IAE V2522-A5

Service difficulty reports · 3,464

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 CALA2014032490675Structure · corrodedFWD CABIN L1 & L2 FWD & AFT GIRT BAR FITTINGS HAS LIGHT CORROSION UNDER FITTING AROUND BOLT HOLES.Mar 24, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014032490674Cover · crackedLEFT NAV LIGHT COVER HAS 3 INCH CRACK. STOP DRILLED & TAPED OVER IAW AMM33-4199-350-001-A.Mar 23, 2014 · N826UA · Airbus A319131 · Exterior LightingSDR CALA2014031990633Battery Pack · failedEMERGENCY LIGHT BITE TEST FAILED BATTERY OVER LT WING 11WL. REPLACED BATTERY PACK 565-003 3 & EPSU POWER SUPPLY 565-6758 IAW TASK 33-51-38-400-002-A & 33-51-38-400-001-A, OPERATIONS GOOD.Mar 16, 2014 · N812UA · Airbus A319131 · Emergency LightingSDR CALA2014031290588Fitting · corrodedFWD CABIN L1 & L2 FWD & AFT GIRT BAR FITTINGS HAS LIGHT CORROSION UNDER FITTING AROUND BOLT HOLES.Mar 11, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014031290598Fitting · corrodedFWD CABIN L1 & L2 FWD & AFT GIRT BAR FITTINGS HAS LIGHT CORROSION UNDER FITTING AROUND BOLT HOLES.Mar 11, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014031090560Fastener · damagedLIGHTNING STRIKE DAMAGE AT RIVET AREA FRAME 8 APPROXIMATELY 9.5 INCHES RT OF TOP CTR LINE. R & R FASTENER.Mar 8, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014031090561Fastener · damagedLIGHTNING STRIKE DAMAGE AT RIVET AREA FRAME 13 APPROXIMATELY 10 INCHES RT OF TOP CTR LINE. R & R FASTENERS.Mar 8, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014031090562Fastener · damagedLIGHTNING STRIKE DAMAGE AT RIVET AREA FRAME 12 APPROXIMATELY 10 INCHES RT OF TOP CTR LINE, R & R FASTENERS IAW SRM 53-11-11-FG 208.Mar 8, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014031090563Fastener · damagedLIGHTNING STRIKE DAMAGE AT RIVET AREA FRAME 9 APPROXIMATELY 9 INCHES RT OF TOP CTR LINE. R & R FASTENERS IAW SRM 53-11-11-FG 208.Mar 8, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014031090558Wire Harness · brokenFOUND ON 2 SERVICE, EMERGENCY EXIT LIGHT IN SEAT ARMREST SIDE PANEL AT 31C IS OUT. FOUND HARNESS BROKEN AT CONNECTOR.Mar 7, 2014 · N844UA · Airbus A319131 · Light System WiringSDR CALA2014030790555Warning System · activatedECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN, APU.Mar 6, 2014 · N817UA · Airbus A319131 · APU Indicating SystemSDR CALA2014030790541Unknown · malfunctionedFUEL ON BOARD INDICATION INOPERATIVE ON FUEL SYS ECAM PAGE. FUEL CREW COMMENTS 1500 LBS FUEL UNACCOUNTED FOR OVER 20 MINUTES. CREW REPORTED RT FUEL QTY GAUGE WAS ERRATIC. FOLLOW TSM 28-11-00-810-806-A. ACCOMPLISHED MT 28-013, NO FAULTS FOUND. CHECKED SUMMMar 5, 2014 · N833UA · Airbus A319131 · Fuel Indicating SystemSDR CALA2014030790543Sill · corrodedR2 DOOR SILL BEAM CORRODED AT FRAME 66 & FRAME 68. R & R SILL BEAM IAW A319 SRM 51-42-11 PARA 6 & 7.Mar 5, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014030790544Battery · dischargedEMERGENCY LIGHT TEST FAILED AT EMERGENCY EXIT LT. REPLACED BATTERY AT EMERGENCY EXIT LT IAW AMM 33-51-38, EMERGENCY LIGHT TEST PASSED ON GND.Mar 5, 2014 · N826UA · Airbus A319131 · Emergency LightingSDR CALA2014030790545Stringer · corrodedAFT FUSELAGE STRINGER 26R AT FRAME 64 HAS CORROSION. R & R STRINGER IAW A-319 SRM 51-42-71 PG 25 PARA 7.Mar 5, 2014 · N850UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014030390503Connector · looseNR 1 FUEL VLV FAULT DISPLAYED ON UPPER ECAM. ECAM CAME ON AT ENG START BUT STARTED NORMAL. FAULT CLEARED BUT CAME BACK AT CRUISE, POSSIBLE FMU. ACCOMPLISHED COMPLETION OF FMU INSTALLATION, SECURED CANON PLUGS & CLAMP.Mar 1, 2014 · N813UA · Airbus A319131 · Engine Fuel System WiringSDR CALA2014030390504Actuator · out of adjustREVERSER FAULT DISPLAYED ON UPPER ECAM SCREEN WITH REVERSER INDICATION FLASHING AMBER. ENG 1 CREW COMMENTS ENG 1 REV ISOL FAULT, INOPERATIVE IAW MEL IAW PTT 3762002. HAD TO ADJUST LOCKING ACTUATOR TO GET SLEEVE TO LOCK OUT. SUGGEST REPLACING LOCK ACT & RIG IMar 1, 2014 · N823UA · Airbus A319131 · Engine Thrust ReverserSDR CALA2014030390505Blanking Plate · damagedSTATIC PORT BLANKING PLATE RT SIDE FWD OF NLG DOORS HAS BLENDING & PITTING MARKS. REPLACED BLANKING PLATE.Mar 1, 2014 · N843UA · Airbus A319131 · Pitot/Static SystemSDR CALA2014022590481Attach Bolt · damagedRT THS BOX SUPPORT ATTACH BOLT & FITTING HAVE SIGNS OF LIGHTNING DAMAGE AT FRAME 77 INBD END OF RT HORIZONTAL STABILIZER. FOUND BOLT REMOVED AT START OF DAYSHIFT. HAVE NEW BOLT & BUSHINGS IN HAND, HOWEVER UPPER BUSHING ITEM 90 NEEDS APPROXIMATELY .020 INCH Feb 25, 2014 · N834UA · Airbus A319131 · Horizontal Stabilizer Miscellaneous StructureSDR CALA2014022790485Stringer · corrodedCORROSION ON RT BULK CARGO COMPARTMENT STRINGER 31R AT FRAME 65.Feb 25, 2014 · N850UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014022790490Flap · malfunctionedAIR RETURN DUE TO FLAP SYS FAULT MESSAGE ON ECAM. FLAPS STUCK IN POSITION NR 2.Feb 25, 2014 · N809UA · Airbus A319131 · Trailing Edge Flap Control SystemSDR CALA2014022590475Thrust Reverser · faultedENG 2 REVERSER FAULT ON LANDING INOPERATIVE. THE REVERSER IAW MEL 7830N REVIEWED WITH TOMC.Feb 22, 2014 · N841UA · Airbus A319131 · Engine Thrust ReverserSDR CALA2014022590430Sill · corrodedR2 DOOR SILL FWD & AFT GIRT BAR PLATE ATTACH AREA HAS CORROSION. R & R DOOR SILL IAW SRM51-42-11.Feb 21, 2014 · N843UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014022590431Sill · corrodedAFT CABIN L2 DOOR SILL BEAM HAS CORROSION FRAME 68 Y 1292 FRAME 68. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR IAW A319 SRM 51-42-11 PARA 7.Feb 21, 2014 · N843UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014022190406Power Supply · inoperativeEMERGENCY LIGHT TEST FAILED ON 2 SERVICE. REPLACED RT OVERWING EPSU WL 12 & LT OVERWING EPSU BATTERY IAW MM33-51-38. ACCOMPLISHED OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW MM33- 51-00, OPERATIONS CHECKED GOOD.Feb 20, 2014 · N818UA · Airbus A319131 · Emergency LightingSDR CALA2014022190407Fitting · corrodedAFT CABIN CROSS BEAM RT END FITTING HAS CORROSION AT FRAME 70, STRINGER 23. ORIGINAL THICKNESS WAS 0.300 & REMAINING THICKNESS AFTER CORROSION REMOVAL IS 0.200. MATERIAL LOSS IS 0.100. OUT OF LIMITS IAW A319 SRM 51-73-11, PAGE 11. REMOVED DAMAGED FITTING &Feb 18, 2014 · N843UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014022190408Warning