LOOSE RIVET(MARKED). MAJOR REPAIR ACCOMPLISHED. BEAM OUT AND ON BENCH WORKING. FOUND CORRODED BEAM REPLACED. ACP INSP OF BEAM 145.Sep 9, 2008 · N816UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05664Floorbeam · corrodedFLOORBEAM Y254 HAS CORROSION BETWEEN FR65 AND FR66 (MARKED). REPLACED BEAM 160. REPLACED FLOORBEAM 160.Sep 9, 2008 · N816UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05643A/C Pack · malfunctionedHARD CONT TEMP PACK 1 WILL NOT GO TO HIGH FLOW. OPERATED NR 1 PACK THROUGH ALL PARAMETERS AND GROUND CHECKS NORMAL. PACK WENT TO HIGH FLOW WITH NO DELAY OR MESSAGES.Sep 8, 2008 · N826UA · Airbus A319131 · Cabin Cooling SystemSDR 2008UALA05648Slide · lowDOOR 2L SLIDE PRESSURE IN RED. Sep 8, 2008 · N854UA · Airbus A319131 · Escape SlideSDR 2008UALA05654Skin · damagedPREVIOUS SKIN BLEND AT FRAME 2 STR 23R OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.Sep 8, 2008 · N815UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR 2008UALA05656Sill · corrodedTHE 2R DOOR SILL CORRODED AT FWD SPLICE OUTBOARD SIDE, AT NUT CLIP HOLE. MAJOR REPAIR ACCOMPLISHED. STARTED TO REMOVE FASTENERS, INBOARD AND OUTBOARD ANGLES, NEW ANGLES FOR REPAIR IN WORK AREA. ACCOMPLISHED REPAIR PER MT 53-025. INSPECTED REPAIR.Sep 8, 2008 · N816UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR 2008UALA05658Floorbeam · corrodedFLOORBEAM 185 HAS CORROSION AT FR68 (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM. BEAM OUT AND ON BENCH WORKING. STARTED INSTALLATION OF BRACKETS. RIVETING OF STANDOFF BRACKETS IS WHAT IS LEFT. DRILLED AND INSTALLED NEW BEAM 185. ALL BRACKETS Sep 8, 2008 · N816UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05662Shear Tie · corrodedAFT RT SHEAR TIE CORRODED BETWEEN FRAME 69 & 70. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SHEAR TIE. INSTALLED SHEAR PLATE.Sep 8, 2008 · N816UA · Airbus A319131 · Fuselage Internal Mounting StructureSDR 2008UALA05659Floorbeam · corrodedFLOORBEAM 195 HAS CORROSION ALONG LENGTH (MARKED). MAJOR REPAIR ACCOMPLISHED. STARTED REMOVING FASTENERS. REMOVED SEVERAL FASTENERS FROM BEAM 190 TO REMOVE BEAM 195. BEAM REMOVED. INSTALLED 8 NUT PLATES ON BEAM 195 FOR PNL 261FF. SECURED NUT PLATES FOR FSep 8, 2008 · N816UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05661Floorbeam · corrodedFLOORBEAM 190 HAS CORROSION AFT OF FR68 (MARKED). MAJOR REPAIR ACCOMPLISHED. STARTED REMOVING FASTENERS. BEAM REMOVED. STARTED INSTALLATION OF BEAMS 190 AND 195. SECURED NUT PLATES FOR FLOORBOARD. INSTALLATION IS COMPLETE.Sep 8, 2008 · N816UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05657Floorbeam · corrodedFLOORBEAM 175 HAS CORROSION ALONG LENGTH BETWEEN FR68 AND FR70. MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM. INSTALLED LAV AND GALLEY MOUNT FITTINGS TO NEW FLOORBEAM. DRILLED AND INSTALLED BEAM. Sep 7, 2008 · N816UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05660Floorbeam · corrodedFLOORBEAM 140 HAS CORROSION ON ENTIRE LENGTH. MAJOR REPAIR ACCOMPLISHED. BEAM OUT AND ON BENCH WORKING. FAB'D SPLICES FOR BEAMS FORE AND AFT PRIMED, SEALED & INSTALLED AFT END TO BEAM 145, FWD READY TO INSTALL. INSTALLED SPLICE TO BEAM 80. REPLACED BEAM ASep 6, 2008 · N816UA · Airbus A319131 · Fuselage Main, Floor BeamSDR 2008UALA05642Oxygen System · faultyCREW