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 UALA2012081404512Sliding Window · damagedCAPTAIN'S SLIDING WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS, NEED TO EVALUATE CONDITION. DELAMINATION ALSO AT RT SIDE AND BOTTOM. VISIBILITY NOT AFFECTED. CHECKED DIMENSIONS OF DELAMINATED AND FOUND MAX AREA B DIMENSION TO BE JUST UNDER 3.0 INCHES WHICH ISAug 12, 2012 · N817UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2012081404507Unknown · faultyRIGHT WINDOW DISPLAYED ON UPPER ECAM SCREEN. REPLACED RIGHT SLIDING WINDOW PANEL PER MM. RIGHT WINDOW MESSAGE ON UPPER ECAM STILL PRESENT.Aug 11, 2012 · N837UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2012081004358Battery · faultyFWD LEFT EPSU BATTERY FAULT. REPLACED EPSU BATTERY FORWARD LEFT PER AMM.Aug 10, 2012 · N834UA · Airbus A319131 · Emergency LightingSDR UALA2012080904335Stowage Box · malfunctionedCAP O2 MASK NOT OPERATING PROPERLY. REMOVED AND REPLACED CAPTAIN'S O2 MASK STOWAGE BOX, OPS OK.Aug 8, 2012 · N854UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2012080904336Bottle · low pressureCOCKPIT FIRE EXTINGUISHER NOT IN THE GREEN. REPLACED BOTTLE.Aug 8, 2012 · N802UA · Airbus A319131 · Fire Bottle, PortableSDR UALA2012080804284Feeder Cable · inoperativeEMERGENCY PATH LIGHT ON SEAT 11C INOP. REPLACED SEAT CABLE AND SEAT AISLE EMERGENCY LIGHT ASSY, OPS CHECKED OK.Aug 7, 2012 · N815UA · Airbus A319131 · Light System WiringSDR UALA2012080704261Wire Harness · damagedWIRE HARNESS DAMAGED IAW WDM 71-51-03. REPLACED HARNESS, OPS CHECKED GOOD.Aug 7, 2012 · N841UA · Airbus A319131 · Electrical Power System WiringSDR UALA2012080704260Tire · out of roundNOSE LANDING GEAR VIBRATION DURING TAKEOFF ROLL. REPLACED ALL MAIN TIRE-WHEELS ASSEMBLY TS MM.Aug 6, 2012 · N806UA · Airbus A319131 · TireSDR UALA2012080704262Plug · damagedRT INBOARD INNER MOST FLAP HOIST POINT NYLON PLUG DAMAGED. INSTALLED NEW PLUG.Aug 6, 2012 · N843UA · Airbus A319131 · Leading Edge DevicesSDR UALA2012080604191Apu · odorSMOKE ODOR IN COCKPIT, RETURNED TO FIELD. FLIGHT ATTENDANT REPORTED BOTH AFT LAV DETECTORS ALARMED. ODOR DISSIPATED AFTER LEVEL OFF AND THROTTLES RETARDED TO IDLE. LAV SMOKE DETECTORS STOPPED ALARMING AT THAT TIME. ODOR APPEARS TO BE COMING FROM VENTS. OPEAug 6, 2012 · N803UA · Airbus A319131 · Airborne Auxiliary Power Unit (APU) SystemSDR UALA2012080604169Light · inoperativeCAPTAIN'S DOME LIGHT INOPERATIVE. RELAMPED, CAPTAINS OVERHEAD DOME LIGHT. OPS CHECKED GOOD .Aug 4, 2012 · N854UA · Airbus A319131 · Flight Compartment LightingSDR UALA2012080704251Door · out of adjustSTRONG VIBRATION IN CLIMB FROM FL200 TO FL290, 79 MACH. PER VIBRATION REPORTING CHECKLIST