IAE V2527-A5

Service difficulty reports · 8,011

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 UALA2011022100883Wire · brokenR-2 DOOR EMERGENCY EXIT LIGHT IDENTIFIER AT FLOOR LEVEL IS INOP. FOUND LIGHT ASSY WITH BROKEN WIRE. R & R LIGHT ASSY. OPS CHECKED LIGHT ASSY. ALL CHECKED GOOD.Feb 19, 2011 · N442UA · Airbus A320232 · Light System WiringSDR UALA2011022100896Wire Harness · damagedTURNING OFF RUNWAY. STOPPED ACFT, CYCLED NWS SWITCH AND GOT IT BACK. REPLACED UPPER HARNESS 2M IAW MM. ACCOMPLISHED STEERING CHECK BY TAXIING ACFT. TAXI LIGHT, RUNWAY TURN OFF LIGHT CHECK OK, ALSO LANDING GEAR BITE OK AND BSCU OK.Feb 17, 2011 · N456UA · Airbus A320232 · Landing Gear System WiringSDR UALA2011021700824Pump · faultyRAT FAILED. SPINS BUT FAILS TO INDICATE FULL SPEED. SUSPECT INTERNAL SPEED SENSOR, NEED RAT ASSY. REPLACED RAT PUMP AND RAT HYD MODULE, BOTH PARTS, NO HELP.Feb 17, 2011 · N415UA · Airbus A320232 · Hydraulic System, AuxiliarySDR UALA2011021600800Actuator · failedTRIMMABLE HORIZ STABILIZER ACTUATOR FAILED JAMMING TEST. START REMOVING THS ACTUATOR. ACCOMPLISHED UP TO ITEM NR 5. COMPLETED INSTALLATION OF THS ACTUATOR. INSPECTED THE INSTALLATION OPERATION, SAFETY AND SECURITY OF THE THS ASSY.Feb 14, 2011 · N408UA · Airbus A320232 · Stabilizer Control SystemSDR UALA2011021500792Pump · faultyIAW INBD CREW ZERO FUEL IN CTR TANK UPON DEPARTURE. ON ARRIVAL AT DESTINATION, FOUND 480 LBS OF FUEL IN THE CTR TANK. REMOVED JET ADAPTOR ASSY FROM SCAVENGE JET PUMP 66QM AND CHECKED FOR BLOCKAGE, FOUND ASSY AND JET PUMP CLEAR OF ANY BLOCKAGE. REPLACED FQIC Feb 14, 2011 · N416UA · Airbus A320232 · Aircraft Fuel Distribution SystemSDR UALA2011021500796Rudder · out of rigVIBRATION-NOISE ENCOUNTERED IN FLIGHT. CREW COMMENTS: NOTICEABLE MINOR LATERAL SHAKE FELT THROUGHOUT ACFT IN CLIMB AND CRUISE. VIB STOPPED IMMEDIATELY. ACCOMPLISHED RUDDER NEUTRAL TRIANGLE INSTALLATION, ACCOMPLISHED RUDDER NEUTRAL RIGS IAW MM, OPS CHECKED GOOFeb 14, 2011 · N465UA · Airbus A320232 · Rudder Control SystemSDR UALA2011021400783Smoke Detector · faultySMOKE LAV DET FAULT RESET, NO HELP. REPLACED FWD LAV SMOKE DETECTOR. CHECKED GOOD.Feb 13, 2011 · N469UA · Airbus A320232 · Smoke DetectionSDR UALA2011021400766Unknown · vibrationLATERAL MOD VIBRATION FELT IN AFT GALLEY DURING CLIMB. PERFORMED RUDDER, AND ELEVATOR T/E FREE PLAY CHECK DUE TO VIBE REPORTING FORM DATA. 2 LEGS IN A ROW HAVE AFT FUSELAGE VIBE. PERFORMED ELEVATOR SERVO CONTROLS AND HINGE BEARING CONDITION CHECK AND RUDDEFeb 12, 2011 · N451UA · Airbus A320232 · Flight Control SystemSDR UALA2011021400776Container · delaminatedCREW REPORT: OXY PANEL ROW 27 ABC LOOSE. -O2 CONTAINER BOX IS DELAMINATING, SEPARATING FWD OTBD CORNER LOWER