OXY PSI SLOWLY DECREASING WITH NO CREW USE. IN ABQ CREW O21300 PSI - 1HR LATER 1200P. FOUND STICKY PRESS TO TEST PLUNGER AT 1ST OBSERVER'S LOCATION. REPLACED O2 MASK & BOX. OPS TEST OKAY. SERVICED CREW O2. NO SYSTEM BLEED DOWN WITHIN 45 MINUTES.Sep 6, 2008 · N806UA · Airbus A319131 · Crew Oxygen SystemSDR 2008UALA05585Door · out of adjustCREW REPORT: IN FLIGHT, DOOR 2R SHOWS DISARMED ON DOORS PAGE. DOOR INDICATES ARMED AT DOOR. FOUND DOOR OUT OF ADJUSTMENT. PERFORMED DOOR ADJUSTMENT, ALL OPERATIONS ARE NORMAL.. NO REPEATS SINCE ORIGINAL.Sep 3, 2008 · N826UA · Airbus A319131 · Service DoorsSDR 2008UALA05572Skin · corrodedRT WING TOP SKIN AT REFUEL PORT CUTOUT FLANGE HAVE PITTING CORROSION. REPAIRED PER UA-EVA-71896 AND REO-L01103. RECEIVED RAS-BAE-1008098-2008. TO BE REINSPECTED AT 123,500 CYCLES. CURRENT PTC 13082. INSPECTION INTERVAL AND METHOD TO BE DETERMINED BY AIRBUS ONSep 2, 2008 · N815UA · Airbus A319131 · Wing, Plate/SkinSDR 2008UALA05530Hydraulic System · lowLANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. AIRCRAFT TOWED TO GATE.Sep 1, 2008 · N827UA · Airbus A319131 · Hydraulic System, MainSDR 2008UALA05537Cover · missingEXIT PATH LIGHT COVER MISSING ON SEAT 1B.Aug 30, 2008 · N839UA · Airbus A319131 · Emergency LightingSDR 2008UALA05501Hydraulic System · overheatedGREEN HYD SYSTEM OVERHEAT AFTER TAKEOFF. FLIGHT DIVERTED.Aug 28, 2008 · N827UA · Airbus A319131 · Hydraulic System, MainSDR 2008UALA05483Landing Gear · vibrationNOSE GEAR VIBRATION. FLIGHT DIVERTED.Aug 26, 2008 · N840UA · Airbus A319131 · Nose/Tail Landing GearSDR UALA2008111305483Strut · lowNOSE GEAR VIBRATION. FLIGHT DIVERTED. SERVICED ALL THREE LANDING GEAR STRUTS, SHIMMED NLG LINKS, CHANGED NLG TIRES. FOUND LT MLG SHIMMEY DAMPNER WORN AND TORQUE LINKS AS WELL. REPLACED SAME.Aug 26, 2008 · N840UA · Airbus A319131 · Nose/Tail Landing Gear Strut/AxleSDR 2008UALA05470Structure · dentedFUSELAGE DENT AT STR 10R FRAME 34. *S/D* MAJOR REPAIR. INSTALLED DOUBLER REPAIR.Aug 25, 2008 · N815UA · Airbus A319131 · Fuselage Main, StructureSDR 2008UALA05465Unknown · unknownCABIN PRESSURE PROBLEM. RTFL. Aug 24, 2008 · N832UA · Airbus A319131 · Cabin Pressure Control SystemSDR 2008UALA05449Structure · dentedFUSELAGE DENT AFT OF FRAME 23 JUST BELOW STR 22L. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.Aug 24, 2008 · N815UA · Airbus A319131 · Fuselage Main, StructureSDR 2008UALA05410Skin · gouged21AUG ORD CF -T : NR 2 ENG RIGHT SIDE FAN COWL GOUGED APPROX 3 INCHES FROM REAR ABOUT 3 O'CLOCK POSITION. ACCOMPLISHED INTERIM REPAIR PER UA-EVA-71852, NO DELAMINATION PRESENT & APPLIED SPEED TAPE. RECHECK REPAIR AT NEXT A01 CHECK, REPAIR WITHIN 500 FLIGHT HAug 21, 2008 · N822UA · Airbus A319131 · Nacelle/Pylon, Plate/SkinSDR 2008UALA04344Gasket · crushedO2 LEAK. 70 PSI LOSS IN 30 MIN. FOUND CRUSHED GASKET LEAKING, AT CAPT O2 MASK. REPLACED CRUSHED GASKET AT CAPTAINS O2 MASK, ALL LEAK CHECKS GOOD.Aug 19, 2008 · N823UA · Airbus A319131 · Crew Oxygen SystemSDR 2008UALA04343Slide · faultyTHE 'ESPU EXT LOAD FWD L' FAULT DISPLAYED ON PTP DISPLAY DURING EMERGENCY LIGHTING TEST. ISOLATED FAULT TO DOOR 1R ESCAPE SLIDE. INSTALLED NEW SLIDE PACK (MR25611) AT DOOR 1R. Aug 19, 2008 · N805UA · Airbus A319131 · Escape Slide
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