FROM IMB CREW, VIBRATION WAS FELT IN COCKPIT AND FWD CABIN. ACCOMPLISHED VIBRATION SURVEY REF TSM 05-50-00, FOUND NLG DOOR AFT RIGHT OUT OF LIMITS, ADJUSTMENT REF SEQ NAug 3, 2012 · N831UA · Airbus A319131 · Landing Gear DoorsSDR UALA2012080704250Power Unit · leakingYELLOW-GREEN PTU LEAKING. REPLACED GREEN-YELLOW PTU. BLED SYSTEM AND CHECKED FOR LEAKS. CHECKED OK. OPS CHECK ACCOMPLISHED ON SMC 18.Jul 31, 2012 · N814UA · Airbus A319131 · Hydraulic Filter, AuxiliarySDR UALA2012073004102Duct · crackedNR 1 ENGINE INBD THRUST REVERSER C DUCT IS CRACKED AND CHIPS MISSING JUST AFT OF BLEED 7A. CAN BE REPAIRED PER MT 78-10 EPOXY REPAIR. COMPLETED PER MT 78-010.Jul 29, 2012 · N831UA · Airbus A319131 · Engine Thrust ReverserSDR UALA2012080604208Lens · brokenDOOR 2R EMERGENCY EXIT SIGN, LENS BROKEN AND WILL NOT STAY IN PLACE. REPLACED LIGHT ASSY, OPS OKAY.Jul 29, 2012 · N851UA · Airbus A319131 · Emergency LightingSDR UALA2012073004096Elevator · flutterVERY STRONG FLUTTER IN CLIMB FL230M.77 WITH -.4PITCH TRIM AND IN CLEAR SLOWED IN CLIMB AND DSPTD. CW VIBRATION REPORTING CL, PROCESS FOR ID OF VIBRATION SOURCE, DECISION TREE, DECISION TABLE, IAW DECISION TABLE WAS A TYPE 1, CW FAULT ISOLATION TYPE 1 IAW 27-3Jul 28, 2012 · N831UA · Airbus A319131 · Elevator Control SystemSDR UALA2012073004109Computer · faultyELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. ATTEMPTED SEVERAL RESETS, NO JOY. REPLACED NR 1 ELAC REF AMM. ACCOMPLISHED LAND VERIFY TEST, ALL PASS.Jul 27, 2012 · N817UA · Airbus A319131 · Flight Control SystemSDR UALA2012072704083Skin · damagedLEFT LOWER FUSELAGE SKIN HAS TWO LIGHTNING STRIKES BETWEEN S37-S38L, BETWEEN FRAME 11-12 AND BETWEEN S37L-S38L. REMOVED BLIND RIVETS PER SRM. ACCOMPLISHED HFEC OF THE OPEN HOLES PER NTM 51-10-01 PB 6, NO DEFECTS NOTED. INSTALLED SOLID RIVETS PER SRM. TOP CJul 26, 2012 · N843UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2012072704084Skin · damagedLEFT LOWER FUSELAGE SKIN HAS THREE LIGHTNING STRIKES BETWEEN FRAMES 17-20, S36L AND S37L. REMOVED BLIND RIVETS 3 EA PER SRM. ACCOMPLISHED HFEC ON OPEN HOLES PER NTM 51-10-01 PB 6, NO DEFECTS NOTED. INSTALLED SOLID RIVETS PER SRM AND MT 53-021. TOP COATED PJul 26, 2012 · N843UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2012072704085Skin · damagedLEFT LOWER FUSELAGE SKIN HAS TWO LIGHTNING STRIKES BETWWWN FRAMES 25-26, S35L AND BETWEEN FRAMES 26-27, S34L-S35L. REMOVED BLIND RIVETS 2 EA PER SRM.Jul 26, 2012 · N843UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2012072704086Skin · damagedLEFT LOWER FUSELAGE SKIN HAS FOUR LIGHTNING STRIKES BETWEEN FRAMES 27-28, S35L. REMOVED BLIND RIVETS 4 EA PER SRM. ACCOMPLISHED