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 UALA2010062802277Valve · failedACFT EXPERIENCED A PRESSURE DROP ON DESCENT. PFR SHOWS ECAM MSG 'CAB PR LO DIFF PR' AND 'CAB PR SAFETY VALVE OPEN'. PER TROUBLESHOOTING FOUND BOTH SAFETY VALVES AT FAULT. REPLACED BOTH SAFETY VALVES 6HL AND 7HL. OPS NORMAL.Jun 26, 2010 · N822UA · Airbus A319131 · Pressure Regulator/Outflow ValveSDR UALA2010062802273Girt Bar · out of toleranceDOOR 1RT GIRT BAR MISSING ARMING INDICATOR SUPPORT AND INDICATOR. REPLACED GIRT BAR. DOOR ARMING CHECKED NORMAL. ACP INSP OF INSTALLATION.Jun 25, 2010 · N802UA · Airbus A319131 · Emergency EquipmentSDR UALA2010062302232Aspirator · failedDOOR SLIDE AT 2R HAS BAD ASPIRATOR WILL NOT STAY CLOSED. REPLACED DOOR 2R SLIDE ASSY.Jun 23, 2010 · N803UA · Airbus A319131 · Escape SlideSDR UALA2010062302235Socket · unsecureLT OVERWING SLIDE INDICATION INOP. RESEATED SOCKET AT 2WNVC1 SLIDE ARMED IND LITE AT EMER EXIT DOOR. LT OVERWING DOOR. PINNED BOTH RT AND LT OVERWING ESCAPE SLIDE BOTTLES AND INOPED BOTH OVERWING DOORS FOR T/S. SECURED BOTH OVERWING ESCAPE SLIDE BOTTLES AND DJun 23, 2010 · N829UA · Airbus A319131 · Escape SlideSDR UALA2010062302230Power Supply · failedCABIN EMERGENCY LIGHT TEST FAILED. POWER SUPPLY IN INOPERATIVE. REPLACED EPSU POSITION 12WL, TESTS OKAY.Jun 23, 2010 · N822UA · Airbus A319131 · Emergency LightingSDR UALA2010062402236Bearing · corrodedNR 1 PYLON SPIGOT BEARING CORRODED. INSTALLED NEW NR1 PYLON SPIGOT BEARING.Jun 23, 2010 · N818UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR UALA2010062402237Sleeve · crackedNR1 PYLON FWD ATTACHMENT INBD UPR SLEEVE CRACKED. INSTALLED NEW NR1 PYLON FWD INBD UPR SLEEVE.Jun 23, 2010 · N818UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR UALA2010062302214Unknown · odorCREW REPORTS BURNED FOOD SMELL IN AFT GALLEY, OVENS WERE NOT ON. CHILLER, COFFEEMAKERS AND HOT PLATES IN USE. SWITCHED ABOVE UNITS OFF AND SMELL WENT AWAY. MX OPERATED GALLEY EQUIPT AND CONFIRMED NORMAL OPS WITH NO ODORS. INVESTIGATED AREA TO DETERMINE SOURCJun 22, 2010 · N808UA · Airbus A319131 · Air Distribution SystemSDR UALA2010062302215Sleeve · crackedNR 2 PYLON FWD MOUNT UPPER INBD SHACKLE SLEEVE HAS A CRACK AROUND THE SHANK HEAD AREA. INSTALLED NEW SHACKLE SLEEVE.Jun 22, 2010 · N818UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR UALA2010062302217Sleeve · crackedNR 2 PYLON FWD MOUNT LWR INBD SHACKLE SLEEVE HAS A CRACK AROUND SHANK HEAD AREA. INSTALLED NEW FWD LWR INBD SLEEVE.Jun 22, 2010 · N818UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR UALA2010062302219Sleeve · crackedNR 1 PYLON AFT ATTACHMENT OTBD FITTING SLEEVE CRACKED. REMOVED CRACKED SLEEVE. INSTALLED NEW NR 1 ENG PYLON AFT SHACKLE OTBD PIN ASSY.Jun 22, 2010 · N818UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR UALA2010062302220Sleeve · crackedNR 