IAE V2522-A5

Service difficulty reports · 3,460

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 CALA2026102220518Elec Connector · fodBRAKES AUTO BRK FAULT ECAM ON FINAL APPROACH, DID CHECKLIST, CYCLED LANDING GEAR, NORMAL LANDING AND BRAKES POST FLT FAULTING BRK SELECTOR VALVE (23GG) ON BSCU 2. RAN NORMAL BRAKING AND LRU WIRING AND BSCU TEST BOTH FAULTING BRK SELECTOR VALVE (23GG). NO FAULTOct 22, 2026 · N804UA · Airbus A319131 · Landing Gear System WiringSDR CALA2026102220526Floor Support · crackedFWD CARGO, FRMS 28 - 34, STR 35R. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11/001 2E, SRM 51-44-11/001, SRM 51-46-11/00 1, & SRM 51-75-12-911-002.Oct 20, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026102120482Unknown · odorFUMES THROUGHOUT ACFT AFTER SHUTDOWN OF NR 2 ENGINE AND OPENING APU BLEED. RAN APU & BLEED TO VERIFY ODOR IN CABIN, ACCOMPLISHED INSPECTION IAW AMM 05-50-00-810-831-A. OPS APU FOR EXTENDED PERIOD & PACKS USING APU BLEED. NO ODORS NOTED DURING OPS.Oct 19, 2026 · N831UA · Airbus A319131 · Air Distribution SystemSDR CALA2026102120493Flashlight · no discrepancyAFT FLASHLIGHT NEAR FLIGHT ATTENDANT JUMPSEAT BATTERY FLASHING RED INOP STICKER INSTALLED ON THE AFFECTED FLASHLIGHT BY THE CAPTAIN. AFT OTBD FLASHLIGHT WORKING NORMAL. NO RED LIGHT, TESTING FUNCTION PRODUCES GREEN LIGHT CONSISTENT WITH OTHER FLASHLIGHTS. INOOct 17, 2026 · N831UA · Airbus A319131 · Emergency EquipmentSDR CALA2026101920451Hydraulic Line · leakingGREEN HYD SYS LOW PRESSURE. ECAM RUN MANUAL GEAR EXTENSION. FOUND HYD LINE LEAKING IN LEFT WING BETWEEN RIB 1 AND RIB 2. REMOVED LINE #30 REF IPC 29-11-05-02. REPLACED LEAKING LINE WITH SERVICABLE ONE REF LINE #30 REF IPC 29-11-05-02. LEAK CHECKS GOOD, RESETOct 15, 2026 · N802UA · Airbus A319131 · Hydraulic System, MainSDR CALA2026101620404Pump · leakingHYD G ENG 1 PUMP LO PR, HYD G SYS LO PR, GREEN SYS DEPLETED SDR INFO ADDED FOUND AN ACTIVE LEAK WITH HYD PRESSURE OFF ON LINE AT THE TOP OF NR 1 ENGINE OTBD SIDE. JUST BEHIND THE PYLON INTERFACE BRACKET. REPLACED DAMAGED PYLON HYDRAULIC LINE ON #1 ENGINE REF Oct 14, 2026 · N837UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), MainSDR CALA2026101320358Power Supply · faultedTEST OF THE EMERGENCY LIGHTS FAILS WITH EPSU INT LOAD EMER R, EPSU BATTERY AFT L AND EPSU UNIT EMER L MESSAGES. R&R RIGHT OVER WING EPSU REF AMM 33-51-400-001-A. R&R AFT BATTERY OF EPSU REF AMM 33-51-38-000-002-A. OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME.Oct 12, 2026 · N817UA · Airbus A319131 · Emergency LightingSDR CALA2026101320357Light · inoperativeAISLE SEAT 8C EMERGENCY LIGHT INOP. REMOVED AND REPLACED PATHWAY ILLUMINATION LIGHT ON SEAT 8C IN REFERENCE TO AMM 33-51-19. OPS CHECK GOOD. PARTS USED: BR9644-21,QTY :1Oct 11, 2026 · N811UA · Airbus A319131 · Emergency LightingSDR CALA2026101320315Floor Support · corrodedAFT CARGO COMPARTMENT FLOORBOARD PROFILE AT FR 58-59 STR 38L, FLOORBOARD RISER/RAMP CORRODED. REMOVED AND REPLACED AFT CARGO FLOORBOARD RISER AT FR 58-59 STR 38L IAW SRM 51-42-11 AND SRM 51-72-11-911-001.Oct 10, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026100920246Frame · crackedRIGHT FRAME 16 DOUBLE JOGGLE AREA HOLE 5, HAS A CRACK INDICATION IN CORNER DOUBLER LAYER AT 6 OCLOCK DIRECTION 100%. ACCOMPLISHED A REPAIR IAW REO L26059, REV IR, AND ECRA 5311-03084, REV A.Oct 8, 2026 · N824UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2026100820218Access Panel · damagedDURING REMOVAL OF ACCESS PANEL 540KB, ACFT SKIN WAS DAMAGED. EXCEEDED LIMITS OF SRM 57-21-11-300-002, INTERIM