HFEC ON OPEN HOLES PER NTM 51-10-01 PB 6, NO DEFECTS NOTED. INSTALLED SOLID RIVETS PER SRM AND MT 53-021. TOP COATED PER SRM 51-Jul 26, 2012 · N843UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2012072704087Skin · damagedLT LOWER FUSELAGE SKIN HAS TWO LIGHTNING STRIKE BETWEEN FRAME 23-24 AT S32L AND AT FRAME 25, S35L-S36L. REPLACED BLIND RIVETS 2 EA WITH SOLID FASTENERS PER SRM AND MT53-021. ACCOMP HFEC ON OPEN HOLES PER NTM 51-10-01 PB 6 NO DEFECTS NOTED.Jul 26, 2012 · N843UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2012072704088Skin · damagedLEFT LOWER FUSELAGE SKIN HAS TWO LIGHTNING STRIKES FRAME 28 BETWEEN S36L-S37L AND FRAMES 28-29, S37L. REMOVED BLIND RIVETS 2 EA PER SRM. ACCOMPLISHED HFEC ON OPEN HOLES PER NTM 51-10-01 PB 6, NO DEFECTS NOTED. INSTALLED SOLID FASTENERS PER SRM AND MT 53-021Jul 26, 2012 · N843UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2012072604059Skin · damagedLEFT LWR FUSELAGE SKIN HAS LIGHTNING STRIKES (3EA) BETWEEN FRAMES 21 AND 24 S34L AND S35L.Jul 25, 2012 · N843UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2012072704078Battery · faultyDUE TO REPEAT HITS ON BCL2 WITH BCL2 AND FUSE 4PB2 BEING REPLACED. REPLACED BATTERY 2. TESTED OK ON CFDS.Jul 24, 2012 · N848UA · Airbus A319131 · Battery/Charger SystemSDR UALA2012072704077Oxygen Mask · unwanted deployOXYGEN MASKS DROPPED AT SEATS 25DEF. REPACKED MASKS PER MM, CHECKED CONTAINER PER MT35-003.Jul 24, 2012 · N841UA · Airbus A319131 · Passenger Oxygen SystemSDR UALA2012072303968Wire Harness · burnedAFT LIGHTS FLICKER AND SMELLED SMOKE. AFT GALLEY CONTROL PANEL MODULE HAS TWO BURNED WIRE BUNDLES AT AND ADJACENT TO CONNECTOR 9003ML4. REMOVED MODULE FOR ACCESS AND FOUND CONNECTOR PINS 9003ML4 BURNED. REPLACED WIRES PER WD 25-33-04 PG3.Jul 23, 2012 · N819UA · Airbus A319131 · Electrical Power System WiringSDR UALA2012072303969Power Supply · failedEMERGENCY LIGHT TEST FAILED TEST WITH 'EPSU INT LOAD AFT L'. REPLACED EPSU 13WL, OPS CHECKED OKAY.Jul 23, 2012 · N808UA · Airbus A319131 · Emergency LightingSDR UALA2012072303967Control Unit · failedLANDING GEAR LGCIU 2 ECAM WHEN GEAR EXTENDED ON FINAL. PFR SHOWED LGCIU2. REPACED LGCIU2 PER MM, CHECKED GOOD.Jul 22, 2012 · N846UA · Airbus A319131 · Landing Gear Retraction/Extension SystemSDR UALA2012071903936Structure · missingMETAL PIECE OF FIRE STRIP MISSING INBOARD TOP OF NR 1 ENGINE. APPLIED 3 LAYERS OF SPEED TAPE.Jul 18, 2012 · N806UA · Airbus A319131 · Nacelle/Pylon StructureSDR UALA2012071903937Control Box · failedCIRCUIT BREAKER TRIPPED REAR PANELS. V SHOWING ON LOWER ECAM. AMBER XX'S SHOWN ON ZONE CONTROL. REMOVED, INSPECTED, AND INSTALLED ZONE TEMP