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 2004UALA00996Wire Harness · failedSLIDE LIGHTS ARE BLOWN. RESISTANCE TEST DOES NOT PASS. RESERVOIR VALVE ASSEMBLY FRAYED. SUPPLEMENTAL DATA UPDATE SHOP FINDINGS REVEALED THAT ELECTRICAL HARNESS AND LAMPS WERE FOUND DAMAGED HENCE THE TEST OF THE UNIT WHILE INSTALLED ON THE AIRCRAFT FAILED. SDR 2004UALA00834Bleed Air Sys · overheatedRETURN TO FIELD WITH A NR 2 BLEED AIR FAULT. BLEED AIR FAULT GENERATED BY NR 2 BLEED SYSTEM OVERTEMPERATURE. FOUND FAULTY FAV THERMOSTAT,SDR 2004UALA00832Skin · puncturedPUNCTURE IN LOWER SURFACE OF HORIZ STAB SKIN RT. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2004UALA00790Bleed Valve · malfunctionedRETURN TO FIELD DUE TO A DUAL ENGINE BLEED PROBLEM. *S/D* ADJUSTED RT BLEED LEAK DETECTION LOOP IN RT PACK BAY THAT WAS CONTACTING A DUCT CLAMP. THE BLEED LEAK WARNING RESULTED IN AUTOMATIC SHUTDOWN OF THE ASSOCIATED BLEED SYSTEM. CONCURRENTLY THE AIRCRAFTSDR 2004UALA00772Blade · failedABORTED TAKEOFF DUE TO NR 1 ENGINE COMPRESSOR STALL. FIRST STAGE COMPRESSOR BLADE (R3 BLADE) FAILURE. REPLACED ENGINE.SDR 2004UALA00748Light · inoperativeEMERGENCY SEAT TRACK LIGHTING INOPERATIVE AT ROWS 15, 16, 19, 20, 23 AND 24. WIRE HARNESS WAS INOPERABLE. REPAIRED WIRE HARNESS 350WL10 FOUND UNDER SEATS 23AND 24 ABC.SDR 2004UALA00707Hydraulic System · lowRETURN TO FIELD WITH YELLOW HYDRAULIC SYSTEM LEVEL LOW. FOUND GREEN SYSTEM CHECK VALVE AT MANIFOLD LEAKING, REPLACED O-RING. OPERATIONS CHECK NORMAL.SDR 2004UALA00689Indicator · inoperativeDIVERTED DUE TO LOSS OF NAVIGATIONAL INSTRUMENTS & IFR CONDITIONS AT PLANNED DESTINATION. NAV ACCURACY LOW AND MCDU RAD/NAV PAGE UNAVAILABLE. IRU'S REALIGNED AND NAV SWITCHES ON RADIO MANAGEMENT PANEL CYCLED. INDICATIONS RETURNED TO NORMAL. FMGC BITE READOUT ASDR 2004UALA00633Windshield · failedF/O'S WINDSHIELD SHATTERED FL370. FLIGHT DIVERTED. MOISTURE INGRESS IN THE BUSBAR AND SENSOR AREA CAUSED THE ARCING, WHICH CAUSED THE WINDOW TO SHATTER. WINDSHIELD WAS REPLACED.SDR 2004UALA00634Warning Light · illuminatedFLIGHT DIVERTED DUE TO FWD CARGO DOOR UPPER ECAM WARNING. CARGO DOOR PROXIMITY SWITCH FAILED. REPLACED CARGO DOOR PROXIMITY SWITCH . OPERATIONS CHECK NORMAL.SDR 2004UALA00615Warning Light · illuminatedFLIGHT DIVERTED DUE TO NR 2 EGT OVERTEMP MESSAGE. BLEED VALVE CHECK FOUND 4 LOOSE SCREWS AT BASE OF 10TH STG BLEED VALVE SOLENOID . INTERMITTENT BLEED VALVE OPEN WOULD GIVE OVERTEMP INDICATION. TIGHTENED SCREWS. OPERATIONS CHECK NORMAL.SDR 2004UALA00576Switch · failedFLIGHT DIVERTED DUE TO GREEN HYDRAULIC RESERVOIR