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 2008UALA05894Sill · corrodedR2 DOOR SILL HAS CORROSION AT FRAME 66 -Y1732. INSTALLED RE PAIR PER MT53-025 AND SRM53-41-14 ON NR K8545G.SDR 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.SDR 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.SDR 2008UALA05845Sill · corrodedCORROSION ON R2 DOOR SILL BETWEEN FR 67 AND 68. MAJOR REPAIR. CUT OUT DAMAGE AND INSTALLED REPAIR.SDR 2008UALA05824Sill · corrodedCORROSION ON L2 DOOR SILL FWD OF FR 68. REPAIRED PER SRM 53-41-14 ON NR K8564G.SDR 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.
SDR 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.
SDR 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.SDR 2008UALA05759Floorbeam · corrodedFLOORBEAM 150 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. ASSEMBLED AND PICKED UP HOLES. ATTACHED TO BEAM 95 AND STARTED INSTALLATION. INSTALLED BEAM.
SDR 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.
SDR 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.
SDR 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 FLSDR 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.
SDR 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.
SDR 2008UALA05740Cylinder · low pressureDOOR 1 RIGHT EMERGENCY OPERATION CYLINDER PRESSURE IS LOW. SERVICED CYLINDER. SERVICED CYLINDER, NO LEAKS NOTED AT TIME OF SERVICE.SDR 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.SDR 2008UALA05723Cover · missingEMERGENCY EXIT LIGHT COVER MISSING FROM FWD CLOSET BULKHEAD AT DOOR 1L. DISCOVERED COVER IS MISSING. REPLACED LIGHT ASSY. OP CHECKS GOOD.SDR 2008UALA05733Floorbeam · corrodedFWD GALLEY FLOORBEAM "A" HAS CORROSION AT FR16. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE.SDR 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.
SDR 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.SDR 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.SDR 2008UALA05667Stiffener · crackedSTIFFENER IN NOSE WHEEL WELL LEFT SIDE IS CRACKED ON THE RISER. REPAIRED STIFFENER PER SRM 57-11-16.SDR UALA2013031301498Skin · corrodedLEFT & RIGHT OUTER WING TOP SKIN AT REFUEL PORT CUTOUT FLANGE HAVE PITTING CORROSION. REPAIR PER EVA-71896 AND REO-L01103.SDR 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.SDR 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.SDR 2008UALA05664Floorbeam · corrodedFLOORBEAM Y254 HAS CORROSION BETWEEN FR65 AND FR66 (MARKED). REPLACED BEAM 160. REPLACED FLOORBEAM 160.SDR 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.SDR 2008UALA05648Slide · lowDOOR 2L SLIDE PRESSURE IN RED.
SDR 2008UALA05654Skin · damagedPREVIOUS SKIN BLEND AT FRAME 2 STR 23R OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 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.SDR 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 SDR 2008UALA05662Shear Tie · corrodedAFT RT SHEAR TIE CORRODED BETWEEN FRAME 69 & 70. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SHEAR TIE. INSTALLED SHEAR PLATE.SDR 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 FSDR 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.SDR 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.
SDR 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 ASDR 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.SDR 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.SDR 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 ONSDR 2008UALA05530Hydraulic System · lowLANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. AIRCRAFT TOWED TO GATE.SDR 2008UALA05537Cover · missingEXIT PATH LIGHT COVER MISSING ON SEAT 1B.SDR 2008UALA05501Hydraulic System · overheatedGREEN HYD SYSTEM OVERHEAT AFTER TAKEOFF. FLIGHT DIVERTED.SDR 2008UALA05483Landing Gear · vibrationNOSE GEAR VIBRATION. FLIGHT DIVERTED.SDR 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.SDR 2008UALA05470Structure · dentedFUSELAGE DENT AT STR 10R FRAME 34. *S/D* MAJOR REPAIR. INSTALLED DOUBLER REPAIR.SDR 2008UALA05465Unknown · unknownCABIN PRESSURE PROBLEM. RTFL.
SDR 2008UALA05449Structure · dentedFUSELAGE DENT AFT OF FRAME 23 JUST BELOW STR 22L. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.SDR 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 HSDR 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.SDR 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.
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