CONTROL BOX. VERIFIED GOOD DUCT TEMP.Jul 18, 2012 · N835UA · Airbus A319131 · Cabin Temperature Control SystemSDR UALA2012071803876Blade · damagedNR 2 ENGINE BLADE DAMAGE DUE TO BIRD STRIKE. BEGAN REMOVAL OF FAN BLADE IAW REF AMM. CONTINUE INSTALLATION OF OF FAN BLADES I,A,W REF AMM. NEED TO CON, FROM ITEM-7 THRU END. INSTALLED ENTIRE SET OF BLADES REF, V2500 FAN BLADE DISTRIBUTION PROGRAM FOR WINDOJul 17, 2012 · N818UA · Airbus A319131 · Turbine Engine Compressor SectionSDR UALA2012071703866Bolt · looseFLUID FOUND UNDER NR 1 ENGINE. INVESTIGATED LEAK REPORT FINDINGS IAW AMM 71-70-00(201) FOR ENGINE VENTS AND DRAINS LEAK RATE LIMITS. LCL MAINT REPORTED SCAVENGE OIL TUBE AFT OF DRAIN MAST HAD 2 LOOSE BOLTS, TORQUED BOLTS, CREW ACCOMPLISHED AN IDLE RUN, LEAK Jul 13, 2012 · N850UA · Airbus A319131 · Turbine Engine Oil SystemSDR UALA2012071203777Exhaust Duct · damagedNR 2 ENG EXHAUST TAILCONE AREA. TWO DAMAGED RIVETS AND 1 MISSING RIVET APPROX 7 O'CLOCK POSITION. CARRIED FORWARD IAW MT 78-001 ITEM G. REPLACED RIVETS.Jul 12, 2012 · N812UA · Airbus A319131 · Engine Collector/Tailpipe/NozzleSDR UALA2012071203779Battery · faultyPOST SLIDE REPLACEMENT TEST OF EMERGENCY LIGHTS REVEALED "EPSU RIGHT" MESSAGE. REPLACED EPSU AND BATTERY.Jul 12, 2012 · N852UA · Airbus A319131 · Emergency LightingSDR UALA2012071203778Lens · missingRT SIDE EMERGENCY LIGHT LENS MISSING. EMERGENCY LIGHTS WORK NORMALLY, NO PASSENGER HAZARD.Jul 11, 2012 · N846UA · Airbus A319131 · Emergency LightingSDR UALA2012071103710Rivet · damagedENGINE 2 HAS RIVET ON PENNIB--LEFT SIDE. INSPECTED AREA AND REPORTED 1 RIVET HEAD MISSING, WITHIN 5 0HRS FLY BACK LIMITS OF AMM MT78-001 PARA\M\(2) ON PAGE 6 OF 10. REPLACED RIVET IN NR 2 ENG CNA REF MT 71-001.Jul 11, 2012 · N831UA · Airbus A319131 · Engine Air Intake SystemSDR UALA2012071203767Girt Bar · lack of lubeDOOR 2R WILL NOT ARM. LUBED GIRT BAR FITTINGS AND ROLLERS ON DOOR FRAME. ARM DISARM FUNCTIONS OKAY.Jul 10, 2012 · N816UA · Airbus A319131 · Emergency EquipmentSDR UALA2012070903698Thermostat · failedNR 1 ENGINE BLEED AIR FAULT, RETURNED TO FIELD. ONLY ABNORMAL WAS BLEED TEMP 300C. ECAM PROC FOLLOWED. CHANGED FAN AIR VALVE THERMOSTAT 644-0035 PER AMM 36-11-43.Jul 9, 2012 · N853UA · Airbus A319131 · Pneumatic Distribution SystemSDR UALA2012071103701Connector · unsecureNR 2 ENGINE ANTI-ICE VALVE FAULT, RTFL SECURED CONNECTORS 2420VC, 2421VC, 2425VC, PERFORMED OPS CK PER AMM, SYSTEM TESTED OK.Jul 9, 2012 · N805UA · Airbus A319131 · Ice/Rain Protection System WiringSDR UALA2012071103703Seat · lockedFLT DECK JUMP SEAT UPPER GUIDE BAR LOCKED IN EXTENDED POSITION ACROSS DOORWAY, UNABLE TO RETRACT. INSTALLED INTERIM