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 UALA2011072803899Door · brokenCAPTAIN`S FWD OXYGEN MASK DOOR IS BROKEN. REPLACED O2 BOX PER AMM.Jul 27, 2011 · N829UA · Airbus A319131 · Fixed Inner DoorsSDR UALA2011072703851Computer · intermittentECAM FLT CNTL - ELAC 2- CYCLED ELAC 2. OPS OK, OCCURRED ON GROUND. ELAC2 FAULT INTERMITTENT, ALSO ORDERED FCDC2 ON AOG. ACP TSM27-93-00-810-836. REPLACED ELECTRONIC MODULE N1 ON PITCH TRIM ACTUATOR. OPS CHECKED OK. FAULT CLEARED.Jul 27, 2011 · N823UA · Airbus A319131 · Flight Control SystemSDR UALA2011072703859Battery · failedFWD LT DOOR FAILED EMERGENCY LIGHT CHECK. REPLACED BATTERY.Jul 27, 2011 · N832UA · Airbus A319131 · Emergency LightingSDR UALA2011072703848Actuator · malfunctionedRUDDER IS HARD TO DISPLACE TO THE LEFT ON TAKEOFF ROLL. RIGHT DISPLACEMENT NORMAL. ACCOMPLISHED CHECKS FOR RUDDER PEDAL STIFFNESS PER TSM. PER TSM TASK 27-20-00-810- 801 ACCOMPLISHED OPS OF RUDDER ARTIFICIAL-FEEL LOADS. ACCOMPLISHED YAW DAMP FUNCTION TEST Jul 26, 2011 · N848UA · Airbus A319131 · Rudder ActuatorSDR UALA2011072503757Battery Pack · inoperativeEPSU BATTERY AFT L, WHEN PERFORMING CABIN EMERGENCY LIGHTS CHECK. REPLACED BATTERY, TESTED GOOD.Jul 23, 2011 · N834UA · Airbus A319131 · Emergency LightingSDR UALA2011072503809Starter · sparksCREW REPORTED SPARKS FROM NR 1 ENG COWL DURING ENGINE START. REPLACED STARTER PER MM.Jul 23, 2011 · N806UA · Airbus A319131 · Engine StarterSDR UALA2011072503783Igniter · malfunctionedSTART FAULT DISPLAYED ON UPPER ECAM SCREEN. ENGINE START USING MANUAL PROCEDURE NORMAL. REPLACED A IGNITOR PLUG AND A IGNITION PER MM. ACP OPS CHECK PER MM. OPS CHECKS GOOD.Jul 23, 2011 · N840UA · Airbus A319131 · Spark Plug/IgniterSDR UALA2011072503805Flt Controls · malfunctionedON 2 LEGS NOTED EXCESSIVE YAWING IN BACK OF A-C. PASSENGERS GETTING SICK FLYING IN SMOOTH AIR. PERFORMED AFS BITE=BOTH FAC COMPUTERS=NO FAULTS. PERFORMED OPERATIONAL TEST OF THE YAW DAMPER FUNCTION OF SYSTEM 1 AND SYSTEM 2=NO FAULTS.Jul 22, 2011 · N833UA · Airbus A319131 · Flight Control SystemSDR UALA2011072103702Computer · faultedSPOILER 1 FAULT DISPLAYED. REPLACED FCDC NR 2 AND SECURED SEC UNITS IN POSITION NR 2 AND 3. SPOILER SYSTEM OPS CHECKED GOOD.Jul 21, 2011 · N831UA · Airbus A319131 · Drag Control SystemSDR UALA2011072103701Structure · damagedFWD CARGO DOOR OPENING DAMAGED AT FWD EDGE OF DOOR OPENING APPROX MEASURES 3-4" BY 5-16". REMOVED DAMAGE. BLENDED AND NOW MEASURES 1.500" LENGTH BY .260" WIDTH BY .220" DEPTH.Jul 21, 2011 · N847UA · Airbus A319131 · Cargo/Baggage DoorsSDR UALA2011072103713Structure · puncturedPUNCTURE HOLE IN LOWER SIDE OF RIGHT INBOARD FLAP. SMALL PUNCTURE IN FOIL-TAPE HOLE COVER. HOLE IN QUESTION, 24 INCHES OUTBOARD OF INBOARD EDGE OF RIGHT INBOARD T/E FLAP APPEARS