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 UALA2013053003757Fire Loop · shortedFIRE LOOP B FAULT DISPLAYED ON UPPER ECAM SCREEN. PERFORMED MT 26-001 AND TSM 26-12-00-810-808-A, FOUND FAN DETECTOR LOOP "B" HIGH RESISTANCE READING OUT OF LIMITS. R & R NR 2 ENG FAN LOOP ASSY. OPS CHECKED GOOD.May 26, 2013 · N838UA · Airbus A319131 · Fire DetectionSDR UALA2013053003750Oxygen Mask · damagedF/O OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). ANCHOR PIN ON HARNESS ON THE TOP LEFT IS SHEARED OFF. REPLACED F/O O2 MASK, OPS CHECKS GOOD NO LEAKS.May 25, 2013 · N808UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2013052303588Structure · damagedAFT PIT METAL EXPOSED. COLD WORK METAL BACK INTO SHAPE AND RETAPED. ALL OK.May 23, 2013 · N829UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR UALA2013052403617Floorbeam · crackedAFT CARGO FLOORBEAM SECTION ABOVE FRAME 56 FOUND CRACKED. REPAIRED.May 23, 2013 · N839UA · Airbus A319131 · Fuselage Main, Floor BeamSDR UALA2013052303584Shade · tornCAPTAIN`S SIDE WINDOW SCREEN RIPPED AT HANDLE. MYLAR PULL OUT SUN SHADE DAMAGED CAPT SIDE AFT OF SLIDING WINDOW SHADE, INOPERATIVE NOT USABLE. REPLACED CAPTAIN'S SIDE WINDOW SCREENMay 23, 2013 · N846UA · Airbus A319131 · Flight Compartment EquipmentSDR UALA2013052303587Cover · crackedR2 DOOR SLIDE DECORATIVE COVER HAS A 14 INCH CRACK HORIZONTALLY IN OUTER LAYER 4 INCHES FROM BOTTOM. ALSO, HAS 4 INCH CRACK IN OUTER LAYER EXTENDING 4 INCHES VERTICALLY. VISUAL INSPECTION ACCOMPLISHED, NO ADDITIONAL DAMAGE. BUSTLE IS RIGID. INSTALLED ONE 8May 23, 2013 · N826UA · Airbus A319131 · Escape SlideSDR UALA2013052303589Oxygen Mask · frayedFIRST OFFICER`S O2 MASK HOSE IS FRAYED. REPLACED O2 MASK IAW AMM, OPS CHECKED GOOD.May 23, 2013 · N853UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2013052303590Overheat Loop · shortedTROUBLESHOT LEFT WING LEAK DETECTOR LOOP "B". FOUND SEGMENT 61HF CENTER CONDUCTOR SHORTING TO GROUND. R & R LOOP 61HF IAW, OPS CK GOOD IAW AMM.May 22, 2013 · N842UA · Airbus A319131 · Overheat DetectionSDR UALA2013052203551Attach Fitting · damagedINTERCOSTAL ATTACH FITTING, AT FRAME C58 BETWEEN STR 2 AND 3R HAS ONE MISDRILLED HOLE IN FRAME C58. REPAIRED INTERCOSTAL ATTACH FITTING AT FRAME C58 BETWEEN STR 2 & 3R IAW ECRA 5340-01493 & EA130125. REPAIRED CEILING PANEL. INSPECTED REPAIR IAW ECRA 5340-0May 22, 2013 · N813UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR UALA2013052303580Switch · looseCAPTAIN`S MICROPHONE TRIGGER ON SIDE STICK IS LOOSE. REPLACED IAW AMM AND ACCOMPLISHED OP TEST OF SIDE STICK ASSY, OPS NORMAL.May 22, 2013 · N832UA · Airbus A319131 · Audio Integrating SystemSDR UALA2013052203548Trunnion · wornLEFT INBD FLAP TRUNNION WORN AT AREA D. BLENDED OUT DAMAGED AREA.May 21, 2013 · N816UA · Airbus A319131 · Wing, Control Surface Attach FittingsSDR UALA2013052303585Shroud · crackedRIGHT OVERWING SLIDE CRACKED SHROUD. REPLACED UNIT.May 21, 2013 · N813UA · Airbus A319131 · Escape SlideSDR UALA2013052203545Wire Harness · faultedFLAPS FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED FLAP WIRING AND OPS CHECKED GOOD.May 