SURFACE. BOX IS SECURE IN OVERHEAD. AS PRECAUTION, APPLIED TAPE OVER CORNER, INOP SEATS 27ABC. WILL NEED NEW CONTAINER. SEATS PLACARDED INOP, REPLACED Feb 12, 2011 · N446UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2011021100730Packing · leakingFUEL LEAK L-1 MAGNETIC FUEL LEVEL IND. FOUND FUEL LEAKING FROM LT WING OTBD BOOST PUMP HSG 26QA. HEAVY LEAK MEASURES 6-7 INCHES. MAG LEVEL IND HAS NO LEAKS. REPLACED PACKINGS ON LT OTBD BOOST PUMP AND SLIDE VALVE. REPLACED LEAKING WATER DRAIN OUTER VALVE,Feb 11, 2011 · N426UA · Airbus A320232 · Fuel Boost PumpSDR UALA2011021100739Girt Bar · fodUNABLE TO ARM DOOR 2R. FOUND SOME DEBRIS AROUND DOOR SILL AND GIRT BAR. CLEANED AREA, OPS CK OK IAW MM.Feb 11, 2011 · N425UA · Airbus A320232 · Emergency EquipmentSDR UALA2011021000694Connector · disconnectedEMERGENCY EXIT LIGHTS INOP SEAT ROW 24, 25 AND 26. FOUND CONNECTOR OFF AT SIDEWALL, REINSTALLED AND LIGHTS CHECKED GOOD.Feb 10, 2011 · N424UA · Airbus A320232 · Light System WiringSDR UALA2011021000695Sleeve · delaminatedNR 2 ENG INBD THRUST REVERSER SLEEVE HAS WIRE MESH MISSING AND DELAMINATED. NR 2 ENG INBD REV SLEEVE, R & R SLEEVE.Feb 10, 2011 · N417UA · Airbus A320232 · Engine Thrust ReverserSDR UALA2011021100727Amu · faultyBURNING SMELL ON TAXIOUT IN FWD GALLEY AREA. SUSPECT VIDEO SYS. HOT ITEM IS THE AMU. CONNECTOR PLUG REMOVED. "ACCESS MEMORY UNIT" CONNECTOR PLUG REMOVED, SECURED WITH TAPE TO PREVENT HAZARD. REPLACED VIDEO PROJECTION SYSTEM ACCESS MEMORY UNIT. OPS NORMAL.Feb 10, 2011 · N433UA · Airbus A320232 · Entertainment SystemSDR UALA2011021100714Unknown · odorCHEMICAL ODOR IN AFT GALLEY DURING TAKEOFF. AFTER LAV SVC. ODOR CLEARED, SPRAYED AIR FRESHENER TO AFT CABIN.Feb 10, 2011 · N471UA · Airbus A320232 · Air Distribution SystemSDR UALA2011020800671Solenoid · faultedREGULATOR LOW PRESSURE MESSAGE DISPLAYED ON LOWER ECAM WHEN MASKS ARE TESTED. REPLACED PRESSURE SWITCH 4WV IAW MM, NO HELP. REPLACED OXYGEN PRESSURE REGULATOR 4HT IAW MM (TWICE). NO HELP. PILOT REPORTED "ALONG WITH MESSAGE, WE DO NOT GET ENOUGH OXYGEN FROMFeb 8, 2011 · N427UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2011020800673Transducer · faultyREPETITIVE ELAC 2 FAULTS. DUE TO REPETATIVE ELAC 2 FAULTS-FAULTING THE ELAC2 OR INPUT OF F/O ROLL CTL SSTU: REPLACE THE F/O ROLL CTL SSTU (4CE2). ELAC 2 PREVIOUSLY REPLACED TWICE. REPLACED ROLL TRANSDUCER IAW MM. OPS NORMAL.Feb 8, 2011 · N493UA · Airbus A320232 · Flight Control SystemSDR UALA2011020700656Control Unit · burnedRAMP REPORTED SMOKE COMING FROM GROUND POWER CABLE HOOKED TO ACFT. FOUND RECEPTACLE PINS BURNED AND CASE MELTED. REPLACED GROUND POWER CONTROL UNIT ON OV WU N9016Y.Feb 7, 2011 · N470UA · Airbus A320232 · Electrical