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 UALA2013041802691Power Supply · inoperativeWHILE PERFORMING EMERGENCY LIGHT SYSTEM TEST ON CIDS, GOT FAULT MSG EPSU BATTERY AFT L (ATA 33-51-38). REPLACED AFT LEFT EMERGENCY POWER SUPPLY AND BATTERY FOR 13WL UNIT. ACP POWER SUPPLY BITE AND AC EMERGENCY BATTERY CHECK BOTH TESTED GOOD REF AMM 33-51-38-Apr 16, 2013 · N497UA · Airbus A320232 · Emergency LightingSDR UALA2013041702622Line · leakingNR 1 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMIT. FOUND OIL LINE LEAKING FROM WEAR AT CLAMP. REPLACED LINE REF MM79-20-00 AND PTT SEQ 0592002 THRU 0592007. NR 1 ENGINE,OIL LINE LEAKING UNDER CLAMP, SEE IPC 79-21-49-81 ITEM 50A PCN 222-0664. REPLACED OIL LINE PApr 16, 2013 · N452UA · Airbus A320232 · Engine Oil Distribution (Airframe Furnished)SDR UALA2013041602602Computer · faultyRIGHT WING AIR LEAK MESSAGE DISPLAYED. CFDS REPORTING ISSUE WITH RIGHT WING LOOP B. REPLACED NR 2 BMC AS PER AMM, OPS GOOD.Apr 15, 2013 · N417UA · Airbus A320232 · Pneumatic Distribution SystemSDR UALA2013041502592Fastener · missingTWO RIVETS MISSING ONE POPPED ALONG UPPER INBOARD OF NR 1 ENGINE TAILCONE. INSTALLED NEW RIVETS PER MT 78-001.Apr 15, 2013 · N413UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR UALA2013041602601Unknown · odorPACKS PRODUCE A STRONG ACIDIC SMELL IN THE DESCENT. OCCURS WHEN THRUST IS REDUCED. REPEAT ITEM PERFORMED HIGH POWER ENGINE RUN WITH BOTH ENGINES, PACKS ON, NO SMELL NOTED. OK TO CONTINUE.Apr 15, 2013 · N458UA · Airbus A320232 · Air Distribution SystemSDR UALA2013041802690Duct · crackedNR 1 ENGINE PRECOOLER 'Y' DUCT IS CRACKED. REPLACED PRECOOLER 'Y' DUCT.Apr 15, 2013 · N414UA · Airbus A320232 · Pneumatic Distribution SystemSDR UALA2013041502574Controller · faultyCABIN PRESSURE RISED TO 11230 FT. SAFETY VALVE YELLOW & OPEN. OUTFLOW VALVE YELLOW & OPEN. PERFORMED STEEP DESCENT TO EQUAL OUT PRESSURE. PERFORMED TSM TASK 21-31- 00-810-809-A. PRESSURIZED ACFT TO 4.06 PSID FOR 10 MINUTES. NO LEAKS OR DEFECTS NOTED. PEApr 14, 2013 · N442UA · Airbus A320232 · Cabin Pressure ControllerSDR UALA2013041502593Latch · detachedSTRANGE PIECE OF METAL PROTRUDING FROM NR 1 ENGINE JUST BEHIND DRAIN VENT. OPENED FAN COWLING, WAS ABLE TO SEE A LOOSE LATCH MECHANISM. THAT HAS BEEN PROPERLY SECURED. CHECKED ALL THE OTHER LATCHES, FOUND SECURE. CLOSED AND LATCHED THE FAN COWL. PROPERLY Apr 14, 2013 · N408UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR UALA2013041502599Receptacle · damagedFASTENER AT FWD EDGE 197BB PANEL LOOSE. REPLACED RECEPTICLE.Apr 14, 2013 · N498UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2013041702629Connector · looseMOMENTARY ELAC 2 PITCH FAULT AFTER LIFT OFF. FAULT CLEARED AFTER A FEW MIN. SAMC TEXT: DUE TO HISTORY NEXT STEP