21, 2013 · N820UA · Airbus A319131 · Flight Control System WiringSDR UALA2013052303591Actuator · out of adjustRT ELEVATOR DURING GROUND CONTROL CHECK IN FULL UP POSITION SAGGED BUT WAS STILL IN BOX. CREW ALSO REPORTED ENROUTE, RT ELEVATOR NOW BELOW LEVEL BOX. PLANE FLYS NORMAL. COMPLIED WITH DDP. INDICATION PROBLEM ONLY. FOUND RIGHT ELEVATOR IS SAGGING, WHEN GREEN HYMay 21, 2013 · N843UA · Airbus A319131 · Elevator Control SystemSDR UALA2013052303582Floor Panel · delaminatedAFT CARGO FLOOR PANEL 151ZG FOUND DELAMINATED MEASURING ABOUT 17" X 24" EQUALING ABOUT 408 SQUARE INCHES. REMOVED FLOOR PANEL 151ZG AND CLEANED AREA IAW REPLACED AFT FLOOR PANEL 151ZG.May 20, 2013 · N806UA · Airbus A319131 · Fuselage Floor PanelSDR UALA2013052303583Floor Panel · delaminatedAFT CARGO FLOOR PANEL 151VG FOUND DELAMINATED MEASURING ABOUT 45" X 24" EQUALING ABOUT 1,080 SQ INCHES. REMOVED AFT CARGO FLOOR PANEL 151VG AND CLEANED AREA IAW MM. INSTALLED AFT CARGO FLOOR PANEL 151VG.May 20, 2013 · N806UA · Airbus A319131 · Fuselage Floor PanelSDR UALA2013052303581O-Ring · leakingEVIDENCE OF HYDRAULIC LEAK AT MLG AREA. CLEANED EXTERNAL PANELS & INSIDE RT MLG AREA. FOUND YELLOW HYD MODULE NEAR YELLOW HYD RESERVOIR LEAKING THREE DROPS IAW MINUTE. REPLACED O-RING ON YELLOW SYS HYD PRESSURE TRANSDUCER. OPS & LEAK CHECKED GOOD.May 19, 2013 · N806UA · Airbus A319131 · Hydraulic System, MainSDR UALA2013052003473Seat Back · looseF/O SEATBACK LT SIDE HAS LOOSE CONNECTION. REPLACED F/O SEAT.May 18, 2013 · N833UA · Airbus A319131 · Flight Compartment EquipmentSDR UALA2013052003472Computer · faultedECAM FLAP FAULT. POST FLIGHT REPORT SHOWS SFCC-1. REPLACE COMPUTER, SLAT FLAP CONTROL IAW AMM.May 18, 2013 · N820UA · Airbus A319131 · Trailing Edge Flap Control SystemSDR UALA2013052303592Pedal · lack of lubeF/O RUDDER PEDALS FAILED TO SPRING FWD FROM THE EXTENDED POSITION WHEN LEVER PULLED. RUDDER PEDAL ADJUSTMENT IS SERVICEABLE BUT REQUIRES UPGRADE. F/O PEDALS MOVE SLOWER THAN EXPECTED TO THE RETRACTED POSITION. LUBED AND OPS CHECKED OK IAW AMM.May 18, 2013 · N844UA · Airbus A319131 · Rudder Tab Control SystemSDR UALA2013052003456Seal · chafedL2 DOOR HAS CHAFING OF DOOR SEAL AT UPPER FWD CORNER OF DOOR. REPAIRED CHAFED DOOR SEAL CORNER IAW AMM. PRESSURIZED ACFT IAW MT52-020. NO LEAKS FOUND.May 18, 2013 · N831UA · Airbus A319131 · Passenger/Crew DoorsSDR UALA2013052003455Valve · faultyCREW REPORTED LOSING CABIN PRESSURE ON DESCENT. FAULTS INDICATE CABIN PRESSURE SAFETY VALVE HAS FAILED OPEN, ECAM 21-31, CABIN PRESSURE LOW DIFFERENTIAL PRESSURE, ECAM 21-31 CABIN PRESSURE SAFETY VALVE, REFER TO TSM 21-31-00-810-808, TSM 21-31-00-810-810. ACMay 17, 2013 · N805UA · Airbus A319131 · Cabin Pressure Control SystemSDR UALA2013052303586Oxygen Mask · leakingCAPTAIN`S O2 MASK LEAKS. SWAPPED MASK WITH SECOND OBSERVER'S. MASK DOES NOT LEAK WHILE STOWED. R & R O2 MASK.May 17, 2013 · N823UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2013051603381Mount · brokenSEAT 12DEF INBD AFT SEAT MOUNT BROKEN FASTENER. REPLACED AFT MOUNT.May 14, 2013 · N853UA · Airbus A319131 · Passenger Compartment EquipmentSDR