Power SystemSDR UALA2011021000706Skin · crackedCRACK FOUND ON RT MLG DOOR. FOUND LESS THAN 1-4 INCH LENGTH CRACK ON RT GEAR DOOR FWD OUTER SKIN. NO WATER DAMAGE FOUND AND NO DAMAGE UNDER SKIN. SPEED TAPE AREA. AREA IS UPPER TOP SKIN OF RT GEAR DOOR WHEN DOOR IS UP POSITION. RECHECK TAPE AFTER EVERY DEPFeb 7, 2011 · N419UA · Airbus A320232 · Landing Gear DoorsSDR UALA2011020800669Unknown · odorNOTICED ELECTRICAL BURNING ODOR IN CABIN. CREW REPORTED GEN 1 FAULTED SEVERAL TIMES ON TAXI OUT, NUMEROUS FAULTS REPORTED ON BUSS 1 THRU CFDS. AFTER APU PUT ON LINE, WITH ENG 2 POWERING BUSS 2, IT APPEARED GEN 2 HAD PROBLEMS REFLECTED BY A FAULT LIGHT & FLICFeb 7, 2011 · N416UA · Airbus A320232 · Air Distribution SystemSDR UALA2011020700644Unknown · odorON APPROACH, GOT HOT PLASTIC ODOR IN COCKPIT AND CABIN. EMERGENCY LIGHTS STARTED FLASHING . CAPT SHUTDOWN CABIN FANS AND GALLEY FANS, EMERGENCY LIGHTS STARTED TO FLASH ON & OFF. CHECKED DISTRIBUTION DUCTS IN MID & FWD E/E BAYS. NO ODOR DETECTED. OPS CHECK EMEFeb 6, 2011 · N480UA · Airbus A320232 · Air Distribution SystemSDR UALA2011020700664Slat System · malfunctionedECAM FLT CONTROL SLAT SYS 2 FAULT APPEARED AT FLAP RET AT 2000 FT ON CLIMBOUT. REF LOG 1 AND 2 SLAT LOCK OUT. CHECKED ALL SLAT DRIVE OVERLOAD INDICATORS LT AND RT ALL OK. ACCMP'D INSP OF SLAT WING TIP BRAKES. FOUND RT WING TIP BRAKE 0036CU VERY STIFF AND CHFeb 6, 2011 · N432UA · Airbus A320232 · Leading Edge Slat Control SystemSDR UALA2011020700627Microphone · inoperativeF/O'S OXYGEN MASK MICROPHONE IS INOPERATIVE. WHEN MASK IS STOWED WHITE TAB INDICATING MASK MICROPHONE IS HOT WILL NOT RESET. REPLACED STOWAGE BOX OP'S GOOD IAW MM.Feb 5, 2011 · N496UA · Airbus A320232 · Communications SystemSDR UALA2011020700626Electrical Box · odorELECTRICAL SMOKE SMELL DETECTED BETWEEN 17A AND B. FOUND PCU'S INOP AT ROWS 16ABC & 17ABC. ALSO NOTED ODOR. REPLACED SEB UNITS AT ROWS 15ABC, 16ABC & 17ABC. OPERATIONS NOW NORMAL.Feb 4, 2011 · N496UA · Airbus A320232 · Passenger Compartment EquipmentSDR UALA2011020300584Frame · corrodedMAJOR REPAIR. AFT PIT CORROSION AT FRAME 52A STRINGER 38R AND 39R. REO L01295 AND A-B RAS-DAHAM-4033757-2011 THIS REPAIR IS CONSIDERED MINOR WITH NO SUPPLEMENTAL INSP REQUIRED. PERMANENT REPAIR. CORROSION REMOVED IAW SRM. NDT IAW NTM, NO RELEVANT INDICATIOFeb 3, 2011 · N416UA · Airbus A320232 · Fuselage Main, FrameSDR UALA2011020400598Panel · damagedEMERGENCY LIGHT COVER AT 2L BROKEN OFF. REPLACED AFT ATTENDANT LIGHTING AND COMMAND PANEL AT 2L. ASSOCIATED PANEL FUNCTIONAL TESTED OK.Feb 3, 2011 · N480UA · Airbus A320232 · Emergency LightingSDR UALA2011020400597Latch · obstructedDURING DROP CHECK OF PASS O2 MASKS. FOUND MASKS IN AFT LAV DID NOT