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 CALA2014060991230Stringer · corrodedSTRINGER 33R BETWEEN FRAME 59 & 60 HAS LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-73-11. THICKNESS OF THE FLANGE IS 0.063. LOW READING AFTER BLENDING IS 0.037. MAX LOSS ALLOWED IS 0.0315, 0.5 X TC. WITHIN LIMITS IAW SRM 53-00- 13 FIG 202 SH 4 PG 231. Jun 5, 2014 · N844UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014060591210Circuit Board · burnedAT CRUISE 38000' FLIGHT ATTENDANT`S ADVISED OF BURNING SMELL IN THE AFT CABIN. AFTER INVESTIGATING FOUND BURNING, RUBBER SMELL BETWEEN FWD LAVATORY & LAST TWO ROWS OF SEATS. WORK TSM 24-00-00-810-823-A & 05-50-00-810-831-A. FOUND OVEN TRAY WITH BURNED FOOD Jun 3, 2014 · N820UA · Airbus A319131 · Passenger Compartment LightingSDR CALA2014060591212Sensor · faultyUNABLE TO RETRACT LG AFTER TAKEOFF. INSTALLED RT MLG EXTEND SENSOR 20GA IAW MM 32-31-73-400-001-A. FIRST SENSOR FROM STOCK WAS NO HELP. TRIED SECOND SENSOR & ALL WAS GOOD. SHOOK OUT WIRING FROM 20GA TO THE JUNCTION BOX ON TOP OF THE GEAR. RAN ENGS FOR 5 MJun 3, 2014 · N835UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2014060291183Door Sill · corrodedAFT CABIN R2 DOOR SILL HAS CORROSION FRAME 66 - 68, STRINGER 23R - 23R. R & R R2 DOOR SILL PN 5348004320701 & PN D5348004220701 IAW SRM 51-72-11. NO ADDITIONAL ACTIONS REQUIRED.Jun 2, 2014 · N844UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014060291184Stringer · corrodedAFT PIT HAS CORROSION LOCATED AT FRAME 61 - 64 STRINGER 41. R & R STRINGER LOCATED AT FRAME 61 - 64 STRINGER 41R PN D53476433200 IAW SRM 51-72-11. NO FURTHER ACTION REQUIRED.Jun 2, 2014 · N844UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014060291182Lug · gougedLT FWD PIT DOOR LATCH FITTINGS NR 2 FWD & AFT LUG & NR 3 FWD LUG WERE GOUGED ON THE RADIUS EDGE IN ZONE A. LUGS REWORKED IAW SRM 53-26-00 PAR 4 A. REMAINING MATERIAL THICKNESS IS FTG NR 2 FWD LUG 0.471 INCHES, AFT LUG 0.483 INCHES & FTG NT 3 FWD LUG 0.478 INMay 29, 2014 · N844UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014060291185Door Frame · crackedFRAME 68 WEB CRACKED AT DOOR 2L AFT LOWER STOP FITTING LOWER INBD HOLE. HOLE ENLARGED TO 0.510 INCHES & FREEZE PLUG REPAIR ACCOMPLISHED IAW SRM 53-41-12 PARA 5 C & PARA 5 F FIG 205. REQUIRES INSPECTION IAW SRI53-41-12-2-005-00 PARA 3 E TABLE 206, FIG 201. FIMay 29, 2014 · N846UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2014060291203Indication Sys · unknownAIR RETURN TO ORD FOR POSSIBLE GEAR INDICATION ISSUE.May 29, 2014 · N815UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2014052791167Battery Pack · not seatedEMERGENCY EXIT LIGHTS WILL NOT TEST PER 2 SERVICE. RESEATED LT EMER BATTERY PACK & FAULT CLEARED. RETESTED & GND CHECKED OKAY.May 27, 2014 · N829UA · Airbus A319131 · Emergency LightingSDR CALA2014052791143Eec · faultyENGINE 1 FADEC A FAULT. LCL MX REPORTED ENG 1 FADEC B FAULT, UNABLE TO ACCESS 1B VIA MCDU, GND SCAN FAULTING EEC1 CELL 48 FAULT CODE \XSWDOA. R & R NR 1 ENG EEC IAW AMM 72-22-34. CHECKS OKAY.May 25, 2014 · N834UA · Airbus A319131 · Fuel Control/Turbine EnginesSDR CALA2014052791142Container · faultyDURING PASS O2 DROP CHECK FOUND O2 MASK COMPARTMENT DOOR AT DOOR 2L DID NOT RELEASE DURING TEST. R & R EMERGENCY O2 CONTAINER & GENERATOR AT DOOR 2L. OPERATIONS CHECKED GOOD AT THIS TIME.May 23, 2014 · N814UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2014052791145Smoke Detector · false activationAVIONIC SMOKE MSG DISPLAYED ON TAXI OUT AT ENG SHUT DOWN. CYCLED AEVC CBS, SMOKE MSG CLEARED, BUT NOW HAVE VENT AVIONICS SYS FAULT, UNABLE TO CLEAR. ALSO, DUE TO SMOKE MSG, WILL NEED TO CYCLE FWC CBS BEFORE DISPATCH. AVIONICS COMPARTMENT SMOKE DETECTOR REPLMay 23, 2014 · N841UA · Airbus A319131 · Smoke DetectionSDR CALA2014052291119Oxygen Box · defectiveSEAT ROW 28ABC OXYGEN DOOR WILL NOT RESET AFTER DROP TEST, REQUIRES O2 BOX REPLACEMENT. SEAT ROW 28ABC INOPERATIVE. PSU PANEL SECURED CLOSED.May 22, 2014 · N837UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2014052291121Frame · corrodedFRAME 20RH INBD FLANGE BETWEEN Z=-520 & Z=-460 IS CORRODED AT FLOOR LEVEL IN THE MAIN CABIN. REMOVED CORROSION IAW ECRA 5311-01689 & SRM 51-74-00. NDT NOTED NO CRACKS. AIRBUS APPROVED THIS AS INTERIM MAJOR REPAIR WITH 6 MONTH LIFE LIMIT FROM REPAIR EMBODIMENMay 22, 2014 · N846UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2014052791144Actuator · malfunctionedSEAT ROW 28 ABC OXYGEN DOOR WILL NOT RESET AFTER DROP TEST. REPLACED ACTUATOR ON CONTAINER & OPERATIONS TESTED IAW AMM 35-23-00. OPERATIONS CHECKED GOOD.May 22, 2014 · N837UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2014110792659Frame · corrodedFRAME 20RT INBD FLANGE BETWEEN Z=-520 & Z=-460 IS CORRODED AT FLOOR LEVEL IN THE MAIN CABIN, DF9035. REMOVED CORROSION IAW ECRA 5311-01689 & SRM 51-74-00. NDT NOTED NO CRACKS. AIRBUS APPROVED THIS AS INTERIM MAJOR REPAIR WITH 6 MONTHS LIFE LIMIT FROM REPAIRMay 22, 2014 · N846UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2014051991057Skin · corrodedLEFT OVERWING FILLER ADAPTOR LAND UPPER SURFACE WAS FOUND CORRODED. CORROSION WAS REMOVED IAW SRM 57-21-11 PARA 5 E FIG 205. MAXIMUM MATERIAL LOSS WAS 0.017, MAX ALLOWABLE IS 0.020.May 19, 2014 · N846UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2014051991058Skin · corrodedRIGHT WING LOWER FUEL TANK PANEL LANDINGS 650 AB HOLE B & 640 MB HOLE K WERE FOUND CORRODED. HOLES WERE BUSHED & BRIDGING PLATES INSTALLED IAW SRM 57-21-11 PARA 5 B FIG 202. INSPECTION REQUIRED IAW SRI 57-21-11-2-002-00 3 B TBL 203. FIRST INSPECTION 43600FCMay 19, 2014 · N846UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2014051991059Skin · corrodedLEFT WING LOWER FUEL TANK PANEL LANDINGS 540 NB HOLES C & F & 540HB HOLE N WERE FOUND CORRODED. HOLES WERE BUSHED & BRIDGING PLATES INSTALLED IAW SRM 57-21-11 PARA 5 B FIG 202. INSPECTION REQUIRED IAW SRI 57-21-11-2-002-00 3 B TBL 203. FIRST INSPECTION 4360May 19, 2014 · N846UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2014051691028Door Sill · corrodedDOOR 2R SILL CORRODED AT FWD EDGE. R2 DOOR SILL & AFT CORNER FITTING REPLACED IAW SRM 51-21-11, 51-44-1 & 51-21-11.May 16, 2014 · N846UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014051991055Spar · wornNUMBER 2 PYLON LOWER SPAR HAD A .005 WEAR MARK ON THE PYLON LOWER SPAR FROM CONTACT WITH THE CNA. THE WEAR WAS BLENDED IAW SRM 54-51-12 FIG 103, & AN ANTI-CHAFING PLATE INSTALLED IAW SRM 54-51-12, 5B FIG 202. REPAIR WAS ACCOMPLISHED ON NR37572. REQUIRES INSPMay 16, 2014 · N846UA · Airbus A319131 · Nacelle/Pylon, Frame/Spar/RibSDR CALA2014051991056Spar · wornLT NR 1 PYLON LOWER SPAR HAD A .005 WEAR MARK ON THE PYLON LOWER SPAR FROM CONTACT WITH THE CNA. THE WEAR WAS BLENDED IAW SRM54-51-12 FIG 103, & AN ANTI-CHAFING PLATE INSTALLED IAW SRM 54-51-12, 5B FIG 202. REQUIRES INSPECTION IAW SRI 54-5 1-12-2-001-00 PARAMay 16, 2014 · N846UA · Airbus A319131 · Nacelle/Pylon, Frame/Spar/RibSDR CALA2014051691027Door Sill · corrodedL2 DOOR SILL HAS CORROSION AROUND NUTPLATE HOLE AT FRAME 68. REPAIRED THE AREA AT NP ATTACH HOLE IAW SRM 53-41-14 FIG 201 SH 1 - 3. REMOVED CORROSION & INSTALLED PLATE DOUBLER IAW ABOVE SRM.May 12, 2014 · N846UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014051391011Transceiver · faultyPREDICTIVE WIND SHEAR & WEATHER RADAR INTERMITTENT FAULT DISPLAYED. R & R WEATHER RADAR RT IAW AMM TASK34-41-33-000-0004-A & 34-41-33-400 -003-A, TESTED NORMAL.May 10, 2014 · N812UA · Airbus A319131 · Weather Radar SystemSDR CALA2014050990992Unknown · malfunctionedECAM ON TO SCREEN DIM & HARD TO READ. ABORT AT 60KTS. PFR HAS NO A & T ISSUE, CHECKED ALL FADEC LLR & EIU. NO FAULT NOTED. RESET FMGC 1 & 2 PRECAUTIONARY. PERFORMED NORMAL AFS & LAND TEST IAW MM 22-97-00. ACFT RETAINS CAT III STATUS.May 8, 2014 · N837UA · Airbus A319131 · Auto Flight SystemSDR CALA2014050990991Battery · dischargedEMERGENCY LIGHT TEST FAILED EPSU BATTERY FWD LT. REPLACED FWD LT EMER LIGHT BATTERY IAW MM33-51-39. OPERATIONS CHECKED NORMAL. BATTERY PN AD-3214-30.May 7, 2014 · N826UA · Airbus A319131 · Emergency LightingSDR CALA2014050690954Rivet · damagedRIVET HEAD MISSING INSIDE ENG 2 TAILPIPE AT APPROXIMATELY 1230 POSITION. R & R BAD RIVET IAW SRM 51-40 & CMM 78-11-11.May 4, 2014 · N812UA · Airbus A319131 · Engine Collector/Tailpipe/NozzleSDR CALA2014050690955Skin · crackedNR 2 ENG CHANGE, EXHAUST CONE SKIN HAS A CRACK EXCEEDING SIX INCHES AT THE 530 POSITION. REPLACED IAW MM-78-11-12- 400-010-A13.May 4, 2014 · N815UA · Airbus A319131 · Engine Collector/Tailpipe/NozzleSDR CALA2014050690956Transmitter · faultyBRAKE SYS 1 FAULT ON ENG 2 SHUTDOWN WITH MOMENTARY LOSS OF BRAKING. REPLACED BRAKE PEDAL TRANSMITTER. NO FAULTS ON BSCU BITES IAW AMM 32-42-47.May 4, 2014 · N837UA · Airbus A319131 · Landing Gear Brake SystemSDR CALA2014042190870Sill · corrodedCORROSION PRESENT ON R2 DOOR SILL ATTACH HOLES AT FRAME 68. INSTALLED REPAIR STRAP AT DOOR SILL AT FRAME 68 IAW SRM 53-41-14, REPAIR