REPAIR REF ECRA2511-01208. SEAT OPERATES NORMALLY.Jul 9, 2012 · N842UA · Airbus A319131 · Flight Compartment EquipmentSDR UALA2012070903654Actuator · failedAIRFRAME VIBRATION, RTFL. WORSE IN AFT PART OF AIRCRAFT. BOTH LEFT AILERON ACTUATORS REPLACED.Jul 8, 2012 · N831UA · Airbus A319131 · Aileron Control SystemSDR UALA2012071103745Window · damagedNR 3 RT FIXED COCKPIT WINDOW HAS HEAT DAMAGE AND IS CRACKED ALONG FWD EDGE MIDPOINT OF WINDOW. INSPECTED DEPT VERIFIED CRACK PER AMM, MIDDLE PLY CRACKED, PCN 110-3206, AOG R1897.Jul 8, 2012 · N826UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2012070903669Ignition Sys · malfunctionedCREW REPORTED LEFT ENGINE EXPIREANCED HUNG START, ENGINE START FAULT FOLLOWED BY EGT OVER LIMIT FAULT, NO EGT EXCEEDED. SECOND AUTO START SAME RESULT, CYCLED CIRCUIT BREAKERS A04, R41 AND F01, ACCOMPLISHED FADEC AND EIU GROUND SCANS, ANOTHER AUTO START NO HELJul 7, 2012 · N821UA · Airbus A319131 · Ignition Harness (Distribution)SDR UALA2012071103733Bracket · brokenCRASH AXE INBOARD METAL CRADLE BRACKET BROKEN. REPLACED THE SHEARED CLIP.Jul 7, 2012 · N804UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR UALA2012070503588Life Vest · missingCAPTAIN'S LIFE VEST MISSING. SUPPLEMENTAL DATA UPDATE, REPLACED LIFE VEST.Jul 4, 2012 · N808UA · Airbus A319131 · Life JacketSDR UALA2012070303551Fire Bottle · faulty'ENG FIRE EXTING-DISCH' LIGHT OF 'AGENT 1' ILLUMINATED WITHOUT FIRING BOTTLE 1. FOUND CONNECTOR 6WE2 ON BOTTLE NR 1 ENGINE NR 2 LOOSE, SECURED AND CHECKS NORMAL. PROBLEM RECURRED. REPLACED NR 2 ENGINE, NR 1 FIRE BOTTLE PER MM, SYSTEM OPS CHECKED NORMAL. PAJul 3, 2012 · N842UA · Airbus A319131 · Fire Bottle, FixedSDR UALA2012070503612Exhaust Duct · damagedENGINE 1 LOWER EXHAUST TAILCONE FAIRING IS ALSO MISSING ONE RIVET OUTBOARD SIDE ONE HOLE FWD. OK TO CARRY FORWARD FOR REPAIR IN 50 HRS PER MT78-001. REPLACED RIVET REF MR87-0 01.Jul 3, 2012 · N842UA · Airbus A319131 · Engine Collector/Tailpipe/NozzleSDR UALA2012070503613Exhaust Duct · damagedENGINE 1 EXHAUST TAILCONE LOWER FIXED FAIRING OUTBOARD SIDE AFT MOST RIVET DAMAGED AND PROTRUDING. OK TO CARRY FORWARD FOR REPAIR IN 50 HRS PER MT78-001. REPLACED RIVET REF MT 87-001.Jul 3, 2012 · N842UA · Airbus A319131 · Engine Collector/Tailpipe/NozzleSDR UALA2012070503622Exhaust Duct · damagedENGINE 1 UPPER EXHAUST TAILCONE FAIRING HAS 2 MISSING RIVETS ONE INBOARD, ONE OUTBOARD. SUPPLEMENTAL DATA UPDATE, HAVE ONE RIVET ON EACH SIDE OF THE PEN NIB FAIRING MISSING. MEETS THE REQUIREMENT OF MT 78-001 OK TO CONTINUE FOR 50 HRS TO REPAIR. REPLACED RIJul 3, 2012 · N842UA · Airbus A319131 · Engine Collector/Tailpipe/Nozzle
Back to IAE V2522-A5