LOW LEVEL WARNING ON ECAM. *S/D* GREEN HYDRAULIC PUMP SWITCH FAILED. REPLACED SWITCH, OPERATIONS CHECK NORMAL.SDR 2004UALA00557Oxygen System · dischargedFLIGHT CREW OXYGEN SYSTEM REPORTED AT 50 PSI. FLIGHT DIVERTED. CREW O2 MASK SET TO 100% AND IMPROPERLY STOWED. SERVICED TO FULL. OPERATIONS CHECK NORMAL.SDR 2004UALA00563Pump · failedYELLOW HYDRAULIC SYSTEM FAILED. NR 2 ENGINE DRIVEN PUMP FOUND LEAKING. REPLACED ENGINE DRIVEN PUMP. OPERATIONS CHECK NORMAL.SDR 2004UALA00549Light · will not testEMERGENCY LIGHT TEST FAILED AFTER SLIDE REPLACEMENT AT DOOR 2L. THE SLIDE SHOP TESTED THE SLIDE ASSEMBLY UPON RECEIPT AND THE SHOP VERIFIED THE UNIT TO HAVE FAILED THE LIGHT TEST. THE COMPLETE LAMP HARNESS WAS REPLACED AND THE 22 BLOWN LIGHTS WERE REPLACEDSDR 2004UALA00498Warning Light · illuminatedCREW ADVISED MOMENTARY LOSS OF BLUE & YELLOW HYDRAULICS WHILE EN ROUTE. REGAINED YELLOW. AMBER ALERT DECLARED. UNABLE TO DUPLICATE DISCREPANCY. NO PARTS REPLACED. OPERATIONS CHECK NORMAL.SDR 2004UALA00486Servo · failedLANDED UNDER AMBER ALERT DUE TO A NOSE WHEEL STEERING FAULT PROBLEM. NOSE STEERING SERVO UNIT FAILED. REPLACED NOSE STEERING SERVO UNIT. OPERATIONS CHECK NORMAL WITH NO MESSAGES OR LEAKS.SDR 2004UALA00470Sensor · inoperativeCABIN EMERGENCY LIGHTS FAILED TO TEST. RESET CIDS SYSTEM AND NO SMOKING LIGHTS. ACCOMPLISHED OPERATIONAL TEST OF EMERGENCY LIGHTS PER MM 33-51-00-710-001, SYSTEM GROUND TESTED OK, NO FAULTS NOTED ON PTP.SDR 2004UALA00391Light · failedEMERGENCY LIGHTS FAIL 3SVC TEST. REPLACED EPSU RT & AFT UNITS AND AFT BATTERY. OPS CK GOOD.SDR 2004UALA00726O-Ring · leakingLOW BOTTLE PRESSURE. SLOW LEAK DETECTED IN VALVE SHAFT THROUGH THE PLATE AND COVER HOUSING. VALVE WAS OVERHAULED AND NEW O-RINGS AND BACKUP RINGS REPLACED.SDR 2004UALA00378Light · malfunctionedEMERGENCY EXIT LIGHTS ARE FLASHING IN ARMED POSITION.SDR 2004UALA00358Nose Cowl · damagedRETURN TO FIELD DUE TO A BIRD STRIKE TO THE NR 2 ENGINE. A BIRD STRIKE CAUSED ENGINE VIBRATION AND REDUCED POWER. REPLACED NR 2 ENGINE AND NOSE COWL.SDR 2004UALA00359Frame · dentedDENT FOUND BETWEEN FR1 & FR2 JUST FWD OF FWD E&E DOOR. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER REPAIR.SDR 2004UALA00328Odor · detectedVERY STRONG ELECTRIC BURNING ODOR IN COCKPIT AND AFT CABIN AREA AT CRUISE ALTITUDE. NO CAUSE IDENTIFIED. CHECKED CABIN AND LAV LIGHTING AND TRASH AREAS, NO DEFECTS. OPERATED BOTH PACKS USING APU AND ENGINES, RAN TRIM VALVES FULL HOT & COLD. OPERATED ENGINES ATSDR 2004UALA00305Stringer · dentedSTRINGER 7L WAS DENTED JUST FORWARD OF FRAME 7. MAJOR REPAIRED