REPLACE NR 1 AND NR 2 SEC'S PCN 482-9549 AND BOTH SDAC'S 482-9503 (P/N 350E5500201). FOUND CONNECTORS (107VC, 109VC, 111VC, 119VC, 115VC, 10VC, Apr 14, 2013 · N461UA · Airbus A320232 · Flight Control System WiringSDR UALA2013041502538Insulation · looseON THRU FLIGHT, FOUND INSULATION BLANKET LOOSE ABOVE AFT OUTFLOW VALVE. REPAIRED BLANKET IAW AMM 25-50-97. ACFT OK TO CONTINUE.Apr 12, 2013 · N442UA · Airbus A320232 · Cargo CompartmentsSDR UALA2013041502582Frame · gougedAFT CARGO BAY LEFT FRAME GOUGED AT FR 59, S36L. REPAIRED FRAME IAW SRM 53-00-12 FIG 201.Apr 12, 2013 · N466UA · Airbus A320232 · Fuselage Main, FrameSDR UALA2013041502539Seal · deterioratedFLAP TRACK SEAL OUTBOARD OF NR 1 ENGINE IS DETERORIATED. REPLACED FLAP TRACK SEAL.Apr 12, 2013 · N490UA · Airbus A320232 · Trailing Edge FlapsSDR UALA2013041502536Manifold · leakingMLG LEFT BRAKE SERVO VALVE MANIFOLD LEAKING AT HOUSING CASTING WHEN PRESSURIZED AND BRAKES APPLIED. REMOVED AND REPLACED THE LEFT NORMAL BRAKE SERVO VALVE MANIFOLD ASSY. OPERATIONAL TESTS PERFORMED NO DEFECTS NOTED REF AMM 32-42-16-400-001-A.Apr 12, 2013 · N467UA · Airbus A320232 · Landing Gear Brake SystemSDR UALA2013041502558Line · leakingDURING WALKAROUND FOUND FLUID LEAKING FROM LEFT WHEEL WELL. REPLACED LEFT GEAR BRAKE LINE ABOVE GEAR.Apr 12, 2013 · N435UA · Airbus A320232 · Fuel Indicating SystemSDR UALA2013041202517Slide · unserviceableLEFT OVERWING SLIDE DOOR HAS LOCK PINS PAINTED. REPLACED SLIDE PER MM 25-62-42 ON WU Y3409H.Apr 12, 2013 · N495UA · Airbus A320232 · Escape SlideSDR UALA2013041502556Warning System · activatedNR 1 FUEL TEMP THERMOCOUPLE TO BE CHANGED AS PRECAUTIONARY DUE TO EICAS MESSAGE. REPLACED NR 1 FUEL TEMP THERMOCOUPLE. LEAK AND OPS CHECK GOOD.Apr 12, 2013 · N453UA · Airbus A320232 · Engine Fuel Indicating SystemSDR UALA2013041502540Acoustic Panel · delaminatedCREW REPORT: A PREVIOUS PATCH OF THE ACOUSTIC PANEL ON THE NR 2 ENGINE APPEARS TO BE DELAMINATED. SAMC TEXT: FBO REPORTS 2 AREAS OF PREVIOUS ATTRITION LINER REPAIR IS SEPARATING. ONE AREA IS APPROX 2 INCH IN DIAMETER AND THE OTHER IS 1 INCH IN DIAMETER. OKApr 12, 2013 · N456UA · Airbus A320232 · Turbine Engine Air Inlet SectionSDR UALA2013041502537Floor Panel · delaminatedFWD CARGO COMPT FLOOR PANEL 131AF DELAMINATED NEAR AFT RIGHT CORNER. REMOVED FLOOR PANEL 131AF INSTALLED SERVICEABLE FLOOR PANEL PER.AMM 53-22-14-400-001-A CONTINUTE FROM PG 3 OF 5 PAR.B7. ACCOMPLISHED FINAL INSTALLATION OF FLOOR PANEL PER MM.Apr 11, 2013 · N401UA · Airbus A320232 · Fuselage Floor PanelSDR UALA2013041202505Fan · failedAVONICS SYSTEM FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED VENT BLOWER FAN.Apr 11, 2013 · N411UA · Airbus A320232 · Air Distribution FanSDR UALA2013041702630Computer · odorAVIONIC VENT ECAM