PRINCIPAL 4, FIG 201.Apr 20, 2014 · N826UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014042190871Oil System · lowAPU OIL QTY LESS THAN 3.9 QTS, PULSING GREEN, APU. APU OIL SERVICED IAW AMM49-90-00- 600-004-A.Apr 19, 2014 · N833UA · Airbus A319131 · APU Oil SystemSDR CALA2014042190872Skin · damaged2 EACH STATIC DISCHARGES ON LT FUSELAGE AFT OF FRAME 30 AT FUSELAGE CENTERLINE. ACCOMPLISHED PERMANENT REPAIR OF 2 EACH STATIC DISCHARGES ON CF 9019.Apr 18, 2014 · N848UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2014041490812Skin · unknownLEFT ELEVATOR S N CG 5192 LOWER SKIN, 8 AREAS INDICATING MOISTURE LOCATED 4.5 INCHES FROM TE & AT 32, 39, 81, 110, 162, 183, 195 & 202 FROM INBD END. DRILLED HOLES TO VERIFY WATER PRESENCE. ACCOMPLISHED REPAIRS IAW SRM 55-21-11, PARA 5E.Apr 14, 2014 · N848UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2014041490813Skin · unknownLEFT ELEVATOR S N CG 5192 UPPER SKIN 10 AREAS INDICATING MOISTURE LOC 5 FROM TE & AT 7, 32, 39, 82, 103, 148, 160, 180, 200 & 205 FROM INBD END & ONE AREA LOCATED AT APPROXIMATELY 17 INCHES FROM TE & 154 INCHES FROM INBD EDGE INDICATED MOISTURE. DRILLED HOLESApr 14, 2014 · N848UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2014041490814Fan · seizedCAPTAIN DIVERTED DENVER DUE TO SMOKE IN CABIN. LOUD NOISE & VIBRATION HEARD THEN STOPPED AS THEY WERE DIVERTING TO DENVER. PERFORM AMM TASK 05-51-10-200-801C1 DUE TO REPORT OF SMOKE SMELL. PFR SHOWS VENT EXTRACT FAULT 3 TIMES ON TAXI OUT. EXTRACT VENT FAULApr 13, 2014 · N851UA · Airbus A319131 · Air Distribution FanSDR CALA2014041490808Doubler · corrodedPREVIOUSLY INSTALLED DOUBLER IN FWD CARGO HAS CORROSION AT SKIN CUT OUT FRAME 26 - FRAME 27 & STRINGER 44R - STRINGER 41R. UPON FURTHER EVALUATION FOUND THE DOUBLER EXFOLIATED. REPLACED DOUBLER & FILLER IAW SRM 53-00-11 FIG 239 SH 2.Apr 11, 2014 · N845UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2014041490809Stringer · corrodedFWD CARGO COMPARTMENT STRINGERS HAVE CORROSION ON UPPER & LOWER SURFACES OF CROWN AT FRAME 26 - FRAME 27 & STRINGER 39L - STRINGER 42L. BLENDED CORROSION ON STRINGER & FOUND THE BLENDED AREAS TO BE OUT OF LIMITS SRM 53-21-13 FIG 101. FABRICATED NEW STRINGERSApr 11, 2014 · N845UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014041490810Stringer Splice · corrodedSTRINGER SPLICES HAVE CORROSION AT FRAME 27 - FRAME 28 & STRINGER 39L - STRINGER 42L. UPON FURTHER EVALUATION CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-73-11. R & R 4 EACH SPLICES AT ABOVE LOCATIONS IAW SRM 51-42-11 PARA 7.Apr 11, 2014 · N845UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014041090792Computer · faultySEVERE VIBRATION IN TAIL AT .76 AT FL240 IN CLIMB. ALL INDICATIONS NORMAL IAW SURVEY 05-50-00-810-8 01A. FOUND TO BE IN TAIL SECTION, PANEL 344DB RT ELEVATOR ACTUATOR PANEL LOOSE. PERFORMED ELEVATOR OSCILLATION TEST IAW 27-34-00, FOUND .005 - .008 ON BOTH SApr 9, 2014 · N812UA · Airbus A319131 · Flight Control SystemSDR CALA2014040890771Sill · corrodedR2 DOOR SILL CORRODED BEYOND LIMITS. REPLACED R2 DOOR SILL IAW SRM51-42-11.Apr 8, 2014 · N848UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014041090795Sill · corrodedL2 DOOR SILL HAS CORROSION AT FWD GIRT BAR FITTING THAT IS OUT OF LIMITS. INSTALLED REPAIR IAW SRM53-41-14 FIGURE 201 REPAIR PRINCIPLE 1.Apr 8, 2014 · N848UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014040390749Skin · saturatedRIGHT ELEVATOR UPPER SKIN PANEL HAS A TRAPPED WATER INDICATION 53.5 FROM INBD, 5 FROM TE, 2 DIAMETER. CUT OUT & SANDED AREA. REMOVED WATER, APPLIED REPAIR & RESTORED FINISH IAW UAL TC 4R5517310 PARA 3 5 & 3 6 & SRM 55-21-11 REPAIR 5A PG 215-217, 51-75-12 PARApr 3, 2014 · N845UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2014040390748Connector · unsecureSEAT EMERGENCY LIGHT AT SEAT ROW 8C INOPERATIVE. LIGHT ASSEMBLY CONNECTOR SECURED UNDER SEAT. NEED UNDER SEAT HARNESS IAW IPC 33-51-09-20C ITEM 40 PCN 565-2457.Apr 2, 2014 · N817UA · Airbus A319131 · Light System WiringSDR CALA2014033190721Sill · corrodedFASTENER HOLE CORRODED ON FRAME 68 RT AFT GIRT BAR MOUNT. CORROSION ON R2 DOOR SILL BEAM WAS OUT OF LIMITS IAW SRM 51-41-14 FIG 101. R & R DOOR SILL BEAM .Mar 31, 2014 · N845UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014033190722Stringer · corrodedCORROSION IN AFT PIT BILGE AREA ON STRINGERS & FASTENERS DOUBLER CUT OUTS FROM FRAME 63 - FRAME 64. R & R STRINGER 41RT FROM FRAME 58 - FRAME 64 IAW SRM 51-42-11, PG 7 E.Mar 31, 2014 · N845UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014033190723Stringer · corrodedCORROSION IN AFT PIT IN BILGE AREA ON STRINGER 43L BETWEEN FRAME 55 - FRAME 56. R & R STRINGER 43L FROM FRAME 53 - FRAME 60 IAW SRM 51-42-11.Mar 31, 2014 · N845UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014033190719Flight Recorder · faultedDFDR FAULT DISPLAYED ON UPPER ECAM. SYS FAULT ECAM AT PARKING INTERMITTENT. NO PREVIOUS HISTORY LAST LEG & PLR NO FAULTS. OPERATIONS CHECKED GOOD IAW AMM 31-33-00-710-007.Mar 30, 2014 · N816UA · Airbus A319131 · Data Recorders (Flight/Maintenance)SDR CALA2014033190720Stringer · corrodedBULK CARGO COMPARTMENT FRAME 65 - 66 STRINGER 31R HAS CORROSION. FRAME 65 - 69, STRINGER 31R FOUND CORRODED EXFOLIATED OUT OF LIMITS IAW SRM 51-73-11. R & R STRINGER IAW SRM 51-72-11 & SRM 51-42-11 AT LCQ HMV2 VISIT.Mar 29, 2014 · N845UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2014032790699Warning Message · activatedEGT OVER LIMIT DISPLAYED ON UPPER ECAM SCREEN DURING START. PEAK & TIME OVER 635C NOTED IN LOG BOOK, ENG 2. 1 SEC OVER 635. APU 18 PSI MAX DURING START. CREW REPORTED EGT WENT TO 635 FOR 1 SECOND, & THAT THEY HAD LOW APU PSI ONLY 24 PSI WITH PACS RUNNING. Mar 25, 2014 · N831UA · Airbus A319131 · Engine EGT/TIT Indicating SystemSDR CALA2014032490672Light · missingEMERGENCY EXIT LIGHTS AT SEATS 1B & 2B MISSING. REPAIRED EMERGENCY LIGHT AT 2B, 1B INOPERATIVE.Mar 24, 2014 · N803UA · Airbus A319131 · Emergency Lighting
Back to IAE V2522-A5