1 PYLON AFT ATTACHMENT INBD FITTING SLEEVE CRACKED. REMOVED CRACKED SLEEVE. INSTALLED NEW NR 1 ENG PYLON AFT SHACKLE INBD PIN ASSY.Jun 22, 2010 · N818UA · Airbus A319131 · Nacelle/Pylon, Attach FittingsSDR UALA2010062302221Sleeve · crackedNR 2 ENG PYLON AFT MOUNT LWR INBD SLEEVE CRACKED. REMOVED CRACKED SLEEVE PIN. INSTALLED NEW NR 2 PYLON AFT SHACKLE LWR INBD SLEEVE PIN.Jun 22, 2010 · N818UA · Airbus A319131 · Nacelle/Pylon, Attach FittingsSDR UALA2010062302222Bearing · corrodedNR2 PYLON SPIGOT BALL JOINT SPHERICAL BEARING HAS PITTING CORROSION. INSTALLED NEW NR 2 PYLON SPIGOT BALL JOINT BEARING.Jun 22, 2010 · N818UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR UALA2010062302223Sleeve · crackedRIGHT PYLON OUTBOARD UPPER SLEEVE CRACKED. REMOVED CRACK SLEEVE. INSTALLED NEW NR 2 PYLON FWD OUTBOARD UPPER SLEEVE.Jun 22, 2010 · N818UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR UALA2010062202199Servo · faultyACFT VIBRATION 310 KIAS. RT TURN AND WINGS LEVEL FL180-220. SMOOTH AIR.CG31.6.GW131.3. EPR1.34. CHECKED RUDDER FREEPLAY FOUND UPPER (BLUE SYSTEM) SERVO BYPASSING AND VERY HOT. REMOVED UPPER RUDDER SERVO. REPLACED RUDDER BLUE SERVO. OPS GOOD.Jun 22, 2010 · N811UA · Airbus A319131 · Rudder Control SystemSDR UALA2010062302218Sleeve · crackedNUMBER 1 PYLON AFT ATTACHMENT CENTER FITTING HAS CRACKED SLEEVE. RMV'D CRACK SLEEVE. INSTALLED NEW NR 1 ENG PYLON AFT SHACKLE CENTER PIN ASSY.Jun 22, 2010 · N818UA · Airbus A319131 · Nacelle/Pylon, Attach FittingsSDR UALA2010062202193Computer · malfunctionedVIB WAS NOTED FROM TAKEOFF THRU APPROX FL 280 AND DISSIPATED. APPEARS WORSE IN BACK. ARTIFICIAL VIBRATION FELT WITH ELACS ON. REPLACED BOTH ELACS ARTIFICIAL VIBRATION DISAPPEARED, REPLACED IAW MM.Jun 21, 2010 · N809UA · Airbus A319131 · Flight Control SystemSDR UALA2010062102165Slide · unserviceableRT OFFWING SLIDE IS UNSERVICEABLE. REPLACED RT OFFWING SLIDE.Jun 20, 2010 · N843UA · Airbus A319131 · Escape SlideSDR UALA2010062102168Slide · debondedLT OVERWING SLIDE PANEL 194AT AFT EDGE HAS AN AREA 11 INCHES BY 1 INCH DISBONDING. REPLACED LT OFFWING SLIDE.Jun 20, 2010 · N843UA · Airbus A319131 · Escape SlideSDR UALA2010061602128Pump · unreliableGREEN HYD RESERVOIR LOW LEVEL MESSAGE, RTFL. ECAM PAGE CONFIRMS FLUID LOSS. SERVICED ALL HYD RSVR TO FULL. REPLACED NR 1 ENG GREEN EDP AND CASE DRAIN FILTER. THERE WAS NO METAL OR ANY EVIDENCE OF FAILURE. NO LEAKS PRESS 3000 PSI. MX FOUND A BLOWN STEEL BRAIDEJun 16, 2010 · N822UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), MainSDR UALA2010061502108Circuit Card · failedREPORT OF ACFT GO AROUND DUE TO UNSAFE GEAR INDICATION. SUBSEQUENT LANDING GOOD WITH ALL INDICATIONS GOOD. NO NOSE OR LT GEAR DOWN INDICATIONS, SECOND ATTEMPT AFTER GO AROUND LT AND RT DOWN INDICATIONS OK BUT NOSE UNLOCKED LIGHT NEVER ILLUMINATED. MCDU FUNCJun 