REPAIR PERFORMED TO FUEL ACCESS PANEL 540KB IAW PART 1 OF ECRA 5721-01445. ACCOMPLISH PERMINATE REPAIR AT LT WING BOTTOM FUEL ACCESS PANEL 540KB HOOct 7, 2026 · N848UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2026100720173Seat Track · corrodedCORROSION LOCATED AT SEAT TRACK Y-1292 AND FRAME 20. REMOVED SEAT TRACK Y-1292 FR12-FR24 IAW A319 SRM 51-42-11/001 RE V 159 PAR 2.F, REPLACED SEAT TRACK Y-1292 FR12-FR24 IAW A319 SRM 51-42-11/001 REV.159 PAR. 2.F.Oct 5, 2026 · N836UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2026100720181Seat Track · corrodedCORROSION ON SEAT TRACK Y-765 AND FRAME 20 2 AEREAS. REMOVED AND REPLACED SEAT TRACK 765 IAW A319 SRM 51-42-11 FROM F R12-FR24.Oct 5, 2026 · N836UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2026100520102Fuel Cap · missingMISSING FUEL CAP UPON ARRIVAL. INSTALLED A FUEL CAP.Oct 3, 2026 · N823UA · Airbus A319131 · Fuel StorageSDR CALA2026100620130Floorbeam · corrodedAFT WET AREA, LT FLOOR BEAM Y160.5, BARREL NUT CORRODED IN LAV MOUNT FITTING, JUST AFT OF FR 68. REMOVED AND REPLACED L/H FLOOR BEAM Y160.5 FR68-70 IAW A319 SRM 51-72-11-911-001Oct 3, 2026 · N836UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2026100620132Window Frame · crackedRIGHT WINDSHIELD FRAME CONTINUITY FITTING AREA ROTO TEST INSPECTIO N FOUND CRACK INDICATION IN MOST I/B HOLE GEN BY V929087 ON AAR LCQ NR 9298821/26821 UP DATED EFSR REPAIRED R/H WINDSHIELD FRAME MOSL I/B FASTENER HOLE IAW A319 EC RA NO.5311-03421 OVERSIZE ANDOct 3, 2026 · N836UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026100520071Light · disconnectedEMERGENCY LIGHTS AT SEATS 27C AND 28C WILL NOT ILLUMINATE. FOUND LIGHT ASSEMBLIES AT SEATS 27C AND 28C TO BE DISCONNECTED. CONNECTED LIGHTING ASSEMBLIES AND PERFORMED OPS CHECK IAW AMM 33-51-00. OPS CHKD GOOD.Oct 2, 2026 · N848UA · Airbus A319131 · Light System WiringSDR CALA2026092920000Floor Support · corrodedAFT CARGO BAY FLOOR SUPPORT, FR 52-56, STR38L HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-41-4.Sep 29, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026092920004Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR BOARD PROFILE AT FR 56-58 STR38L HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR BOARD PROFILE A T FR56-58 STR 38L IAW A319 SRM 51-44-11.Sep 29, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026101320340Feeder Cable · damagedDURING ALI VISIT, FOUND RT PYLON IDG FEEDER CABLE WIRE 2422-4519 INSULATION DAMAGED UNDER PANEL 521BT BETWEEN RIB 5A & PS 6480/RIB09 STA MLB. PERFORMED DAMAGE ASSESSMENT OF RT PYLON WIRE 2422-4519 IAW ESPM 20-53-21-02. REPAIRED WIRE WITH A GRADE 3 TEMP REPAIRSep 27, 2026 · N827UA · Airbus A319131 · Electrical Power System WiringSDR CALA2026092819919Skin · damagedLEFT TOP & BOTTOM SKIN PANEL FOUND LIQUID ENGRESS INDICATION AT 160" FROM INBD EDGE, AND 9 1/2" FROM T/E. DEFECT IS 2 INCHES IN SIZE. REPAIRED THE LT ELEVATOR TOP SKIN 160IN FROM INBD EDGE 9.5IN FROM T/E 2 INCHES IN DIA IAW SRM 55-21-11-300-005.Sep 25, 2026 · N836UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2026092819921Skin · damagedLEFT TOP SKIN PANEL FOUND LIQUID ENGRESS INDICATION AT 146 INCHES FROM INBD EDGE AND 12 1/2 INCHES FROM T/E. DEFECT IS 1 3/4 INCH IN SIZE. REPAIRED THE LT ELEVATOR TOP SKIN IAW SRM 55-21-11-300-005. CATEGORY A REPAIR.Sep 25, 2026 · N836UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2026092519834Panel · corrodedAFT CARGO COMPARTMENT SLOPING PANEL PROFILE AT FR 54-56, STR 35R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO SLOPING PANEL PROFILE IAW SRM 