WENT TO OVERRIDE, AN ODOR ELECTRICAL BURNING FROM VENT. REPLACED AEVC COMPUTER IAW AMM 21-26-34-401, CHECKED GOOD.Apr 11, 2013 · N411UA · Airbus A320232 · Navigation SystemSDR UALA2013041102458Switch · brokenF/O OXYGEN TEST SWITCH BROKEN. ADJUSTED AND SECURED SWITCH, OPS CHECKED OKAY.Apr 11, 2013 · N451UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2013041202503Unknown · malfunctionedFWD CABIN TEMP CONTROL ALMOST IMPOSSIBLE TO CONTROL. CONSTANT COMPLAINTS. SAMC TEXT: NO HELP WITH HOT AIR SWITCH TURNED OFF. BARELY MOVE CONTROLLERS WITH HOT AIR OFF AND STILL WAY UP AND DOWN AFTER PERIOD OF TIME. PEOPLE ARE REALLY COMPLAINING. OUTPUT NOApr 11, 2013 · N449UA · Airbus A320232 · Cabin Temperature Control SystemSDR UALA2013041102456Connector · unsecureLAVATORY TOILET BOWL FLUSH SYSTEM INOPERATIVE AT FWD CAB LT LAV. SECURED LOOSE CONNECTOR AT FCU. OPERATIONAL CHECK NORMAL.Apr 10, 2013 · N419UA · Airbus A320232 · Water/Waste System WiringSDR UALA2013041202499Line · leakingODOR IN ACFT AFTER APU AUTO SHUTDOWN. ACCOMPLISHED TSM & FOUND OIL LINE FROM OIL COOLER LEAKING. REPLACED LINE.Apr 10, 2013 · N433UA · Airbus A320232 · APU Oil SystemSDR UALA2013041202504Rod · defectiveWASTE HOLDING TANK VALVE HANDLE WILL NOT MOVE THE DUMP VALVE. ROD ASSY PARTS.Apr 10, 2013 · N426UA · Airbus A320232 · Waste Disposal SystemSDR UALA2013041102457Post · wornWHILE ACCOMPLISHING CH5544, FOUND COCKPIT DOOR UPPER HINGE PIN WORN IN UPPER MOUNT BLOCK. ALLOWING DOOR PLAY CAUSING DOOR TO DRAG ON FLOOR INTERMITTENTLY. REPLACED UPPER DOOR POST.Apr 10, 2013 · N446UA · Airbus A320232 · Fuselage, Door HingeSDR UALA2013041002414Acoustic Panel · damagedACOUSTICAL PNL ON INLETOF ENG 2 MISSING A CHUNK AT THE 6 O'CLOCK POSITION. FAN CASE ATTRITION LINER HAS MISSING MATERIAL AT 6 O'CLOCK POSITION TOP LAYER MEASURING 2"X 1.750" NEEDS TO BE REPAIRED WITHIN 20 CYCLES. RPR- :REPAIRED ATTRITION LINER AT 6 O'CLOCK PApr 10, 2013 · N419UA · Airbus A320232 · Turbine Engine Air Inlet SectionSDR UALA2013041102455Computer · faultyELAC 2 PITCH FAULT DISPLAYED. REPEAT HIT. ACFT REPORTING ISSUE WITH ELAC 2 OR INPUT OF L PEDAL XDCR UNIT. OPBLM -CHECKED WIRING FROM ELAC 2 TO 25CE1 AND 25CE2, MEGGED WIRING NO SHORTS NOTED. REPLACED CO. "B" ON 25CE1. NOT ABLE TO DUPLICATE FAILURE WITH HYDApr 10, 2013 · N461UA · Airbus A320232 · Elevator Control SystemSDR UALA2013041002415Sdac · malfunctionedBCL 1 FAULT. NR 2 SDAC REPLACED IAW MM 31-55-34 AND 31-32-00. SYSTEM OPS OK. CHECKED WIRING PER TSM 24-30-00-810-807-A AND 24-38-00-810-807-A. NO FAULTS FOUND.Apr 9, 2013 · N408UA · Airbus A320232 · Central WarningSDR UALA2013040902366Windshield · defective1ST OFFICER'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS. CREW COMMENTS: SMALL CREASE IN F/O WINDSHIELD IN DIRECT FIELD OF