15, 2010 · N809UA · Airbus A319131 · Landing Gear Position and WarningSDR UALA2010061502117Oxygen Mask · leakingF/O O2 MASK IS LEAKING. SWAP WITH 2ND OBSERVERS MASK AND APPLY DF STICKER AND PLACARD TO SEAT (THE ONE BEHIND CAPTAIN). MX COMPLIED WITH MEL PLACARD 2511 R. REPLACED AND TESTED REF MM.Jun 14, 2010 · N833UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2010061402092Strainer · cloggedBURNING SMELL IN AFT GALLEY. FOUND GALLEY DRAIN STRAINER CLOGGED. REPLACED STRAINER, CLEANED AIR FILTER AND OVENS. OPS CK OK, NO SMELL ON GROUND.Jun 13, 2010 · N825UA · Airbus A319131 · Buffet/GalleysSDR UALA2010061402061Control Panel · no testBOTH O2 SPEAKER MASKS ON CAPT SIDE WILL NOT TEST. REPLACED AUDIO CONTROL PANEL. CAPTS ACP PERFORMED SYS TEST. OPS ARE GOOD.Jun 12, 2010 · N840UA · Airbus A319131 · Audio Integrating SystemSDR UALA2010061402065Extinguisher · reads lowF/A REPORTS FRONT LAV FIRE EXTINGUISHER GAUGE. NO PARTS SFO. LAV SMOKE DETECTION WORKS NORMAL.Jun 12, 2010 · N830UA · Airbus A319131 · Fire Bottle, PortableSDR UALA2010061402095Oxygen Mask · faulty2ND OB'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). SEAT PLACARDED UNSERVICEABLE AND STICKER APPLIED. REPLACED SECOND OBSERVERS O2 MASK. OPS NORMAL.Jun 11, 2010 · N845UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2010061002025Floorbeam · crackedFLOORBEAM Y254 IS CRACKED ABOUT 2" NEAR CROSSBEAM 35. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED FLOORBEAM SECTION. FABBED NEW SPLICE PLATES AND DRILLED NEW FLOORBEAM. INSTALLED REPAIR PARTS.Jun 9, 2010 · N817UA · Airbus A319131 · Fuselage Main, Floor BeamSDR UALA2010060801997Compressor · stalledCREW REPORTED ENG 1 AUDIBLE COMPRESSOR STALL (5X) WHEN POWER REDUCED TO IDLE FOR LANDING FLARE. ACP TROUBLESHOOTING IAW TSM. NO VISUAL DEFECTS OR FADEC REPORTS FOUND. ACCOMPLISHED SUCCESSFUL POWER ASSURANCE TEST ON BOTH ENGINES.Jun 7, 2010 · N812UA · Airbus A319131 · Turbine Engine Compressor SectionSDR UALA2010060301937Actuator · leakingCREW REPORTS: EVIDENCE OF OIL LEAK FROM NR 1 ENGINE. FOR ENGINE DRAINS LEAK RATE LIMITS REPORT FINDINGS TO SAMC, OPBLM EMC ARSHAD. ENG1 I-B REVERSER HALF UPPER NON LOCKING ACT. LEAKS AT TRIANGULAR FTG. FOR FLEX SHAFT TUBE BEYOND LIMITS OF MM. REPLACE UPPERJun 3, 2010 · N821UA · Airbus A319131 · Engine Thrust ReverserSDR UALA2010060301917Unknown · smokeSMOKE IN CABINS, RTFL. NO VISIBLE SMOKE ONLY PLASTIC BURNING SMELL. NO SMELL IN FIRST CLASS. NO FIRE NOTED AND SMELL WAS COMPLETELY GONE AFTER LANDING. RAN BOTH ENGINES WITH PACKS ON HOT AND COLD. RAN OVEN'S, COFFEEMAKERS, HOT PLATES AND CHILLERS. CKD CABIN Jun 2, 2010 · N828UA · Airbus A319131 · Air Distribution SystemSDR UALA2010060301924Oxygen Mask · frayedHOSE ON CAP O2 MASK IS FRAYED WHERE HOSE CONNECTS. REPLACED CAPTAIN'S O2 MASK.Jun 1, 2010 · N823UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2010060101899Target · bentNO SLIDE ARMED INDICATION WHEN ACCESS PANEL IS REMOVED AT LT OVER WING EXIT. NO LT SLIDE WORD ON LOWER ECAM WHEN ACCESS PANEL IS INSTALLED OR REMOVED. FOUND COVER FLAP FOR THE HATCH PROX TARGET TO BE BENT OUT OF POSITION. REPOSITION TARGET. EMERGENCY EXIT ECAMJun 1, 2010 · N829UA · Airbus A319131 · Door Warning SystemSDR UALA2010060101895Oxygen Mask · noneCAPTAIN'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). CAPT'S O2 MASK DOES NOT TEST PROPERLY. SWAPPED HARNESS AND BOX WITH 2ND OBSERVERS - 2ND OBSERVERS SEAT AND EQUIPMENT INOP. REPLACED MASK. MASK WORKS PROPERLY. BOX DOES NOT TEST AT ALL. REPLACED MASK, May 31, 2010 · N846UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2010060101898Engine · smokeNR 2 ENG EXCESSIVE SMOKE WHEN ENGINE TURNED OFF. ACCOMPLISHED MT79-004. NO SIGNS OF OIL AT TAILPIPE AFTER SHUTDOWN, NO SMOKE. ENGINE DEEMED OK FOR SERVICE. NO FURTHER ISSUES REPORTED AS OF 07/16/10.May 31, 2010 · N823UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR UALA2010052801841Terminal · burnedBURNING ELECTRICAL ODOR COMING FROM AFT GALLEY OVERHEAD. ODOR WENT AWAY AFTER TURNING COFFEEMAKERS & AFT CHILLERS OFF. REMOVED & INSPECTED COFFEEMAKERS. FOUND BURNED WIRE TERMINAL AT BOTTOM OF HOT PLATE ON C-M M42. NO DEFECTS WITH BENCH PLUGS OR REMAINING COFMay 28, 2010 · N851UA · Airbus A319131 · Equipment/Furnishings WiringSDR UALA2010060101888Unknown · odorODOR IN AFT CABIN BURNING PLASTIC SMELL. INSPECTED AFT GALLEY AREA NO SMOKE NOTED. SUSPECT APU EXHAUST SMELLED DUE TO TAIL WIND AT GATE. OK FOR SERVICE AT THIS TIME.May 28, 2010 · N841UA · Airbus A319131 · Air Distribution SystemSDR UALA2010052701832Line · leakingGREEN HYD LOW PRESS: FOUND LT MLG NORMAL BRAKE SUPPLY FLEX LINE LEAKING. FOUND HYD LINE TO BRAKE LEAKING LT GEAR. REPLACED 2 LINES, LEAK CKS OK, BLED BRAKES.May 27, 2010 · N815UA · Airbus A319131 · Hydraulic System, MainSDR UALA2010052801840Computer · malfunctionedON FLT CONTROL CHECK L-R AILERON HAVE HYD NOISE-VIBRATION HEARD AND FELT IN COCKPIT. ISOLATED RT AILERON HYD SYSTEMS, RT AILERON FLUTTERS WITH ONLY GREEN HYD SYSTEM ON. ATTEMPTED ELAC 1 AND 2 RESET, NO HELP. SUSPECT RT GREEN AILERON SERVO ISSUE. THERE WERE May 27, 2010 · N816UA · Airbus A319131 · Hydraulic System, MainSDR UALA2010052601806Unknown · odorF/A REPORT ELECT BURNING SMELL IN AFT GALLEY. STOPPED W- GAL PWR OFF. NEED TO CHECK OVEN INTERIOR FOR CHARRING IN FAN. WITH ACFT DE-ENERGIZED, OPEN TRIANGLE PANEL WHERE GALLEY POWER SWITCHES ARE LOCATED, INSPECT FOR CHARRING. INSPECTED AFT GALLEY ELECTRICAL CMay 25, 2010 · N851UA · Airbus A319131 · Air Distribution SystemSDR UALA2010052601802Unknown · odorCABIN CREW REPORTS STRONG CHEMICAL SMELL IN LAST FEW ROWS OF COACH AND GALLEY. CHECKED GALLEYS, COFFEEMAKERS AND CHILLERS, OVENS, CHECKED UNDER