IAE V2527-A5

Service difficulty reports · 8,009

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 = 'V2527A5'
  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 CALA2013102192214Transceiver · faultyVERY HIGH FREQUENCY RADIO 1 INOPERATIVE. TINNY SOUND & UNREADABLE BY ATC. REPLACED NR 1 VHF TRANSCEIVER, TESTED OK AMM.Oct 19, 2013 · N436UA · Airbus A320232 · VHF Communications SystemSDR CALA2013102192215Transducer · faultyBLUE HYD SYS 3250PSI STDY STATE IN CRUISE. REPLACED HYD PRESSURE TRANSDUCER IAW AMM, OPERATIONS CHECKED NORMAL. NO LEAK FOUND.Oct 19, 2013 · N437UA · Airbus A320232 · Hydraulic Pressure SensorSDR CALA2014110792664Skin · dentedDENT AT FRAME 15 LT SIDE OF FUSELAGE APPROX STRINGER 20, CF9073. MEASURED DENT & FOUND OUT OF LIMITS, INSTALLED REPAIR DOUBLER IAW SRM 53-00-11 FIG 240. REPAIR REQUIRES RE-INSPECTION 60000 FLIGHT CYCLES AFTER REPAIR EMBODIMENT IAW SRM 53-00-11 PG 289 TABLE 2Oct 19, 2013 · N416UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013102192197Handle · unsecureDOOR 2R DOOR ASSIST HANDLE NOT SECURE WILL NEED PCN 110-0938 & 110-0972. SECURED COVER TO HANDLE WITH TAPE. DID OPERATIONAL CHECK OF HANDLE, OPERATIONS CHECKED GOOD, REPLACED HANDLE.Oct 18, 2013 · N408UA · Airbus A320232 · Service DoorsSDR CALA2013102192196Computer · faultyEXTRACT FAULT DISPLAYED ON UPPER ECAM SCREEN, VENT. REPLACED DIRTY DEMISTER FILTER & AEVC. AEVC TESTED GOOD.Oct 18, 2013 · N444UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2013101892187Drain Valve · leakingFOUND YELLOW RESERVOIR DRAIN VLV LEAKING. REPLACED YELLOW HYD RESERVOIR DRAIN VLV, REPLENISHED YELLOW SYSTEM. PRESSURIZED & LEAK CHECKED & NO LEAKS NOTED.Oct 17, 2013 · N406UA · Airbus A320232 · Hydraulic Reservoir, MainSDR CALA2013101892176Generator · malfunctionedNR 2 GENERATOR ELECTRICAL ISSUE, FLT DIVERTED.Oct 16, 2013 · N412UA · Airbus A320232 · AC Generator-AlternatorSDR CALA2013101792135Access Panel · damagedLT WING FUEL TANK ACCESS PANEL 540HB LANDING HAD ONE HOLE ELONGATED. BUSHED IAW SRM 57-21-11, FIG 202. LONGER GRIP LENGTH BOLTS INSTALLED.Oct 16, 2013 · N433UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2013101792136Access Panel · damagedRIGHT WING FUEL TANK ACCESS PANEL 640JB LANDING HAD TWO HOLES ELONGATED. BUSHED IAW SRM 57-21-11, FIG 202. LONGER GRIP LENGTH BOLTS INSTALLED. REPAIRED IAW 57-21-11-2-002-00, PAR 3.B . TABLE 203.Oct 16, 2013 · N433UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2013101592065Unknown · malfunctionedSDCU CHANNEL 1 DOES NOT TURN ON RED MASTER CAUTION LIGHT OR CHIMES DURING SMOKE DETECTOR PUSH BUTTON TEST.Oct 15, 2013 · N436UA · Airbus A320232 · Smoke DetectionSDR CALA2013101692098Fireseal · crackedNR 2 ENG INBD PYLON TO ENG FIRESEALS APPEAR TO BE CRACKED. REMOVED PANELS 425AL, 481AL, 425 BL & SPRING SEALS ON INBD SIDE OF PYLON & REVERSER FOR ACCESS. REMOVED CRACKED SEAL ASSEMBLY, NEW SEAL ASSEMBLY IS PLANE SIDE. INSTALLED NEW SEAL ASSEMBLY & SPRING OOct 15, 2013 · N435UA · Airbus A320232 · Nacelle/Pylon, Bulkhead/FirewallSDR CALA2013101692089Skin · gougedFUSELAGE GOUGE BETWEEN FR 1 & 2 ON BELLY. INSTALLED DOUBLER REPAIR IAW SRM53-00-11 