DEPLOY. FOUND AND CLEARED OBSTRUCTION IN LATCHING MECHANISM. OPS CHECKED GOOD REF MM.Feb 3, 2011 · N420UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2011020200559Fire Warning · false activationCREW REPORTED AT APPROX 1 MIN AFTER APU NORMAL SHUTDOWN, APU FIRE WARNING INDICATED, BOTTLE DISCHARGED. PERFORMED VISUAL INSP OF APU COMPARTMENT AND TAIL PIPE, NO EVIDENCE OF FIRE. PERFORMED FADEC SELF TEST AND APU TEST BOTH OK. CLASS 3 FAULT EMERGENCY STOP Feb 2, 2011 · N482UA · Airbus A320232 · Fire DetectionSDR UALA2011020200562Slide · out of positionDOOR 2R SLIDE PACK HAS FALLEN OUT OF POSITION. REPLACED SLIDE. VERIFIED ALL SAFETIES REMOVED, RII ACCOMPLISHED, CABLE ROUTING CORRECT AND TEST ACCOMPLISHED AND GOOD.Feb 2, 2011 · N407UA · Airbus A320232 · Escape SlideSDR UALA2011020200569Indicator · damagedLIGHT IN ICE PROBE FRONT WINDSHIELD POST BURNED OUT. SAMC TEXT: CREW COMPLIED WITH MEL. DEFERRED IAW SAMC. REPLACED ICING INDICATOR IAW MM, CHECKED OK.Feb 2, 2011 · N496UA · Airbus A320232 · Ice DetectionSDR UALA2011020200572Cable · lack of lubeL2 DOOR WILL NOT ARM. CHECKED EVERYTHING EXTERNAL ALL LOOKS OK. DOOR 2L LININGS REMOVED FOR LUBE OF DOOR. REINSTALLED LININGS. FOUND FLEXIBLE CONTROL CABLE TO ARMING LEVER WITH MOISTURE AT LOWER END. LUBED UPPER AND LOWER ENDS OF CABLE, OPS CHECKED NORMALFeb 2, 2011 · N438UA · Airbus A320232 · Escape SlideSDR UALA2011020200575Compressor · vibratesENG 2 COMPRESSOR VANE ON UPPER ECAM. ENGINE WAS SHUTDOWN AND RESTARTED. FAULT CLEARED BUT RETURNED WHEN THROTTLE ADVANCED TO BREAKAWAY THRUST. LAST LEG FAULT CHANNEL A & B VSV ACT-HC-EEC2 WITH FLT DATA FAULT SVA TK IN FLT PH 02. CHECKED IAW TSM. ACCOMPLISFeb 1, 2011 · N406UA · Airbus A320232 · Turbine Engine Compressor SectionSDR UALA2011013100532Wedge · damagedLT OTBD T/E FLAP, T/E HONEYCOMB WEDGE HAS 2"X 2" BY APPROX 0.125" DENT FROM BIRD-STRIKE. ACCOMPLISHED HFEC INSP OF DENT NO CRACKS FOUND AT THIS TIME REF NDT 51-10-08, PROCEDURE B.Jan 31, 2011 · N460UA · Airbus A320232 · Trailing Edge FlapsSDR UALA2011013100535Engine · leakingSTRONG HOT OIL ODOR IN ACFT. SUSPECT NR 2 ENGINE OIL LEAK. SERVICED, ONLY 17.5 QTS NOW. EFS AMT ISOLATED ENG 2 AS A SOURCE OF OIL ODOR DURING HIGH POWER RUN, WITH ENG 2 BLEED OFF NO ODOR NOTED. INOP ENG 2 BLEED AIR SUPPLY SYS IAW MEL 3611B PRIOR TO FERRY. Jan 31, 2011 · N461UA · Airbus A320232 · Turbine Engine Oil SystemSDR UALA2011020100538Battery · inoperativeF/A FLASHLIGHT AT 2L (OTBD) IS INOPERATIVE. REPLACED BATTERY FLASHES NORMAL.Jan 31, 2011 · N435UA · Airbus A320232 · Emergency EquipmentSDR UALA2011013100503Wire · shortedAPU AUTO SHUTDOWN AT GATE WITH LOW FUEL PRESSURE WARNING ON ECAM. SHORTED WIRE NEAR APU CIRCUIT BREAKER. DURING REPLACEMENT OF