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 2003UALA00675Frame · damagedAFT PIT FRAME 54L DAMAGED AT STR 38L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00612Skin · damagedSKIN DAMAGE AFT LOWER OF DOOR 2L BETWEEN FRAMES 69 AND 70 AT STRINGER 23L. MAJOR REPAIR ACCOMPLISHED. EXTERNAL SKIN DOUBLER INSTALLED.SDR 2003UALA00603Warning Light · failedFLIGHT DIVERTED DUE TO PRESSURIZATION FAILURE. REPLACED CPC1 AND SKIN AIR OUTLET VALVE.SDR 2003UALA00584Connector · looseDVTD TO MCI DUE TO LGCIU 1 FAULT ON ECAM / ELECT CONNECTOR LOOSE ON SENSOR. REPLACED THE LGCIU.SDR 2003UALA00560Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED THE LANDING GEAR LEVER. REPLACED THE LANDING GEAR CONTROL AND INTERFACE UNIT (LGCIU). UNIT FAILED TEST 6DA AND 6BC DUE TO DEFECTIVE SOLDER JOINTS.SDR 2003UALA00486Proximity Sensor · dirtyFWD CARGO MESSAGE DISPLAYED ON UPPER ECAM SCREEN. CLEANED CARGO DOOR PROXIMITY SENSOR.SDR 2003UALA00485Door · openECAM WARNING AFTER TAKEOFF. AFT AVIONICS COMPARTMENT DOOR OPEN. RETURN TO FIELD. LUBRICATED AFT AVIONIC COMPARMENT DOOR PROXIMITY SWITCHSDR 2003UALA00472Warning System · malfunctionedRETURNED TO FIELD DUE TO SMOKE INDICATION IN THE AVIONICS COMPARTMENT. *SUPPLEMENTAL DATA UPDATE* ACCOMPLISHED AIRBUS TSM TASK 21-26-00-810-813, VISUAL CHECK OF AVIONICS COMPARTMENT, TESTS OF AEVC & FWC 1 & 2. NO DEFECTS OR DISCREPANCIES NOTED. NO FURTHER SDR 2003UALA00437Computer · malfunctionedFLIGHT DIVERTED DUE TO STALL WARNING AND MASTER CAUTION LIGHTS. SUPPLEMENTAL DATA UPDATE THE SPURIOUS STALL WARNING WAS CAUSED BY A FAULTY FLIGHT WARNING COMPUTER (FWC) AND WAS CORRECTED BY REPLACING NR 1 FWC.SDR 2003UALA00418Valve · malfunctionedABORTED TAKEOFF DUE TO A VENT AVIONIC FAULT. ABORTED A 2ND TIME FOR THE SAME REASON. SUPPLEMENTAL DATA UPDATE SKIN AIR OUTLET VALVE SUBSEQUENTLY REPLACED (AFTER BEING FAULTED) AND NO FURTHER DISCREPANCIES REPORTED.SDR 2003UALA00414Angle · bentANGLE SUPPORTS ARE BENT UNDER THE LOWER ACCESS PANEL ON AFT CARGO DOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SUPPORT ANGLES.SDR 2003UALA00417Check Valve · leakingYELLOW SYSTEM LOW LEVEL LIGHT ILLUMINATED AND ECAM SHOWS 0 QUANTITY. FOUND LEAK AT HYD CHECK VALVE IN PTU MANIFOLD REPLACED CHECK VALVE AND FILLED YELLOW SYSTEM AND LEAK CHECKED SYSTEM NO LEAKS FOUND.SDR 2003UALA00415Stringer · damagedAFT OF DOOR 2L AT THE FLOOR LINE THERE IS STRINGER & SKIN DAMAGE. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER AND INSTALLED DOUBLER REPAIR ON SKIN.SDR 2003UALA00281Rub Strip · debondedDIVERTED DUE TO NR 1 ENGINE COMPRESSOR STALL. COMPRESSOR STALL CAUSED BY HIGH PRESSURE COMPRESSOR (HPC) 6TH STAGE (C6) BLADE DAMAGE WHICH WAS IN TURN CAUSED BY HPC C6 RUBSTRIP COATING DISBONDING. SERVICE BULLETIN 72-0369 IS IN PLACE TO UPGRADE COATING TO AVOSDR 2003UALA00280Transceiver · intermittentDIVERTED DUE TO INOPERATIVE WEATHER RADAR. REPLACED WEATHER RADAR TRANSCEIVER, SYSTEM GROUND CHECKS OK AND CFDS SELF TEST NORMAL.SDR 2003UALA00190Fmu · inoperativeDURING CLIMBOUT NR 2 ENGINE SHUTDOWN DUE TO FMU ECAM WARNING. FUEL METERING UNIT (FMU) REPLACED,SDR 2003UALA00156Ram Air Turb · failedRAT TEST FAILED RPM TEST. REPLACED RAM AIR TURBINE.SDR 2003UALA00001Windshield · crackedCAPTAINS WINDSHIELD OUTER PANE CRACKED. SUPPLEMENTAL DATA UPDATE LOWER BUS BAR ARCED DUE TO DELAMINATION AND WATER INGRESSION CAUSED BY WEATHER SEAL DETERIORATION. WINDSHIELD WAS REPLACED.SDR 2002UALA01895Power Supply · faultyRECEIVED 'EPSU FWD L' MESSAGE ON FWD FLT ATTENDANT PANEL. REPLACED EMERGENCY POWER SUPPLY UNIT. OPS CHECKED OK.SDR 2002UALA01893Control Unit · failedANTI-SKID NWS MESSAGE ON ECAM. LOST ANTISKID AND NOSE WHEEL STEERING. AIRCRAFT TOWED TO GATE. SUPPLEMENTAL DATA UPDATE RECYCLED BSCU CB'S M33,M34,M35 & M36, SYSTEM RETURNED TO NORMAL WITH NO FURTHER DEFECTS.SDR 2002UALA01862Transducer · failedBRAKE STEERING CONTROL UNIT CHANNEL 1 ECAM MESSAGE IN FLIGHT. *S/D* FAILURE OF THE NORMAL BRAKE PRESSURE TRANSDUCER (12GG) AS IDENTIFIED BY THE BSCU. REPLACED NORMAL BRAKE PRESSURE TRANSDUCER (12GG) AND PERFORMED OPERATIONAL CHECKS.SDR 2002UALA01754Strut · incorrectUNABLE TO RETRACT LANDING GEAR. THE NLG LOWER STRUT ASSEMBLY WAS FOUND TO BE ASSEMBLED INCORRECTLY. THE UPPER CAM WAS MISALIGNED PREVENTING THE SHOCK ABSORBER LUGS FROM ENGAGING INTO THE SHOCK STRUT BACKPLATE. THE NLG LOWER STRUT ASSEMBLY, WHEELS, TIRES ANDSDR 2002UALA01745Skin · dentedFUSELAGE SKIN DENTED BETWEEN STRINGER 28L AND 29L, 2" AFT OF FRAME 18 STA 760 DAMAGE IS AT THE SKIN LAP. MAJOR REPAIR ACCOMPLISHED. SKIN DOUBLER REPAIR.SDR 2002UALA01670Battery · discharged"EPSU BATTERY L" MESSAGE DISPLAYED AFTER EMERGENCY LIGHTS TEST. REPLACED BATTERY ASSEMBLY.SDR 2002UALA01642Iru · malfunctionedLOST CAPTAIN'S AIRSPEED TAPE INDICATION ON ROTATION. REPLACED AIR DATA INERTIAL REFERENCE UNIT NR 1. BUILT IN TEST EQUIPMENT CHECKED GOOD.SDR 2002UALA01588Valve · failedNR 2 RIGHT HAND THRUST REVERSER TRANSLATING SLEEVE COWL DELAMINATED ON FORWARD ACOUSTIC SKIN. CAUSED BY HEAT OF FAILED VALVE IN THE OPEN POSITION FOR 10TH STAGE BLEED VALVE. ENGINE VIBRATION SURVEY ACCOMPLISHED ON GROUND, WITH FAILED VALVE, LEADING TO UNUSUASDR 2002UALA01578Seal · debondedLANDED UNDER AMBER ALERT DUE TO CRACKED RIGHT WINDSHIELD. THE DISBONDING