System · false activationCIDS CAUTION LIGHT ILLUMINATED. TOMC RESET, NO HELP. RETURN TO GATE, CIDS PANEL SHOWED NO FAULTS. CYCLED AIRCRAFT POWER & FAULT CLEARED.Feb 18, 2014 · N851UA · Airbus A319131 · Audio/Video MonitoringSDR CALA2014021790382Light · inoperativeEMERGENCY LIGHT TEST FAILED ON 2 SERVICE. RELAMPED OVERWING EMERGENCY EXIT LIGHT IAW MM 33-51-15, TEST PASSED.Feb 15, 2014 · N819UA · Airbus A319131 · Emergency LightingSDR CALA2014021290360Oil System · overservicedENG 2 OIL QTY GAUGE SHOWING AMBER XX. LATER OIL QTY INDICATOR BECAME NORMAL, SHOWING 26Q TS. REMOVED 2.5 QTS OF OIL IAW AMM 12-13-79, 5 MIN IDLE RUN QTY WITHIN ACCEPTABLE LIMITS & PRESENT IN ECAM AFTER ENG RUN, NO FURTHER SERVICE NEEDED.Feb 12, 2014 · N816UA · Airbus A319131 · Turbine Engine Oil SystemSDR CALA2014021090334Drum · damagedNR 2 ENG SN V11200 IAW EC3071-2 & EA 7241-01201, 7TH STAGE DRUM HAS MISSING COATING UNDER PATH OF PROBE HEAD, MISSING COATING AREA LARGER THEN PROBE. PICTURES POSTED ON RVI SITE. ENG MUST BE CHANGED PRIOR TO FLT.Feb 9, 2014 · N848UA · Airbus A319131 · Turbine Engine Combustion SectionSDR CALA2014021090330Light · inoperativeEMERGENCY LIGHT TEST FAILED. MESSAGE ATA 33-51-38, EPSU EXT LOAD FWD LT DISPLAY46. IAW MM 33 51 38, TRIED NEW POWER SUPPLY & BATTERY, NO HELP. REPLACED FWD EPSU & FAILED FOR SAME EXT LOAD FWD. NEW SLIDE REPLACED, RESET OVERWING EPSU & THEY CHECKED GOOD. REFeb 8, 2014 · N812UA · Airbus A319131 · Emergency LightingSDR CALA2014020690303Fitting · corrodedR2 DOOR SHAPE SEAL & AFT CORNER UNDER SCUFF PLATE HAS CORROSION FRAME 66 - FRAME 68 STRINGER 23R. CORROSION OUT OF SRM LIMITS. R & R AFT CORNER FITTING & SHAPE SEAL IAW A319 SRM 51-72-11.Feb 5, 2014 · N842UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014020390283Light · faultedEMERGENCY EXIT LIGHT TEST FAIL WITH EXTERNAL LIGHTS FAULT ON FWD LT BATTERY PACK 1L. TRIED NEW BATTERY & EPSU, NO HELP. 10WL A CONNECTOR PIN F RING OPEN FOR RT SLIDE 1R. SUGGEST SHUNT TEST MT33-01.Feb 2, 2014 · N819UA · Airbus A319131 · Emergency LightingSDR CALA2014020390291Battery Pack · dischargedIAW 2 CHECK EMERGENCY EXIT LIGHTING TEST FAILED WITH EXTERNAL LIGHTS FAULT ON FWD LT BATTERY PACK 1L. WHEN POWERED UP AT HANGAR EPSU HAD BATTERY FAULT. REPLACED BATTERY PACK IAW AMM33-51-38, ACP SHUNT TEST, SYSTEM CHECKED OK.Feb 2, 2014 · N819UA · Airbus A319131 · Emergency LightingSDR CALA2014020390292Sill · corrodedR2 DOOR SILL HAS CORROSION. REPLACED R2 DOOR SILL IAW SRM51-42-11 ON TIMCO NR 49490.Feb 2, 2014 · N842UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014013190266Start Valve · malfunctionedDURING NR 2 ENG START ATTEMPT, START VLV FAILED TO OPEN. CREW GOT THE ASSOCIATED ECAM MESSAGE. CONFIRMED NO DUCT PSI DROP & NO N2 ROTATION. ACCOMPLISHED A SECOND START ATTEMPT USING CROSS BLEED AIR FROM NR 1 ENG START VLV FUNCTIONED NORMALLY. NR 2 ENG GOODJan 30, 2014 · N826UA · Airbus A319131 · Engine Start Valves/ControlsSDR CALA2014012890251Cable · defectiveUNABLE TO ARM DOOR 2L. REF SEQ 4812004, ARMING CABLE REPLACED IAW AMM 52-13-22.Jan 28, 2014 · N826UA · Airbus A319131 · Passenger/Crew DoorsSDR CALA2014012790233Lens · crackedNOSE LANDING LIGHT LENS IS CRACKED. SYMM REPORTS SCREW HEAD IS STRIPPED. R & R NOSE LANDING LIGHT, OPERATIONS CHECKED GOOD. SCREW HEAD IS STRIPPED NEEDS SERVICE BULLETIN REQ UPGRADE CF944.Jan 26, 2014 · N837UA · Airbus A319131 · Exterior LightingSDR CALA2014012790234Stringer · corrodedFOUND STRINGER 26R CORRODED OUT OF LIMITS IAW SRM 51-74-00. REPLACED STRINGER 26R AT FRAME 65 IN BULK CARGO PIT IAW SRM 51-42-11 PARA'S 5, 6 & 7.Jan 26, 2014 · N842UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014012790232Support · wornAIR RETURN LAX DUE TO A NOSE GEAR INDICATION ISSUE. JACKED NOSE GEAR, FOUND PLAY IN TARGET SUPPORT PUTTING INDUCTANCE AT MINIMUM FOR SWITCH 25GA & 24GA, FOUND TARGET SUPPORT WORN WHERE PUSH ROD ATTACHES.Jan 25, 2014 · N833UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2014012890253Unknown · leakingFUEL LEAKING FROM NR 2 ENG.Jan 25, 2014 · N821UA · Airbus A319131 · Engine Fuel DistributionSDR CALA2014012490226Sensor · failedAIR RETURN LAX DUE TO A NOSE GEAR INDICATION ISSUE. BOTH LANDING GEAR SENSORS FAILED.Jan 24, 2014 · N833UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2014012290209Apu · shutdownECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN APU. NO START 2ND ATTEMPT, CREW ASSISTED BY TRYING ANOTHER APU START, START WAS GOOD. APU IS OPERATING NORMALLY, OK TO CONTINUE.Jan 21, 2014 · N855UA · Airbus A319131 · APU Core EngineSDR CALA2014012290210Seal · unsecureCREW NOTICED WHEN DEPARTING THE AIRCRAFT, WHAT APPEARS TO BE A BULB SEAL HANGING FROM THE AFT TE OF THE NR 1 ENG THRUST REVERSER ON THE RT HAND SIDE. REVERSER HALF OPENED FOR ACCESS WAS ABLE TO RESEAT BULB SEAL IN ITS TRACK, REVERSER CLOSED & SECURED, OK TO Jan 21, 2014 · N830UA · Airbus A319131 · Engine Thrust ReverserSDR CALA2014011590151Warning System · false activationENG 2 EIU FAULT. PAGE WRITER FAULTING START SWITCH SELECTOR. CYCLED SWITCH MESSAGE CLEARED, STARTED ENG NO FAULTS NOTED.Jan 14, 2014 · N821UA · Airbus A319131 · Engine Starting SystemSDR CALA2014011590162Computer · inoperativeFMGC NR 2 INOPERATIVE, FAILED IN FLIGHT.Jan 14, 2014 · N809UA · Airbus A319131 · Autopilot ComputerSDR CALA2014011390121Computer · inoperativeDMC 1 INOPERATIVE. SWAPPED DMC 1 WITH DMC 3 & PLACED ON MEL 3163C, ALL FUNCTIONS NORMAL IAW AMM 31-63-34 PB 401, PLACARD INSTALLED.Jan 11, 2014 · N817UA · Airbus A319131 · Central DisplaySDR CALA2014011390123Latch · defectiveOXYGEN MASKS DEPLOYED 34 ABC, STOWED MASK, O2 DOOR WILL NOT LATCH, SECURED O2 DOOR. SEATS 34 ABC NOT USEABLE, COMPLIED WITH MEL.Jan 11, 2014 · N843UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2014011390122Hose · damagedLEAK FOUND BELOW CHILLER UNIT AT LOWER PANEL, AT CHILLER DRAIN HOSE ATTACH FITTING. NEW CLAMP INSTALLED, NEEDS NEW HOSE, STILL LEAKS. REPLACED HOSE, LEAK CHECKED OK, REPLACED CHILLER, SUSPECT ICING IAW MM 25-34-51. OPERATIONS CHECKED OK, SECURED ALL PANELS.Jan 10, 2014 · N823UA · Airbus A319131 · Buffet/GalleysSDR CALA2014010890091Epr System · faultedDIVERTED TO IAD DUE TO AN EPR MODE FAULT ON THE NR 1 ENG.Jan 8, 2014 · N835UA · Airbus A319131 · Engine Pressure Ratio (EPR)
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