UALA2013051403344Contact · damagedEVACUATION ALARM CHIRPS DURING POWER TRANSFERS. REPLACED GEN LINI CONTACT OR 9-XU2, TESTED OK.May 13, 2013 · N823UA · Airbus A319131 · Electrical Power System WiringSDR UALA2013051403356Cover · missingSEAT TRACK COVER MISSING AT ROW 27DEF. INSTALLED NEW SEAT TRACK COVER.May 13, 2013 · N849UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR UALA2013051403332Rub Strip · unsecureRUBBER STRIP HANGING DOWN AT ROW 22. SECURED STRIP AT ROW 22, OK FOR SERVICE.May 12, 2013 · N829UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR UALA2013051303322Sensor · faultyWHEEL NW STRG FAULT ECAM. ACCOMPLISHED CHECKLIST. CYCLED A-SKID N-W STRG SW OFF THEN ON. R & R RT NW STEERING FEEDBACK SENSOR IAW MM, OPS CHECKED GOOD.May 12, 2013 · N842UA · Airbus A319131 · Steering UnitSDR UALA2013051403331Warning Light · false activationALTERNATE LAW DISPLAYED AFTER ENGINE START. ADR1 FAULTED ON CFDS, NO ECAM CAUTIONS OR ADVISORIES , OR FAULT LIGHTS DISPLAYED. REACTIVATED ADIRU NR 2 AND ACCOMPLISHED TEST AMM 34-10-00-040-002 AND SFCC 1&2 AND ADR 1 & 2 TESTS, NO FAULTS. AFS LAND III TEST 2May 12, 2013 · N806UA · Airbus A319131 · Flight Environment DataSDR UALA2013051403355Sliding Window · delaminatedF/O SLIDING WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS. DELAMINATING UPPER LEFT. R & R FO'S SLIDING WINDOW PANE IAW AMM, CHECKED GOOD.May 12, 2013 · N829UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2013051003268Epsu · faultyEPSU EMERGENCY LIGHT FAULT DISPLAYED. REPLACED EPSU #11-WL PER AMM.May 10, 2013 · N808UA · Airbus A319131 · Emergency LightingSDR UALA2013051403354Power Supply · faultyEPSU EMERGENCY LIGHT FAULT DISPLAYED. REPLACED EPSU 11-WL PER AMM 33-51-28-000-001-A.May 10, 2013 · N808UA · Airbus A319131 · Emergency LightingSDR UALA2013051303308Cylinder · leakingLEFT MAIN GEAR UNLOCK ACTUATOR IS LEAKING. REPLACED LEFT MLG LOCK STAY ACTUATOR CYLINDER IAW AMM, CHECKED OK.May 10, 2013 · N807UA · Airbus A319131 · Landing Gear Retraction/Extension SystemSDR UALA2013051003270Battery Pack · failedFORWARD FLIGHT ATTENDANT CIDS PANEL FAILED EMERGENCY LIGHT TEST. REPLACED BATTERY PACK.May 9, 2013 · N813UA · Airbus A319131 · Emergency LightingSDR UALA2013051003269B-Nut · leakingNR 2 ENGINE LEAK CHECK FOUND IDG OIL COOLER RETURN LINE LEAKING. FOUND B-NUT LEAKING, TIGHTENED AND RAN ENGINE NO ACTIVE LEAKS NOTED AT THIS TIME.May 9, 2013 · N811UA · Airbus A319131 · AC Generator-AlternatorSDR CALA2013082690764Power Supply · faultyEPSU EMERGENCY LIGHT FAULT DISPLAYED. REPLACED EPSU NR 11-WL IAW AMM 33-51-28-000-001-A.May 9, 2013 · N808UA · Airbus A319131 · Emergency LightingSDR UALA2013050903264Controller · faultedNR 1 PACK OUTLET TEMPERATURE INDICATION INOPERATIVE ON BLEED SYSTEM ECAM PAGES. SWAPPED PACK CONTROLLERS 1 & 2 FOR TROUBLESHOOTING AND PROBLEM MOVED, RETURNED TO ORIGINAL CONFIG REF MM 21-61-34. PACK OPERATION IS NORMAL ONLY INDICATION ISSUE. REPLACED NR 1 May 8, 2013 · N817UA · Airbus A319131 · Cabin Temperature Control SystemSDR UALA2013050803234Tail Cone · crackedNR 1 ENGINE TAIL CONE HAS AN ELEVEN INCH CRACK REPORTED