FIG 244.Oct 15, 2013 · N416UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2013101592067Connector · unsecureFIRST OFFICERS O2 MASK MIC INOPERATIVE. SECURED MASK CONNECTOR & OPERATIONS CHECKED OKAY.Oct 14, 2013 · N477UA · Airbus A320232 · Oxygen System WiringSDR CALA2013101592068Control Panel · faultyENG 2 AGENT 1 DISCHARGE LIGHT DOES NOT ILLUMINATE WITH FIRE TEST. OK WITH LAMP TEST. ENG APU FIRE CONTROL PANEL, OPERATIONS OK.Oct 14, 2013 · N461UA · Airbus A320232 · Fire DetectionSDR CALA2013101692097Control Unit · faultyCARGO SMOKE DETECTOR TEST SMOKE LIGHTS ONLY ILLUMINATED ONCE DURING TEST. REPLACED SDCU IAW MM 26-17-34. RE-RACKED FWC 1 & 2, SECURED ALL CONNECTORS ON ALL 9 SMOKE DETECTORS, VERIFIED ALL WIRES WERE SECURE ON TB 1871VT BLOCK 63, ACCOMPLISHED TEST IAW 26-17-0Oct 14, 2013 · N436UA · Airbus A320232 · Smoke DetectionSDR CALA2013101892188Landing Gear · malfunctionedTEST FLT FAILED. REPORTEDLY TOOK RT MLG 4 ADDITIONAL SECONDS & LT MLG 6 ADDITIONAL SECONDS TO RELEASE THE BALK SOLENOID TO ALLOW GEAR HANDLE TO BE MOVED UP. REPLACED LT & RT MLG IAW ECRA 3210-02291.Oct 14, 2013 · N407UA · Airbus A320232 · Main Landing GearSDR CALA2013101592066Sensor · malfunctionedSLAT SYSTEM 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. HAD THIS ECAM TWICE DURING FLT ACCOMPANIED BY SLOW SLAT FLAP RETRACTION AFTER TAKEOFF, ONE TIME IN CRUISE. FAULTS "SLT FLP CSU 51CV OR WIRING TO SLT 2", CSU PCN 482-9083. REPLACED COMMAND SENSOR UNIT IAW MOct 14, 2013 · N474UA · Airbus A320232 · Leading Edge Slat Control SystemSDR CALA2013101492051Power Supply · failedEMERGENCY LIGHT TEST FAILED EPSU FWD LT. REPLACED EPSU AT FWD LT TEST NOT FAULTING FWD EPSU IAW TSM 33-51-00.Oct 13, 2013 · N481UA · Airbus A320232 · Emergency LightingSDR CALA2013101592055Engine · making metalENG 2 STALL ECAM, FLT DIVERTED. EXAMINE THE INLET & EXHAUST FOR FOREIGN MATERIAL OR INDICATION OF INTERNAL ENG DAMAGE. IAW MM TASK 71-00-00-810-809-A, INSPECTED ENG FOUND METAL PIECES IN TAILPIPE.Oct 12, 2013 · N485UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2013101491999Fan · malfunctionedCB X18-RECIRCULATING FAN LT SUPPLY TRIPPED. ALSO HAD ELEC SMELL BEFORE TRIPPING. R & R RECIRCULATING FAN IAW AMM, OPERATIONS NORMAL ACFT OK FOR SERVICE, REMOVED PLACARD.Oct 12, 2013 · N443UA · Airbus A320232 · Air Distribution FanSDR RJEF20131011009Coffeemaker · odorDURING FLIGHT, PILOT REPORTED ELECTRICAL FUMES DETECTED FWD AND AFT GALLEY, ACFT DIVERTED AND DECLARED AOG. MAINTENANCE PERFORMED TSM 05-50-00-810-831-A. FOUND FWD COFFEE MAKER RESPONSIBLE.Oct 11, 2013 · N492TA · Airbus A320233 · Buffet/GalleysSDR CALA2013101191954Structure · dentedFUSELAGE DENT BETWEEN FR 63 & 64 AT STRINGER 21L. DENT OUT OF LIMIT, INSTALLED DOUBLER REPAIR.Oct 10, 2013 · N417UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013101191965Actuator · faultyCOMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENG PARAMETERS ABNORMAL, ENG NR 2. REPLACED NR 2 ENG VSV ACTUATOR IAW AMM.Oct 10, 2013 · N411UA · Airbus A320232 · Compressor Bleed ControlSDR CALA2013100991878Drain Valve · leakingGREEN SYSTEM RESERVOIR DRAIN VLV LEAKING. REPLACED