TO BE HOIST POINT. APPLIED METAL TAPE PER MM, TO BE REPAIRED AT NEXT C-CHECK.Jul 21, 2011 · N838UA · Airbus A319131 · Trailing Edge FlapsSDR UALA2011072203742Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. FLT CONTROL ELAC PITCH FAULT WILL NOT RESET PER SYS RESET. CIRCUIT BREAKER RESET NO HELP, ELAC 1 REPLACED: NO HELP, FAILS DURING FLT CONTROL CHECK WITH FAULT CODE "ELAC 1 COM OR WIRING TO L.B. ELEV SERVO 34CE3". Jul 21, 2011 · N803UA · Airbus A319131 · Flight Control SystemSDR UALA2011072003689Computer · faultyELEV SERVO FAULT DISPLAYED. CREW ACTUALLY CYCLED SEC 2 CB, NOT ELAC 2 PER CREW. REPLACED SEC 2 FOR T-S PER AMM. STARTED ADJ AND TEST PER AMM. TEST FAILED AT STEP 21 PG 506. PITCH TRIM FAILED TO ROLL BACK TO ZERO AUTOMATICALLY. PFR, 02-27-94-34 SEC2 COM OJul 20, 2011 · N840UA · Airbus A319131 · Elevator Control SystemSDR UALA2011071903684Computer · faultyREJECTED TAKEOFF, LESS THAN 60 KNTS, DUE TO ELAC 1 FAULT. RESET ELAC AND FAULT CLEARED. PERFORMED FLT CONT CHECK AND ELAC 1 FAULTED WITH MOVEMENT OF F/O'S SIDESTICK. REPLACED ELAC1 PER MM. PERFORMED NORMAL AFS AND LAND TEST PER MM. A/C RETAINS CAT III B SJul 18, 2011 · N846UA · Airbus A319131 · Elevator Control SystemSDR UALA2011071903669Battery · dischargedEMERGENCY LIGHTS TEST FAILS WITH "EPSU INT LOAD EMER R" MESSAGE. REPLACED EPSU BATTERY AT RIGHT OVERWING LOCATION. EMER LIGHTS TEST PASSED.Jul 18, 2011 · N806UA · Airbus A319131 · Emergency LightingSDR UALA2011071703616Connector · damagedNO GPS 2 INFORMATION DISPLAYED ON GPS MONITOR. REPLACED GPS 2 ANTENNA, NO HELP. FOUND GPS#2 COAX CABLE TO ANTENNA OPEN. UPPER ANTENNA CONNECTOR BAD, WORKING TO REPAIR. NR 2 GPS ANTENNA CONNECTOR WAS REPAIRED AND RETURNED GPS BACK TO SERVICE.Jul 17, 2011 · N817UA · Airbus A319131 · Navigation System WiringSDR UALA2011071703620Seal · missingDOOR 2L SQUEAL. REPOSITIONED ESCAPE SLIDE MOORING LINE IN GIRT CURTAIN ACCT HANGING IN DOOR SILL AND CLEANED LWR AREA OF DOOR SEAL. FOUND OUTFLOW SEAL MISSING. REPLACED PER MM. OPS CHECKED WITH NO FAULTS NOTED.Jul 17, 2011 · N821UA · Airbus A319131 · Pressure Regulator/Outflow ValveSDR UALA2011071903685Apu · faultyEXCESSIVE SMOKE FROM APU EXHAUST AFTER ENGINE START. COMPLIED WITH MEL. APU INOP. CHK'D APU COMPARTMENT AND TAILPIPE FOR OIL WETTING, LEAKS, OR EVIDENCE OF BURNING, NONE FOUND. ATTEMPTED TWO STARTS AT GATE ON TURN: HUNG AT 27-29% N, TEMP 770-800 DEG BOTH TJul 17, 2011 · N810UA · Airbus A319131 · APU Core EngineSDR UALA2011071703625Seal · brokenAUTOMATED EXTERNAL DEFIBRILLATOR (AED) HAS BROKEN OR MISSING GREEN SEAL. REPLACED KIT.Jul 16, 2011 · N834UA · Airbus A319131 · Emergency EquipmentSDR UALA2011071703624Tire · damagedEXCESSIVE NOSE WHEEL SHIMMY ON TAKEOFF AND AFTER ROTATION. REPLACED BOTH NOSE TIRES IAW AMM. FOUND ONE