BY RAMP. REPLACED TAIL CONE PER AMM.May 7, 2013 · N819UA · Airbus A319131 · Engine Collector/Tailpipe/NozzleSDR UALA2013050703186Closeout Panel · crackedRIGHT WING INBD SLAT CLOSING PLATE CRACKED. RPL- :INSTALLED PANEL.May 7, 2013 · N801UA · Airbus A319131 · Leading Edge DevicesSDR UALA2013050703213Radome · damagedDURING BIRD STRIKE INSPECTION FOUND 14 IN DIA. BY 4 IN DEPTH. DENT ON CENTER OF RADOME. REPLACED RADOME IAW AMM 53-15-11-000-001A.May 6, 2013 · N809UA · Airbus A319131 · Aerodynamic FairingsSDR UALA2013050703214Paint · damagedBIRD STRIKE ON APPROACH. FOUND DAMAGE TO WEAR ABRASION RESISTANT PAINT ON LEFT WING OTBD FLAP INBD LEADING EDGE NEAR INBD FLAP FAIRING. NO OTHER DAMAGE NOTED.May 6, 2013 · N852UA · Airbus A319131 · Trailing Edge FlapsSDR UALA2013050703215Ptu · inoperativeWHILE TROUBLESHOOTING NOISE FOUND PTU INOP. REPLACED PTU REF AMM TASK 29-23-41-000-001-A.May 6, 2013 · N854UA · Airbus A319131 · Hydraulic System, AuxiliarySDR UALA2013050703171Gcu · no testEMERGENCY GENERATOR FAILED TEST PER EQ3022. REPLACED GCU. OPS CHECKED GOOD.May 6, 2013 · N817UA · Airbus A319131 · AC Generator-AlternatorSDR UALA2013050903239Control Unit · faultedRECORDER SYSTEM FAULT ECAM PRESENT. POST FLT MESSAGES RECORDER SYS FAULT, FDIU, DFDR. REPLACED FDIU.May 6, 2013 · N831UA · Airbus A319131 · Data Recorders (Flight/Maintenance)SDR UALA2013050603154Actuator · leakingCREW REPORTS NR 1 ENGINE LEAKING OIL. FBO REPORT LEAK IS HYDRAULIC FLUID FROM THRUST REVERSER INBD LOWER LOCKING ACTUATOR PISTON SEAL AT A RATE OF 8-10 DR OPS PER MIN. REF AMM 78-32-43-200-010-A OK TO CARRY FORWARD.May 5, 2013 · N819UA · Airbus A319131 · Engine Thrust ReverserSDR UALA2013050703203Floor Panel · delaminatedAFT CARGO BAY FLOOR PANEL 151VG DELAMINATED 34 INCHES X 17 INCHES. REPLACED AFT FLOOR PANEL IAW AMM 53-42-16 & 53-42-14.May 5, 2013 · N807UA · Airbus A319131 · Fuselage Floor PanelSDR UALA2013050703188Transceiver · faultyVHF 1 NOT TRANSMITTING ON 135.22. REPLACED NR 1 VHF.May 4, 2013 · N846UA · Airbus A319131 · VHF Communications SystemSDR UALA2013050703187Oxygen System · low pressureCREW OXYGEN SYSTEM LOW. SERVICED OXYGEN SYSTEM IAW TASK 35-11-41 AND TASK 12-14-35-600-001-A. NO LEAKS NOTED. BOTTLE SAFTIED AND ACCESS SECURED. OK FOR SERVICE.May 4, 2013 · N813UA · Airbus A319131 · Fuselage Main, StructureSDR UALA2013050203070Contactor · defectiveBCL 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ELEC ECAM MSG CAME ON INTERMITTENTLY. CFDS ATA 243800 CHECK CONTACTOR 6PB2-BCL2 CIRCUIT. ID:BCL2. REFER TO TSM24-38-00-810-813-A, FAILURE OF THE BATTERY 2 CONTACTOR PSBL CAUSES: 6PB2 565-0010, 1PB2 565-0073. REPLMay 1, 2013 · N852UA · Airbus A319131 · Battery/Charger SystemSDR UALA2013050203081Floor Panel · delaminatedAFT CARGO PIT FLOOR PANEL 151ZG IS DELAMINATED 24 INCH BY 22 INCH, 7.5 INCH FROM FWD EDGE AND 4 INCH FROM DOOR EDGE. IPC REF 53-42-04-22X ITEM 90, P/N BF530014-103. SRM REF 53-02-00 PG 120. REMOVED AFT CARGO PIT FLOOR PANEL IAW IPC 53-42-04-22X FLOOR PNL 110May 1, 2013 · N832UA · Airbus A319131 · Fuselage Floor Panel
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