ACCOMPLISHED. REPLACED STRINGER.SDR 2004UALA00276Selector · leakingAIRCRAFT LOST YELLOW SYSTEM HYDRAULIC SYSTEM. RETURN TO FIELD. FOUND HYD FLUID (AFT RT WHEEL WELL) LEAKING FROM AUTOMATIC SELECTOR BRAKE VALVE. REMOVED VALVE FOUND O RING DAMAGED. REPLACED AUTOMATIC SELECTOR BRAKE VALVE.SDR 2004UALA00256Light · inoperativeFOUND WHITE EEL LIGHT IS INOP AT ROW 21 ABC. REPLACED EEL LIGHT. OPS CHECKED NORMAL.SDR 2004UALA00244Generator · failedFLIGHT DIVERTED DUE TO A LOST GENERATOR. NR 2 GENERATOR BUSS LOSS. NUMBER 2 GENERATOR FAULT LIGHT ILLUMINATED SUPPLEMENTAL DATA UPDATE PIN AND SOCKET ON PYLON FIREWALL CONNECTOR 400VC CORRODED AND BURNED. REPLACED HARNESS ASSEMBLIES.SDR 2004UALA00202Shock Absorber · failedRETURN TO FIELD DUE TO FAILURE OF LANDING GEAR TO RETRACT. LANDING GEAR SHOCK ABSORBER FAULT. LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) FAILED. THE LGCIU COMPONENT EXPERIENCED A HARD FAILURE DURING OUTPUT TESTS. REPLACED LGCIU. OPERATIONS CHECK NORMAL.SDR 2004UALA00163Sensor · failedFLIGHT DIVERTED DUE TO FWD CARGO DOOR OPEN ECAM MESSAGE. FORWARD CARGO DOOR PROXIMITY SENSOR WAS REPLACED 28WV. THE FORWARD CARGO DOOR PROXIMITY TARGET WAS ALSO ADJUSTED.SDR 2004UALA00157Transmitter · malfunctionedFLIGHT DIVERTED DUE TO LOW NR 2 ENGINE OIL INDICATION. REPLACED OIL QUANTITY TRANSMITTER.SDR 2004UALA00100Odor · detectedRETURN TO FIELD DUE TO AN ELECTICAL ODOR IN THE CABIN. AVIONICS COOLING BLOWER FAN BEARINGS FAILED. REPLACED UNIT WITH NO FURTHER PROBLEMS REPORTED.SDR 2004UALA00086Warning Light · illuminatedRETURN TO FIELD DUE TO ECAM NR 2 FUEL CONTROL FAULT. DEBRIS FLOWING THROUGH FMU CAUSED TORQUEMOTOR FAULT. THE DEBRIS WAS SUBSEQUENTLY FLUSHED OUT. THIS IS AN ISOLATED INCIDENT AND ENGINEEING WILL CONTINUE TO MONITOR THE FMU.SDR 2004UALA00030Frame · damagedFRAME 23 AT STR 36L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME 23 LWR SECTION PER EVA -MOC 8468A.SDR 2004UALA00022Frame · bentFRAME 24 BENT BTWEEN STR 36L AND 37L. MAJOR REPAIR ACCOMPLISHED. REPAIR OF FRAME 24 WAS ACP'D PER EVA MOC1-8467C.SDR 2004UALA00005Skin · scratchedAPPROX 2 FT LONG SCRAP ALONG FUSELAGE BELLY AT FWD CARGO DOOR LEADING TO LOWER TCAS ANTENNA. MAJOR REPAIR. DOUBLER TRIPLER REPAIR TO SKIN AT STRINGER 42R AND FRAME 27.SDR 2003UALA00986Lens · missingFIRST CLASS CLOSET EEL LIGHT IS MISSING LENS ASSY. REPLACED LIGHT ASSY.SDR 2003UALA00976Seat Track · corrodedCABIN SEAT TRACK OB FR 62 FWD, SEVERAL LUGS WITH LIGHT CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED DAMAGED SECTION IAW SRM 53-00-15.SDR 2003UALA00932Skin · dentedLARGE DENT APPROX 1 FT BY 1 FT UNDER LT STATIC PORT. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER SRM 53-00-11 & SRM 51-47-00.SDR 2003UALA00911Oil Cooler · failedFLIGHT DIVERTED DUE TO LOSS OF OIL IN NUMBER 1 ENGINE. FUEL COOLED OIL COOLER FAILED AND ALLOWED THE OIL TO ESCAPE INTO THE FUEL SIDE OF THE COOLER. REPLACED FCOC PER AMM 79-21-43.SDR 2003UALA00903Warning Light · illuminatedEMERGENCY LIGHTS SYSTEM TEST FAILS WITH MESSAGE EPSU INT LOAD EMERGENCY L DISPLAYED. RESET SYSTEM C-B'S AND EMERGENCY LIGHTS PER MM 33-51-00. TESTS NORMAL.SDR 2003UALA00870Odor · detectedFLIGHT DIVERTED DUE TO ELECTRICAL ODOR IN CABIN BETWEEN ROWS 3 AND 6. VENT BLOWER AND EXTRACT FANS RUNNING NORMAL, CHECKED RECIRCULATION FANS, BOTH PACKS OPERATING NORMAL. CHECKED CABIN LIGHTING AND PASSENGER ENTERTAINMENT SYSTEM, NO DEFECTS FOUND.SDR 2003UALA00861Compressor · damagedNUMBER 2 ENGINE COMPRESSOR STALLS WHEN OPERATED ABOVE IDLE. UPON ENGINE TEARDOWN SIGNIFICANT DAMAGE WAS FOUND TO THE FRONT OF THE HIGH PRESSURE COMPRESSOR, WHICH CAUSED THE ENGINE TO EXPERIENCE A COMPRESSOR STALL WHEN ADVANCED ABOVE IDLE POWER. SIGNIFICANSDR 2003UALA00849Blade · failedCREW REPORTED LOUD BANG ON T/O ROLL AT APPROXIMATELY 40 KNOTS. TAKEOFF ABORTED. ENGINE WAS REMOVED FOR TEARDOWN AND INVESTIGATION, WHICH REVEALED A HIGH COMPRESSOR BLADE FRACTURE WITH SIGNS OF FOREIGN OBJECT DAMAGE (FOD) AT FRACTURE INITIATION SITE. THIS FSDR 2004UALA00725O-Ring · leakingLOW BOTTLE PRESSURE. BOTTLE TO VALVE O-RING DETERIORATED. REPLACED CYLINDER ASSY.SDR 2003UALA00768Controller · failedRETURN TO FIELD DUE TO A PRESSURIZATION PROBLEM. CFDS REPORTED NO FAULTY SYSTEMS OR COMPONENTS. GROUND TESTING OF CABIN PRESSURE CONTROL, FMGC, AND ADIRS SYSTEMS REVEALED NO SYSTEM FAULTS. REPLACED CPC 2 AS PRECAUTIONARY MEASURE AS THIS WAS CPC IN CONTROL ASDR 2003UALA00769Valve · malfunctionedFLIGHT DIVERTED DUE TO A PRESSURIZATION PROBLEM. FLIGHT CREW NOTED CABIN PRESSURE ALTITUDE INCREASING DURING CRUISE, F/A'S NOTED RUMBLING IN AFT GALLEY AREA. REPLACED BOTH SAFETY VALVES.SDR 2003UALA00770Connector · looseRETURN TO FIELD DUE TO A FWD CARGO DOOR ECAM MESSAGE. LOOSE CONNECTOR ON SENSOR 28WV AIRFRAME SIDE, SECURED THE CONNECTOR TO THE CARGO DOOR PROXIMITY SENSOR 28WV.SDR 2003UALA00710Windshield · crackedCAPTAIN'S WINDSHIELD IS CRACKED. WATER INGRESSION AND HEAT SENSOR ARCING DUE TO HUMP SEAL FAILURE. WINDSHIELD REPLACED.SDR 2003UALA00689Fan · seizedFLIGHT DIVERTED DUE TO SMOKE IN COCKPIT. AVIONICS EXTRACT FAN (18HQ) FOUND SEIZED. REPLACED FAN.
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