VLV IAW MM, LEAK CHECKED GOOD.Oct 9, 2013 · N497UA · Airbus A320232 · Hydraulic Reservoir, MainSDR CALA2013101091924Proximity Sensor · brokenLGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN L-G. CONNECTOR BROKEN OFF ON NLG EXT PROX SENSOR 24GA. REPLACED PROX SENSOR 24GA IAW MM.Oct 9, 2013 · N408UA · Airbus A320232 · Landing Gear Position and WarningSDR CALA2013101091925Wire · damagedEMERGENCY LIGHT AT LT FWD WINDSCREEN IS INOPERATIVE. TERMINATED EXIT LIGHT WIRING.Oct 9, 2013 · N458UA · Airbus A320232 · Light System WiringSDR CALA2013101091942Fan · faultyEXHAUST FAN FAULT. SECURED 2 1HQ COND AIR INLET VLV IN THE OPEN POSITION. REPLACED EXTRACT FAN IAW AMM. RESET SYSTEM, PERFORMED AEVC TEST ON CFDU TEST PASSED.Oct 9, 2013 · N496UA · Airbus A320232 · Air Distribution FanSDR CALA2013101091943Warning Light · illuminatedAFTER FIRE TEST APU FIRE AGENT DISCHARGE LIGHT REMAINED ILLUMINATED. PLACARDED APU DISCHARGE LIGHT. APU IS CONSIDERED INOPERATIVE IAW MEL 2622C. STICKER INSTALLED.Oct 9, 2013 · N438UA · Airbus A320232 · Extinguishing SystemSDR CALA2013101091944Structure · damaged2R SLIDE BUSTLE DAMAGED ON BOTTOM SIDE. REPLACED DOOR BUSTLE.Oct 9, 2013 · N442UA · Airbus A320232 · Service DoorsSDR CALA2013100891868O-Ring · damagedOIL PUDDLE UNDER NR 2 ENG. IAW LOG 1, INSPECTED NR 2 ENG & FOUND OIL LEAKING FROM OIL TUBE ON FWD FACE OF ANGLE GEAR HOUSING. OIL PUDDLE UNDER NR 2 ENG, OIL QTY 21.5 QTS. TUBE IS INBD & JUST ABOVE THE ENG DRAIN MAST. REMOVED ADAPTER FROM GEARBOX FOR REPAIR.Oct 8, 2013 · N453UA · Airbus A320232 · Turbine Engine Oil SystemSDR CALA2013100991875Display · faultyCAPTS PFD INOPERATIVE INDMC POSITION 1-2-3. CAPTS PFD DOES NOT DISPLAY SHOWS WHITE DIAGONAL LINE. WHEN SELECTING CAPTS PFD XTR SWITCH, ADI DISPLAYED ON ND, HSI DISPLAYED ON PFD. COMPLIED WITH MEL CARD. REPLACED CAPT'S PFD,TESTED OK.Oct 8, 2013 · N410UA · Airbus A320232 · Central DisplaySDR CALA2013100991876Oxygen Mask · brokenCAPT O2 MASK BROKEN RED INFLATE BUTTON BROKEN. R & R CAPT O2 MASK, OPERATIONS CHECKED GOOD.Oct 8, 2013 · N482UA · Airbus A320232 · Crew Oxygen SystemSDR CALA2013100991879Rivet · looseSEVERAL LOOSE RIVETS ON NR 1 ENGINE CNA. REPLACED LOOSE FASTENERS IAW MT 78-001.Oct 8, 2013 · N429UA · Airbus A320232 · Engine Exhaust SystemSDR CALA2013100791793Liner · missingNR 2 ENG INTAKE INSULATION AT 2 O'CLOCK POSITION HAS COME OFF. ACTUAL IS ATTRITION LINER MISSING 1X1 SECTION AT THE 11 O'CLOCK POSITION. MUST BE REPAIRED IAW MT 72-017 WITHIN 20 CYCLES. REPAIRED ATTRITION LINER IAW MT 72-017.Oct 7, 2013 · N414UA · Airbus A320232 · Turbine Engine Air Inlet SectionSDR CALA2013100891867Valve · faultedNR 2 ENGINE HP VALVE FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED NR 2 ENGINE HP VALVE IAW MM, OPS CHECKED GOOD.Oct 7, 2013 · N486UA · Airbus A320232 · Pneumatic Distribution SystemSDR CALA2013100891835Nut Plate · unsecureLEFT OVERWING SLIDE HAS ONE STUD HANGING OUT IN LOWER AFT CORNER. REMOVED SLIDE & REPLACED NUTPLATE, REINSTALLED LT OVERWING SLIDE IAW MM.Oct 6, 2013 · N473UA · Airbus A320232 · Emergency EquipmentSDR CALA2013100791794Blade · damagedUPON ARRIVAL ACCOMPLISHED TAP