VISION THAT CAUSES SLIGHT DISTORTION. REMOVED AND REPLACED WINDSHIELD.Apr 9, 2013 · N463UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2013040902361Apu · malfunctionedBCL 1 FAULT, FLT DIVERTED. REPLACED APU.Apr 8, 2013 · N475UA · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR UALA2013040902364Microphone · stuckCAPTS HAND MIC PTT BUTTON INOP. STUCK MIC REMOVED AND REPLACED CAPTS HAND MIC. OPS CHECK GOOD.Apr 8, 2013 · N461UA · Airbus A320232 · Audio Integrating SystemSDR USAA2013041200020Relief Valve · failedDURING TAXI, AFTER NR 2 ENGINE SUCCESSFULLY STARTED AND STABILIZED. DURING FLIGHT CONTROL CHECK, NR 2 ENGINE FAILED. ACCOMPLISH TSM 75-24-00-810-802-B DUE TO AIRMAN FAULT OF ACC ACT, HC, EEC2 ON ENG 2. REPLACE PARTS IAW TSM. REPLACED NR 2 ENGINE PREVIOUSLApr 8, 2013 · N659AW · Airbus A320232 · Fuel Controlling SystemSDR UALA2013040902362O-Ring · damagedFOUND FUEL LEAKING AT LOW PRESSURE FUEL SWITCH ON APU. REPLACED O-RING SEALS AT APU LOW PRESSURE SWITCH. ACCOMPLISHED APU RUN, NO LEAKS NOTED.Apr 8, 2013 · N458UA · Airbus A320232 · Aircraft Fuel Distribution SystemSDR UALA2013040802300Armrest · looseARMREST-CONSOLE LOOSE (ROCKS) AT 26D. ARMREST LOOSE. REPAIRED USING ECRA 2521-02520. NEEDS ARMREST, PCN 005-5512. REMOVED AND REPLACED ARMREST ON SEAT 26D. OPS CHECKS GOOD. OK TO CONTINUE.Apr 7, 2013 · N458UA · Airbus A320232 · Passenger Compartment EquipmentSDR UALA2013040902363Control Unit · faultyH2O POURING OUT FWD LAV INTO COCKPIT. REMOVED AND REPLACED FLUSH CONTROL UNIT REF AMM 38-31-12. REMOVED AND REPLACED RINSE VALVE FWD LAV 'A'. OPS AND LEAKS CHECK GOOD. NO FURTHER CLEAN UP IS REQUIRED.Apr 7, 2013 · N421UA · Airbus A320232 · Waste Disposal SystemSDR UALA2013040802299Limiter · malfunctionedBCL 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - ELEC REMOVED AND REPLACED BCL1 PER AMM, OPS CHECK PASS PER AMM. NO FAULTS NOTED.Apr 6, 2013 · N465UA · Airbus A320232 · Battery/Charger SystemSDR UALA2013040802331Seal · missingPERSISTENT LOW VIBRATION IN ALL PHASES OF FLT FELT & HEARD IN COCKPIT & MID-CABIN. DURING INSPECTION, FOUND TWO AREAS OF SEAL AND SEALANT MISSING FROM PANELS 191AT AND 191BT. REPLACED SEAL IAW MM.Apr 6, 2013 · N429UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2013040802332Battery · faultedELEC BCL 1 FAULT DISPLAYED ON UPPER ECAM. REPLACED NR 1 BATTERY IAW AMM 24-38-51. FAULT CLEARED.Apr 6, 2013 · N408UA · Airbus A320232 · Battery/Charger SystemSDR UALA2013040802350Unknown · unknownEMERGENCY EXIT LIGHTS, NO SMOKING SIGN, CABIN LIGHTS ON BRIGHT AND SEAT BELT LIGHT ALL STUCK ON. PERFORMED CIDS RESET AND OP CHECK THRU CFDS PER AMM 23-73-00-740-005-A. OP CHECKED NS FSB LIGHTS PER AMM 23-73-63-400-002-A, ALSO OP CHECKED EMERGENCY LIGHTS PERApr 6, 2013 · N469UA · Airbus