OF THE WHITE SILICONE PRESSURE SEAL ALLOWED WATER TO ENTER THE BUS BAR AREA WHICH RESULTED IN ARCING AND SHATTERED THE WINDOW OUTER PLY. THE WINDOW WAS REPLACED.SDR 2002UALA01485Manifold · damagedRETURNED TO FIELD DUE TO A YELLOW HYDRAULIC LOW LEVEL INDICATION. FOUND TOP CENTER PLUG OF YELLOW SYSTEM LEAKAGE MEASUREMENT VALVE BLOWN OUT. REPLACED GROUND LEAKAGE-MEASUREMENT MANIFOLD OF THE YELLOW SYSTEM, SERVICE YELLOW SYSTEM TO FULL.SDR 2002UALA01279Slide · faultyDURING NR 3 SERVICE CHECK OF EMERGENCY LIGHTING SYSTEM FOUND EPSU EXT LOAD AFT L FAULT. POWER SUPPLY SHOWS EXT LOAD FAULT. SUSPECT SLIDE LIGHTS BAD. BOTH SLIDES REPLACED.SDR 2002UALA01201Fan · seizedSMOKE AND FUMES IN THE CABIN. THE EXTRACT FAN FOR THE AVIONICS COOLING SYSTEM WAS FOUND SEIZED AND CAUSE FOR THE BURNING SMELL IN THE CABIN. REPLACED EXTRACT FAN.SDR 2002UALA01134Lavatory · leakingIMMEDIATELY AFTER TAKEOFF CREW NOTICED WATER LEAKING FROM THE AFT LAV. FLIGHT RETURNED TO SFO FOR REPAIR.SDR 2002UALA01102Electrical Sys · malfunctionedRETURNED TO ORD UNDER AMBER ALERT DUE TO ELECTRICAL PROBLEMS.SDR 2002UALA01075Engine · vibrationRETURNED TO ORD UNDER AMBER ALERT DUE TO NR 2 ENGINE VIBRATION.SDR 2002UALA01069Proximity Switch · looseRETURNED TO FIELD DUE TO A DOOR AFT CARGO ECAM WARNING. INSPECTED DOOR SENSOR AND TARGET, CHECKED SYSTEM THROUGH CFDS.CFDS FAULTED PROX SWITCH 32WV. FOUND PROX SWITCH LOOSE. CLEANED THE SWITCH AND SECURED. OPENED AND CLOSED DOOR SEVERAL TIMES, INDICATION SDR 2002UALA00986Valve · defectiveDOOR 2R DOOR ASSIST BOTTLE PRESSURE OVER LIMIT AT 2100 PSI. FOUND SCHRADER SERVICE VALVE BAD. REPLACED VALVE AND SEAL. SERVICED AND CHECKED OK.SDR 2002UALA00768Computer · faultyRETURNED TO FIELD DUE TO AN AVIONICS VENT MESSAGE. *S/D* FAULT WAS ISOLATED TO MALFUNCTIONING AEVC (COMPUTER). REPLACED SAME.SDR 2002UALA00730Latch · out of adjustCREW REPORTS NOISE-VIBRATION-DRONING IN FORWARD CABIN COCKPIT AREA. NOISE REDUCED UPON REACHING CRUISE ALTITUDE. VIBRATION COULD BE FELT IN COCKPIT FLOOR. GROUND ELECTRICAL CONNECTION DOOR VERY LOOSE. ADJUSTED LATCH DOOR.SDR 2002UALA00657Fuse · blownSEATS 12C, 13C, 16C, 17C & 20C ESCAPE PATH LIGHTING INOPERATIVE. REPLACED FUSE ON POWER PACK.SDR 2002UALA00280Warning System · activatedAFT CARGO DOOR ECAM DOOR PAGE INDICATIONS INOPERABLE. ON DEPARTURE ECAM DOORS, AFT CARGO CAME ON.SDR 2002UALA00278Outflow Valve · faultyVENT SKIN VALVE FAULT ON TAKEOFF. AVIONICS SKIN AIR OUTLET VALVE ELECTRONIC CENTRALIZED AIRCRAFT MONITORING POSITION OSCILLATES BETWEEN AMBER AND CLOSED GREEN. REPLACED FAULTING SKIN AIR OUTLET VALVE.SDR 2002UALA00183Slide · defectiveDURING EMERGENCY LIGHT TEST EXTERIOR LOAD AFT L MESSAGE WAS DISPLAYED. THE FAILURE MESSAGES INCLUDED COMM EMERGENCY R, EMERGENCY L, COMM AFT L, EXT LOADS AFT L. MOVED THE 2L SLIDE TO 2R TO ISOLATE THE PROBLEM. THEN REPLACED THE 2R SLIDE TO FIX THE PROBLEM ASDR 2002UALA00121Battery · dischargedEMERGENCY LIGHT TEST FAILED. FAULT CODE 33-51-38 EMERGENCY POWER SUPPLY UNIT BATTERY AFT LEFT. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY.SDR 2002UALA00122Battery Pack · dischargedEMERGENCY LIGHT TEST FAIL. FAULTS EMERGENCY POWER SUPPLY UNIT BATTERY AFT LEFT. REPLACED BATTERY PACK FOR AFT LEFT POWER SUPPLY. EMERGENCY LIGHT BUILT IN TEST EQUIPMENT GOOD.SDR 2001UALA02502Oven · dirtyFIRST CLASS OVEN SMOKING. PULLED CIRCUIT BREAKER, REMOVED TRAYS AND CLEANED OVEN. RESET CIRCUIT BREAKER AND PERFORMED AN OPERATIONAL CHECK. OVEN CHECKS GOOD.SDR 2001UALA02399Outflow Valve · failedCREW RETURNED TO GATE AFTER CABIN PRESSURE 2 FAULT. CENTRALIZED FAULT DISPLAY SYSTEM REPORTED OUTFLOW VALVE MOTOR 2 FAULT. REPLACED VALVE AND CABIN PRESSURE CONTROLLER NR 2 AS PRECAUTION. NO FURTHER FAULTS REPORTED. (NOTE: THIS INCIDENT OCCURRED ON THE GROSDR 2001UALA02400Valve · failedCREW REPORTS AVIONICS SYSTEM FAULT. EXTRACT VALVE SHOWING CLOSED. AIRCRAFT WAS INDICATING FAULTS FOR BOTH THE SKIN AIR INLET AND OUTLET VALVES WITH THE OUTLET VALVE DEFERRED INOPERATIVE. THE SYSTEM WAS REACTIVATED ON THE GROUND AND THE FAULT WAS ISOLATED TOSDR 2001UALA02384Computer · failedAFTER TAKE-OFF, HEARD A THUMP ON THE RIGHT SIDE OF THE AIRCRAFT. ELECTRONIC CENTRALIZED AIRCRAFT MONITORING WARNING - RIGHT WINDSHIELD HEAT & RIGHT WINDOW HEAT. SLIGHT ELECTRICAL ODOR. CIRCUIT BREAKER ANTI-ICE RIGHT WINDSHIELD POPPED. THE WINDOW HEAT COMPSDR 2001UALA02290Selector Valve · faultyLANDED UNDER AMBER ALERT DUE TO A GEAR EXTENSION AND STEERING PROBLEM. AFTER SELECTION OF LANDING GEAR DOWN ON FINAL APPROACH, THE DOORS OPENED YET THE GEAR DID NOT EXTEND. FOLLOWED THE GRAVITY GEAR EXTEND PROCEDURES, AND THE GEAR EXTENDED AND LOCKED WITHOUTSDR 2001UALA02153Computer · faultyELEVATOR AILERON COMPUTER (ELAC) NR 1 FAILURE MESSAGE DISPLAYED ON UPPER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING. RESET OF THE ELAC CAUSED ELECTRICAL ODOR IN FLIGHT DECK. THE ELAC1 WAS REPLACED AND OPERATIONAL CHECK WAS GOOD. SHOP FINDINGS REVEALED INTERNSDR 2001UALA02155Oxygen System · malfunctionedCREW REPORTING OXYGEN LEVEL AT 20 PSI AND CONFIRMED NO OXYGEN AT THE MASK. MAINTENANCE WAS UNABLE TO DUPLICATE THE CAUSE OF LOSS OF OXYGEN PRESSURE. THE O2 BOTTLE WAS REPLACED SINCE IT HAD FALLEN BELOW 100 PSI.
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