TEST ON ENG NR 1 & FOUND THAT BLADE NR 21 FAILS TAP TEST READ OUT ARE 1867 DB PER SEC. REPLACED FAN BLADE IAW AMM. RAN BOTH ENGINES UP AS PER VIBRATION SURVEY INSTRUCTIONS. N 1 & N 2 VIBRATION OF ENG NR 1 ARE WITHIN LIMITS.Oct 5, 2013 · N465UA · Airbus A320232 · Turbine Engine Compressor SectionSDR CALA2013100891836Master Cylinder · faultyLT BRAKE STILL VERY SENSITIVE, OVER BRAKES AT THE SLIGHTEST TOUCH MAY CAUSE PROBLEMS. LT BRAKE PEDAL MASTER CYLINDER IAW MM.Oct 5, 2013 · N431UA · Airbus A320232 · Master Cylinder/Brake ValveSDR CALA2013100891871Battery · dischargedEMERGENCY LIGHTS FAILED AT CIDS. REPLACED BATTERY AT EPSU 12WL, OPERATION TESTED OKAY.Oct 5, 2013 · N465UA · Airbus A320232 · Emergency LightingSDR CALA2013100891872Regulator · faultyCREW OBSERVED ON COND PAGE AFT CARGO HEAT REG VLV GREEN & CLOSED, PIT TEMP 60. WHEN SELECTING TEMP SELECTOR FULL WARM, TEMP VLV & REG VLV REMAIN CLOSED. NO FAULTS DISPLAYED ON ECAM. REPLACED REGULATOR & TRIM VLV, OPERATIONS CHECKED OK.Oct 5, 2013 · N461UA · Airbus A320232 · Cabin Temperature Control SystemSDR CALA2013100491730Oxygen Mask · unsecurePASSENGER SEAT OVERHEAD 02 MASK FELL AT 24ABC. PERFORMED MT 35-003 ALL PARTS LOOK NORMAL NEEDS MASK DROP TEST.Oct 4, 2013 · N428UA · Airbus A320232 · Passenger Oxygen SystemSDR CALA2013100791766Screw · loosePANEL 191KB LOOSE SCREW INBD SIDE 4 FROM AFT EDGE. NEEDS NEW NUTPLATE TO BE REPAIRED WITHIN 10C.Oct 4, 2013 · N437UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013100791816Engine · bird ingestionHI SPEED ABORT AT 110KTS, DUE TO BIRD STRIKE ON LT MOTOROct 4, 2013 · N432UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2013100891870Bleed Air Sys · fluctuatesNR 1 PRECOOLER INLET PRESSURE FLUCTUATES UP TO 10 PSI WITH HP VALVE OPEN IDLE POWER. AUDIBLE.Oct 4, 2013 · N462UA · Airbus A320232 · Pneumatic Distribution SystemSDR CALA2013100791761Stringer · corrodedCORROSION FOUND ON STRINGER 42L BETWEEN FRAMES 63-64 IN AFT CARGO. R & R STRINGER IAW SRM 51-42-11.Oct 4, 2013 · N475UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013100491727Control Unit · faultedUNABLE TO SELECT HEADING WHILE IN NAV MODE. REPLACED CONROL UNIT PER AMM. PERFORMED CAT III PER AMM 22-97-00. OPS CHECKED GOOD.Oct 4, 2013 · N419UA · Airbus A320232 · Auto Flight SystemSDR CALA2013100491728Seal · out of positionLT WING BODY AFT BODY FAIRING SEAL IS OUT OF PLACE. SEAL IS AFT LT HAND AFT ELEPHANT EAR FAIRING. INTERIM REPAIR WITH HIGH SPEED TAPE MADE.Oct 3, 2013 · N474UA · Airbus A320232 · Aerodynamic FairingsSDR CALA2013100491731Fastener · looseRAMP REPORTED ONE LOOSE FASTENER ON LOWER BODY PANEL TO CREW. REPLACED FASTENER & BARREL.Oct 3, 2013 · N437UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2013100891869Battery Pack · dischargedEMERGENCY LIGHT TEST FAILED FWD LT. REPLACED BATTERY PACK BY DOOR 1L IAW MM, TEST PASSED.Oct 3, 2013 · N457UA · Airbus A320232 · Emergency LightingSDR CALA2013100291651Seat Belt · detachedSEAT BELT AT 25D BECAME DETACHED. ATTACHMENT POINT BROKEN.Oct 2, 2013 · N405UA · Airbus A320232 · Passenger Compartment Equipment
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