A320232 · Emergency LightingSDR UALA2013040802301Valve · failedCABIN TEMP, ALL ZONES EXTREMELY ERRATIC AND IMPOSSIBLE TO CONTROL. ROAMS TO EXTREME. REPLACED HOT AIR PRESSURE REGULATING VALVE. OPS CHECKED GOOD.Apr 6, 2013 · N430UA · Airbus A320232 · Cabin Temperature Control SystemSDR UALA2013040802330Warning System · false activationGEN 2 FAULT DISPLAYED ON UPPER ECAM. INSTALLED GCU, GOT GOOD VOLTS AND FREQS, BUT STILL WOULD NOT COME ONLINE. IDG OIL LEVEL GOOD. RE-INSTALLED OLD GCU AND DEFERRED REF MEL 2420D. INF- :PRIOR TO CLEARING THIS DF ITEM AND RESTORING IDG TO SVC, PYLON MOUNTEDApr 6, 2013 · N438UA · Airbus A320232 · AC Indicating SystemSDR UALA2013040802297Control Valve · malfunctionedREPLACE ELEVATOR ACTUATOR 34CE1. SHOULD READ ELEVATOR SERVO VALVE. REPLACED LEFT GREEN SERVO CONTROL VALVE. (PCN 644-0040)Apr 5, 2013 · N454UA · Airbus A320232 · Elevator Control SystemSDR UALA2013040802298Contactor · faultyREFERENCE LOG 3 ON 5 APR, BCL 1 FAULT REPLACE BCL 1 AS PRECAUTIONARY. REMOVED AND REPLACED BCL NR 1 PER AMM 24-38-3-P401. PERFORMED TEST PER AMM 24-38-00-710-00 1-A. GOT FAULT IN 6PB1 CIRCUIT. LOG 3 REMAINS OPEN FOR T/S. REMOVED AND REPLACED NR 1 BATTERY Apr 5, 2013 · N465UA · Airbus A320232 · Battery/Charger SystemSDR UALA2013040802304Handle · faultyLANDING GEAR NR 1 LGCIU FAULT ECAM ON GEAR DOWN ON APPROACH. REMOVED AND REPLACED LANDING GEAR HANDLE PER AMM, OPS NORMAL.Apr 5, 2013 · N409UA · Airbus A320232 · Landing Gear SelectorSDR UALA2013040802303Fastener · missingNUMEROUS LOOSE AND MISSING FASTENERS ON SIDES AND UNDERSIDE OF AIRCRAFT. SECURED OR REPLACED FASTENERS.Apr 5, 2013 · N425UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2013040802351Control Panel · faultyF/O VHF 2 DOES NOT DESELECT CONTINUE TO HEAR VHF2 WHEN DESELECTED AND VOL. SWAPPED F/O ACP DASH 467 WITH NR 3 ACP DASH 483. CONFIRMED F/O ACP BLEED THRU. PLACED OBSERVER SEAT ON PLACARD. T-S CONFIRMED NEEDS PANEL 582-9012 PART NSU AT TPA AC STILL CONFIGUREApr 5, 2013 · N437UA · Airbus A320232 · VHF Communications SystemSDR UALA2013040802302Switch · stickingF/O CONTROL STICK MICROPHONE SWITCH STICKS IN TRANSMIT POSITION. NEED NEW MIC SWITCH DEACTIVATED PER AMM. F/O SIDE STICK PUSH TO TALK SWITCH. REPLACE THE SIDE STICK GRIP FOR PTT SWITCH FAILURES. REPLACE THE SIDE STICK GRIP FOR PTT SWITCH FAILURES.Apr 5, 2013 · N457UA · Airbus A320232 · Audio Integrating SystemSDR UALA2013040902365Oxygen Mask · failedCAPTAIN'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). SWAPPED CAPTS OXYGEN MASK SERIAL 94410 WITH SEC OBS SEC OBS MASK SER 71814 NOW IN CAPT POS PER TASK 35-12-41 PAGE BLOCK 0401. OPS CHECK TASK 23-51-00-710-004 -A AND TASK 35-12-41-710-001-A. OPS CHECK Apr 5, 2013 · N463UA · Airbus A320232 · Crew Oxygen System
Back to IAE V2527-A5