SEATS, CHECKED LAVS AND CGO PITS, OPERATED PACKS WITH APU BLD, CHECKED LIGHTS, NO UNUSUAL SMELL OR ODOR NOTED. ALL CMay 25, 2010 · N852UA · Airbus A319131 · Air Distribution SystemSDR UALA2010052401779Filter · dirtyOILY SMELL COMING FROM AIR CONDITIONING. APU INOPERATIVE DUE TO HISTORY OF OIL SMELL. ACCMP'D PACK BURNOUT AND REPLACED RECIRCULATION FILTERS. APU WAS A FULL RIP LSV AND JUST INSTALLED. CHECK FOR OIL IN BLEED DUCT. CHECK OIL LINE FROM OIL COOLER, LOP SWITCH, EMay 23, 2010 · N803UA · Airbus A319131 · Air Distribution SystemSDR UALA2010051901685Battery Pack · inoperativeEMERGENCY LIGHT SYS TEST FAILED ON 3SV RT EMERGENCY BATTERY INDICATED. REPLACE BATTERY PACK.May 19, 2010 · N805UA · Airbus A319131 · Emergency LightingSDR UALA2010051901687Slide · no testEMERGENCY LIGHT SYS TEST FAILED ON 3SV. EXTERNAL LOADS FWD L INDICATED. SLIDE WAS TESTED AND DOOR 1L SLIDE IS BAD. SLIDE IS A MR25822, 649-9130. ACFT RESTRICTED TO DAYLIGHT OPS ONLY. REPLACED DOOR 1L SLIDE. PASSED EMERGENCY LIGHT TEST.May 19, 2010 · N805UA · Airbus A319131 · Escape SlideSDR UALA2010051901679Shaft · leakingAFTER 5 MIN RUN ENG 1 ANGLE GEARBOX LEAKS FROM TOWER SHAFT SPLINE AREA AT RATE OF 6 DPM. REMOVED ENG V11294 AND INSTALLED ENG V10163.May 18, 2010 · N841UA · Airbus A319131 · Turbine Engine Reduction GearSDR UALA2010051701667Skin · gougedEXTERNAL FUSELAGE IS GOUGED AT FRAME 34 AT STR 43R DUE TO LONG FUSE FILLET FAIRING ATTACH SCREW. MAJOR REPAIR ACCOMPLISHED: DAMAGE REPAIRED IAW SRM, FIG 224. AREA HFEC INSPECTED, NO CRACKS NOTED. DOUBLER INSTALLED IAW SRM. REPAIR REQUIRES INSPECTION AT DEFIMay 17, 2010 · N837UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2010051701655Oxygen Mask · weakF/O O2 MASK VERY WEAK OXYGEN FLOW. REPLACED F/O O2 MASK. OXYGEN BOX CHECKS OK.May 15, 2010 · N818UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2010051301627Warning Light · illuminatedIDG 1 OIL LO PR DISPLAYED ON UPPER ECAM SCREEN. - ELEC REMOVED WIRE HARNESS FROM IDG AND MEGGERED TO FIREWALL CONNECTOR NO FAULTS. RANG WIRING FROM EGIU PIN AA-5B TO GCU PIN AA-15D ALL NORMAL, NO FAULTS FOUND. REPLACED EGIU 22XU1 PER AMM. RAN ENGINE IAW JRH AMay 13, 2010 · N801UA · Airbus A319131 · AC Generator-AlternatorSDR UALA2010051201610Mount Bracket · brokenMOUNT BRACKET FOR LT RUNWAY TURN OFF LIGHT & N-W STEERING CONTROL SERVO IS BROKEN. REPLACED AFT NOSE GEAR SUPPORT ASSEMBLY FITTING.May 12, 2010 · N842UA · Airbus A319131 · Landing Gear Steering SystemSDR UALA2010051201621Access Panel · leakingFUEL SEEPING FROM RIGHT WING SHORING POINT 21. FUEL TANK ENTRY FOUND LEAK AT AFT SIDE OF MAIN GEAR FISH POLE ATTACH POINT JUST AFT OF DOME NUT. CLEANED AFFECTED AREA AND APPLIED FIRST COAT WITH A1-2. WILL REQUIRE SECOND COAT OF SEALANT AND CLOSE UP TANK PANMay 12, 2010 · N850UA · Airbus A319131 · Wing, Plate/Skin
Back to IAE V2522-A5