51-42-11.Sep 24, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026092519836Floor Support · corrodedAFT CARGO BAY FLOOR SUPPORT AT FR 59-63, STR 38L HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED THE AFT CARGO PROFILE PANEL IAW SRM 51-42-11.Sep 24, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026092519838Floorbeam · damagedFWD CARGO FLOORBEAM, FR28, STR 38R-38L HAD MULTIPLE ELONGATED HOLES . REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11-001A,Sep 24, 2026 · N836UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2026092819854Oil System · lowENG 1 LOW OIL, AFTER ROTATIONIND 4.5 QT AFTER LEVEL OFF 6-8 QT ENGINE 1 FAN COWLS AND THRUST REVERSERS OPENED TO PERFORM VISUAL INSP OF ENGINE. NO LEAKS NOTED. SERVICED ENGINE WITH 9 QUARTS OF OIL AND PERFORMED DRY MOTOR OF ENGINE 1 IAW AMM TASK 71-00-00-710-0Sep 24, 2026 · N814UA · Airbus A319131 · Turbine Engine Oil SystemSDR CALA2026092519805Fitting · corrodedL2 DOOR CUTOUT, AFT CORNER FITTING CORRODED. REMOVED AFT CORNER ON L2 DOOR IAW SRM 51-42-11/001, REV 159, PAR 2.G, 2.F. REPLACED THE AFT CORNER ON L2 DOOR IAW SRM 51-42-1 1/001, REV 159. PARA 2.E,2.F.Sep 23, 2026 · N836UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026092819868Profile · corrodedFWD PIT PROFILE AT FR 27, S38L WAS CORRODED. REMOVED AND REPLACED FWD PIT PROFILE IAW SRM 5 1-42-11.Sep 23, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026092419768Fitting · corrodedFRAME 68 HAS A DRILLED OUT FASTENER WITH CORROSION AROUND IT AFT CABIN. REMOVED AND REPLACED FITTING AT AFT CABIN FLOOR IAW SRM 51-42-11.Sep 21, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026092519801Panel · missingFOUND NR 1 PYLON SECTION PANEL MISSING, REF IPC 54-57-22-07A, ITEM 90, DETERMINED TO BE CATEGORY 2 50.75 SQ-IN R & R THE PYLON TO NACELLE PROFILE PANEL INBD IAW AMM 54-57-22.Sep 21, 2026 · N818UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR CALA2026092219660Panel · crackedFWD CARGO LT BOTTOM SLANT FLOOR PROFILE HAD MULTIPLE CRACKS AROUND FASTENER HOLES AT FR 28 +10 IAW AAR LCQ N/R 9298507/26507. REMOVED AND REPLACED FWD CARGO PROFILE PANEL IAW SRM 51-42- 11.Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026092219662Seal · crackedRIGHT PYLON FWD INBD BLADE SEAL CRACKED. REMOVED AND REPLACED BLADE SEAL AT RT PYLON FWD INBD IAW SRM 51-42-11.Sep 19, 2026 · N836UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR CALA2026092219664Panel · crackedFWD CARGO RT BOTTOM SLANT TO FLOOR PROFILE STR 38 HAD A CRACK AT FR 28 +1. REMOVED AND REPLACED PROFILE PANEL ON FWD CARGO BAY IAW SRM 51-42-11-001.Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026092219666Floorboard · corrodedAFT CARGO BAY CENTER FLOORBOARD AT FR 51 HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO PROFILE PANEL AT FR57 IAW SRM 51-42-11.Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor PanelSDR CALA2026092219668Floorboard · corrodedAFT CARGO COMPARTMENT FLOORBOARD AT FR 59 - 63, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO FLOORBOARD IAW SRM 51-42-11.Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor PanelSDR CALA2026092219670Floorboard · corrodedAFT CARGO BAY, FLOORBOARD AT FR 51-52, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED THE FLOORBOARD IAW SRM 51-42-11.Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor PanelSDR CALA2026092219672Floorboard · corrodedAFT CARGO BAY FLOORBOARD AT FR 52-56, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED FLOORBOARD IAW SRM 51-42-11.Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor PanelSDR CALA2026092119613Wire Harness · faultedNORMAL START ON NUMBER 1 ENGINE. REJECTED TAKEOFF APPROX 60 KNOTS DUE TO NR 1 EGT READING 162 DEGREES. OTHERWISE NORMAL ENGINE INSTRUMENTS AND ACCELERATION NO SWERVING. ADDED FADEC 1B TEST RESUT PICTURE REF TSM 77-20-00-810-801-B, PERFORMED ENG 1 ECTRICAL CASep 18, 2026 · N807UA · Airbus A319131 · Engine Fuel System WiringSDR CALA2026092119615Panel · corrodedFWD CARGO SLOPING PANEL VERTICAL PROFILE 10" FWD OF FR30, STR 38R CORRODED. REMOVED AND REPLACED FWD CARGO PROFILE PANEL AT FR 30, STR 38R IAW SRM 51-42-11.Sep 18, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026092119617Support · corrodedAFT WET AREA, LT FR 69 - 70, SHEAR PLATE SUPPORT CORRODED. REMOVED AND REPLACED SHEAR PLATE SUPPORT ON AFT WET AREA BTW FR 70 -FR 69 LT STR 23 IAW SRM 51-42-11.Sep 18, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026092119626Frame · corrodedAFT CARGO FR 59 HAD CORROSION AT FASTENER HOLES. PERFORMED PERMANENT A REPAIR AT FR 59 IAW EC/RA 5341-01583.Sep 18, 2026 · N819UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2026101220280Gusset · crackedFRAME 66, STRINGER 14R, GUSSET PLATE MIDDLE HOLE IS VISIBLY ELONGATED IN GUSSET PLATE LAYER. THE GUSSET PLATE WAS R & R IAW SRM 53-41-12-300-018, FIGURE 1.Sep 18, 2026 · N836UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026091819548Door Frame · crackedRIGHT EMERGENCY EXIT, FWD LOAD TRANSMITTING PROFILE SHOWS SIGNS OF CRACKING. REMOVED & REPLACED THE FRAME SEGMENT IAW SRM 51-72-11-911-001, & SRM 51-42-11-001.Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026092219642Shear Plate · corrodedAFT WET AREA, RT FR 69 - 70,SHEAR PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11/001 AND 5 1-72-11-911-002.Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026092219644Door Sill · corrodedL2 DOOR SILL HAS CORROSION JUST INBD OF AFT GIRT BAR FITTING. EVALUATED & REPAIRED L-2 DOORSILL JUST INBD OF AFT GIRT BAR FITTING, REPAIR/EVAL FOUND TO BE CATEGORY A NO FURTHER ACTION REQUIRED IAW SRM 53-41-14-300-001, & 53-41-14-283-002.Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026101220271Gusset · crackedFR 66, STR 16L GUSSET PLATE TOP HOLE HA S A REJECTABLE INDICATION. GUSSET PLATE REMOVED AND REPLACED IAW SRM 53-41-12-300-018, FIGURE 1. FLOWCHART SOLUTION 1. GVI & HFEC INSPECTION COMPLETED PER NTMS 51-90-00, 5110-08 AND 51-10-01. NO DAMAGE FOUND ON FRAME ISep 17, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026101220275Gusset · crackedFRAME 68, STRINGER 12R, GUSSET PLATE MIDDLE HOLE IS VISIBLY ELONGATED IN GUSSET PLATE LAYER. GUSSET PLATE R & R IAW SRM 53-41-12-300-018, FIGURE 1.Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026101220277Gusset · crackedFRAME 68, STRINGER 14L GUSSET PLATE 2ND HOLE FROM BOTTOM IS VISIBLY OUT OF ROUND. THE GUSSET PLATE WAS R & R IAW SRM 53-41-12-300-018, FIGURE 1.Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026091719510Fuel Cap · missingFUEL CAP MISSING, CAP FOUND MISSING UPON ARRIVAL. EWR WAS PREVIOUS STATION THEY DID NOT FIND THE CAP AT THIS TIME. INSTALLED A NEW FUEL CAP IAW AMM 28-25-41-400-005-A. REMOVED PLACARD.Sep 13, 2026 · N846UA · Airbus A319131 · Fuel StorageSDR CALA2026091519458Fuel Cap · missingPDA 2 FUELER REPORTING FUEL CAP MISSING REPLACED MISSING FUEL CAP P/N 0727540 PER AMM 28-25-41-00 PARTS USED: 31-2825-9-0001,QTY :1 MFG PN ON - 0727540 MFG SN ON - C260145 M&E SN ON - 00145 M&E PN ON - 31-2825-9-0001 MFG SN OFF - UNABLE TO IDENT MFG PN OFF - Sep 10, 2026 · N823UA · Airbus A319131 · Fuel Storage
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