TIRE WITH FLAT SPOTS.Jul 16, 2011 · N843UA · Airbus A319131 · TireSDR UALA2011071503594Unknown · vibrationNR 2 ENGINE N1 VIBRATION AT 6.2 WHEN ABOVE IDLE. AT IDLE VIBRATION 5.0. DEBRIEF CREW FOR CONDITIONS AND IF VIBRATIONS FELT. VISUALLY ACCOMPLISHED A VISUAL INSPECTION OF INLET AND EXHAUST AND NO APPARENT DAMAGE NOTED. MASTER CHIP DETECTOR FOUND CLEAN. ACCOMJul 15, 2011 · N828UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR UALA2011071403568Unknown · damagedHAIL STRIKE DAMAGE.Jul 14, 2011 · N814UA · Airbus A319131 · Fuselage Structure (General)SDR UALA2011071403569Unknown · damagedCREW REPORT: HEAVY HAIL ENCOUNTERED AT GATE.Jul 14, 2011 · N813UA · Airbus A319131 · Fuselage Structure (General)SDR UALA2011071403570Wedge · damagedLEFT OUTBD TRAILING EDGE FLAP, TRAILING EDGE WEDGE HAS NUMEROUS HAIL-DAMAGE DENTS APPROXIMATELY ONE-SIXTEENTH OF AN INCH DEEP.Jul 14, 2011 · N825UA · Airbus A319131 · Trailing Edge FlapsSDR UALA2011071503608Oxygen Mask · failedF/O'S OXYGEN HARNESS FAILS TO INFLATE (LEAKING). MASK FAILED TO INFLATE DURING TEST. SWAPPED F/O O2 MASK WITH 1ST OBS SEAT REF AMM. F/O O2 MASK HARNESS INFLATES NORMALLY. 1ST OBS MASK INOPERATIVE.Jul 14, 2011 · N810UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2011071403581Skin · dentedFLAP HAS MULTIPLE DENTS FROM HAIL. ACCOMPLISHED INSPECTION OF DENTS PER SRM. NO DENTS WERE FOUND TO BE GREATER THAN .020 INCH IN DEPTH ON TOP AND BOTTOM SURFACES. NO DENTS WERE FOUND TO BE BEYOND LIMITS.Jul 14, 2011 · N830UA · Airbus A319131 · Trailing Edge FlapsSDR UALA2011071303529Module · faultyEMERGENCY LIGHTS COME ON WITH SWITCH OFF WHEN POWER IS REMOVED FROM AIRPLANE. JUMPERED SOCKET "S" OF CONNECTOR 2423VC TO GND AND EMERGENCY LIGHT SHUTS OFF. PANEL FOR EMERGENCY LIGHT SWITCH AND OLD SWITCH 4WL UNSECURED IN A/C. REPLACED SWITCH, NO HELP. REPLJul 13, 2011 · N838UA · Airbus A319131 · Emergency LightingSDR UALA2011071503601Switch · inoperativeCAPTAIN'S OXYGEN MASK RESET SWITCH DOES NOT RESET. REPLACED O2 BOX ASSY, OPS GOOD.Jul 13, 2011 · N850UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2011071203493Windshield · leakingF/O FRONT WINDOW HAS A SQUEAK TOP MIDDLE FRAME STARTS AROUND FL190 AND DECREASES. DUE TO RAIN, FOUND 2 LEAKS IN F/O FRONT WINDOW. ONE LEAK FOUND APPROX 7 INCHES INBD OF LOWER OTBD CORNER AND SECOND LEAK FOUND APPROX 6 INCHES UPPER INBD CORNER (PINHOLE THROUGJul 12, 2011 · N820UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2011071303540Latch · out of adjustO2 MASKS DEPLOYED AT 29ABC. O2 DEPLOYMENT WAS AT 28ABC NOT 29ABC, SEATS 28ABC HAVE BEEN REMOVED FROM SERVICE. ADJUSTED CONTAINER DOOR LATCHING PIN PER MT. REPACKED MASKS PER AMM AND PERFORMED SATISFACTORY OPERATIONAL CHECK OF MANUAL MASK RELEASE PER MM. SEATJul 12, 2011 · N833UA · Airbus A319131 · Passenger Oxygen SystemSDR UALA2011071103432Unknown · malfunctionedLOP LIGHT, RTFL. ENG 2 CREW COMMENTS: ENG LOW OIL PRESS INDICATION. 16 PSI IND. RETURNED TO NORMAL ONE MINUTE LATER. RPL'D BURNDY BLOCK AND OIL PRESSURE TRANSMITTER. IDLE RAN ENGINE FOR 5 MINUTES AND OIL PRESSURE SHOWED 156PSI. REPLACED ENG INTERFACE UNIJul 10, 2011 · N836UA · Airbus A319131 · Engine Oil PressureSDR UALA2011071103472Oxygen Mask · faultyCAPT O2 MASK INTERCOM APPEARS INOP. REPLACED CAPTAINS QUICK DONNING OXYGEN MASK ASSY PER AMM, OPERATIONAL TEST NORMAL.Jul 10, 2011 · N828UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2011070703376Exciter · arcedNR 2 ENGINE IGNITION SYSTEM 'A' INOPERATIVE. FOUND ARCING ON THE IGNITER PLUG AND LEAD, REPLACED LEAD, IGNITER PLUG AND EXCITER BOX, OP CHECK GOOD.Jul 7, 2011 · N826UA · Airbus A319131 · ExciterSDR UALA2011070803395Cap · defectiveSEAT 7F ARMREST HAS SHARP EDGES. NEEDS TAPE JOB. MADE INTERIM REPAIR WITH TAPE ARM CAP COVER MISSING. REPLACED ARM REST.Jul 7, 2011 · N826UA · Airbus A319131 · Passenger Compartment EquipmentSDR UALA2011070703370Computer · faultyENG 1 OIL QUANTITY INDICATION INOP ON ENG ECAM SYSTEM PAGE. OIL PRESSURE AND TEMP NORMAL ENG 1. REPLACED OIL QUANTITY TRANSMITTER. RPLC XMTR DID NOT CORRECT PROBLEM. CHECKED WIRING REF WDM79- 36-01. NO FAULTS FOUND WHILE SHAKING WIRES INSPECTED TB 1851VT Jul 6, 2011 · N843UA · Airbus A319131 · Engine Oil QuantitySDR UALA2011070703366Unknown · odorAFT GALLEY SMOKE SMELL AFTER ENGINE START WITH APU SHUT DOWN. SAMC TEXT: WITH AFT GALLEY EQUIPMENT SHUT OFF SMELL DISSIPATED. OPEN UP AFT GALLEY CEILING AND AFT GALLEY ELECTRICAL PANEL - PERFORM GVI OF AREA. DE-POWERED GALLEY REF MM, OPENED UP AFT GALLEY CJul 6, 2011 · N822UA · Airbus A319131 · Air Distribution SystemSDR UALA2011070503332Oxygen Mask · faulty1ST O/B'S OXYGEN MASK MICROPHONE IS INOPERATIVE. REPLACED O2 MASK AND BOX STOWAGE AT FIRST OFFICER SIDE, TESTS OKAY. O2 MASK REPLACED PER AMM. TEST OKAY.Jul 4, 2011 · N818UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2011070603334Structure · damagedFUSELAGE DAMAGE JUST AFT OF THE FWD PIT. 3 AREAS WITH METAL LOSS "12 INCHES BY 3-8TH" AREA BLENDED AND MAPPED, INFO WITH ORDLE. COMPLETING HIGH WIND INSP, AND CLOSING UP FAIRING. FWD PIT BELLY SKIN DMG. MACHINED REPAIR DOUBLER PLANESIDE. SMC3, AT SKIN DAMJul 2, 2011 · N812UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2011070503282Elt · damagedAFT ELT FOAM DAMAGED AND TORN. NIS DENVER. DF REF MEL2560. REPLACED AFT CABIN TRANSMITTER EMERGENCY LOCATOR ELT PER AMM.Jul 2, 2011 · N801UA · Airbus A319131 · Emergency Locator BeaconSDR UALA2011070103274Computer · faultyELAC 2 PITCH FAULT. DURING T-S UNABLE TO DRIVE THS WITH SPOILER AND ELEVATOR COMPUTER ONLY. (SEC1) REPLACED NR 1 SPOILER & ELEVATOR COMPUTER (SEC1) PER MM. OPS CHECK GOOD PER MM.Jun 29, 2011 · N840UA · Airbus A319131 · Drag Control SystemSDR UALA2011062903211Tire · vibrationNOSE WHEEL CONTINUES TO ROTATE FOR 5 MINS CAUSING VIBRATION AFTER T/O. REPLACED BOTH NOSE TIRES DUE TO VIBRATION.Jun 28, 2011 · N805UA · Airbus A319131 · Tire TubeSDR UALA2011062903220Computer · faultedELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. FLT CONTROL, ACFT PITCHED UP ABRUPTLY WHILE AP 2 ON. POST FLIGHT REPORT SHOW THS ACTR POS ERROR 9CE OF ELAC 2 MSG 274451. REPLACED ELAC 2 COMPUTER, NO HELP. SWAP WITH ELAC 1, NO HELP. REINSTALL TO ORIGINJun 27, 2011 · N840UA · Airbus A319131 · Flight Control SystemSDR UALA2011062703132Panel · damagedDAMAGE NOTED ON PANEL 621EB TRAILING EDGE. DAMAGED ON OUTBOARD SECTION NEAR ENG 2. REPLACED PANEL 621EB RT WING.Jun 26, 2011 · N828UA · Airbus A319131 · Wing, Plate/SkinSDR UALA2011062903222Power Supply · faultyEMERGENCY LIGHT SYS TEST AT DOOR 1LT FAILS SELF TEST. SHOWS 'EPSU INT LOAD AFT LT. REPLACED 13WL.Jun 26, 2011 · N840UA · Airbus A319131 · Emergency LightingSDR UALA2011062703131Valve · faultedENG 1 FUEL HEAT SYS DISPLAYED IN UPPER ECAM ON TAXI OUT. POST FLIGHT REPORTS FAULTS FUEL DIVERTER RETURN VALVE.Jun 25, 2011 · N810UA · Airbus A319131 · Engine Fuel DistributionSDR UALA2011062703133Multiplexer · malfunctionedSMOKE ODOR IN CABIN, NOT VISIBLE, ODOR REPORTED FIRST IN AFT CABIN, RESULTING IN A DIVERSION. RAN COFFEEMAKERS, OVENS AND INSPECTED GALLEY AREAS, NO DEFECTS FOUND. CIRCUIT BREAKER PANELS COOL TO TOUCH, NOTED RESIDUAL SMOKE ODOR NEAR SEATS 34ABC & PCU'S AT THEJun 25, 2011 · N841UA · Airbus A319131 · Entertainment SystemSDR UALA2011062403113Windshield · leakingHIGH PITCHED SQUEAL FROM F/O SIDE. QUIETER AT LOW ALTITUDES. REMOVED WINDSHIELD. CLEANED MATING SURFACES. RE-INSTALLED WINDSHIELD.Jun 24, 2011 · N817UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2011062403101Oxygen Mask · inoperativePAX O2 MASKS DOWN AT 27 ABC. SEAT ROW 27ABC PAX O2 STORAGE RENDERED INOPERATIVE PER MEL 35060. MASK'S HAVE BEEN REPACKED. RAN TEST ON SYSTEM RESET OPS CHECKED NORMAL IAW AMM.Jun 23, 2011 · N802UA · Airbus A319131 · Passenger Oxygen SystemSDR UALA2011062203077Skin · damagedFUSELAGE DAMAGE JUST AFT OF THE FWD PIT. REMOVED DAMAGE PER ACCOMPLISH HFEC AND PROCEED WITH REPAIR WITH NO ALTERATIONS. ACCOMPLISHED HFEC, NO CRACK INDICATION FOUND. MANUFACTURED FILLER SHIMS FOR AREA 1 AND AREA 2 IN LOWER SKIN PER DRAWING IAW UA-EVA-80978.Jun 22, 2011 · N812UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR UALA2011062303097Lanyard · unsecureLANYARD HANGING FROM DOOR 1L AFTER CLOSURE. RE-SECURED LOOSE LANYARD AT DOOR 1L.Jun 22, 2011 · N809UA · Airbus A319131 · Escape Slide
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