CB AA8, POWER WAS APPLIED TO ACFT & ARCING OCCURRED. WIRE HAS INSULATION DAMAGE TO SEVERAL AREAS. DURING WIRE INSPECTION FOUND WIJan 30, 2011 · N458UA · Airbus A320232 · APU System WiringSDR UALA2011013100517Girt Bar · obstructedDOOR 1L SLIDE WILL NOT ARM. FOUND AFT GIRT FITTING CONTACTING NEW FLOOR PLATE. FILED PLATE AT CONTACT POINT TO ALLOW FOR SMOOTH OPERATION. OPS CHECKS OK. ON ACCOUNT OF DOOR 1L DOOR SLIDE ARMING PROBLEMS, ARMING SAFETY PIN INSTALLED.Jan 29, 2011 · N413UA · Airbus A320232 · Emergency EquipmentSDR UALA2011013100527Pump · leakingLEFT WING FUEL TANK PUMP HOUSING AREA IS WET WITH FUEL WIPED DOWN AREA AND 15 MINS LATER AREA IS WET AGAIN. FUEL STAINS APPEAR TO BE STREAMING AFT ALONG WIRE COVER AFT DURING FLIGHT. FOUND FUEL PUMP 25QA LEAKING. BEGAN REMOVAL IAW MM. CIRCUIT BREAKERS HAVE Jan 28, 2011 · N404UA · Airbus A320232 · Engine Fuel PumpSDR UALA2011012800467Connector · crackedLANDING GEAR REV 2, FAULT, RTFL. FOUND CONNECTOR FOR PROX SENSOR 23GA CRACKED. REPLACED CONNECTOR, REF AMM. ACCOMPLISHED LGCIU NR 2 BITE. TEST OKAY.Jan 28, 2011 · N465UA · Airbus A320232 · Landing Gear System WiringSDR UALA2011012800471Slide · failedDOOR 1L DOOR SLIDE DEPLOYED BUT DID NOT INFLATE. SLIDE PACK IS RESTING ON THE AIR STAIR TOP STEP. DISCONNECT THE DOOR 1L SLIDE IAW AMM. AFTER SLIDE IS REMOVED FROM THE DOOR LEAVE THE SLIDE IN THE FWD GALLEY AREA UNTIL THE SLIDE CAN BE PINNED AND SAFTIED. REJan 27, 2011 · N489UA · Airbus A320232 · Escape SlideSDR UALA2011013100494Mask · brokenF/A O2 DEMO MASK BROKEN. REPLACED MASK.Jan 27, 2011 · N475UA · Airbus A320232 · Emergency EquipmentSDR UALA2011012600440Stringer · corrodedCORROSION ON STR 43L BETWEEN FRAMES 54 AND 60. MAJOR REPAIR ACCOMPLISHED: INSTALLED STRINGER REPAIR IAW SRM ON NR M6607L.Jan 26, 2011 · N416UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2011012600441Stringer · corrodedCORROSION ON STR 43R BETWEEN FRAMES 57 & 58. MAJOR REPAIR ACCOMPLISHED: REPLACED FACTORY STR SECTION REF SRM FIG 201 ON NR M6636L.Jan 26, 2011 · N416UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2011012600442Stringer · corrodedCORROSION ON STRINGER 42L BETWEEN FRAMES 56 & 58. MAJOR REPAIR ACCOMPLISHED: INSTALLED SPLICED STRINGER REPAIR IAW SRM ON NR M6637L.Jan 26, 2011 · N416UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2011012700451Frame · corrodedCORROSION ON S43L AFT FRAME 31 IN FWD PIT. EVALUATED CORROSION AND FOUND IT OUT OF LIMITS OF SRM. REMOVED DAMAGED SECTION & FAB AND INSTALLED NEW SECTION & REPAIR SPLICES FROM FR 30 TO FR 31. THIS REPAIR VALID UNTIL 31DEC 2013 ONLY.Jan 26, 2011 · N416UA · Airbus A320232 · Fuselage Main, FrameSDR UALA2011012600447Gauge · obstructedF/A ADVISES SLIDE PACK PRESSURE GAUGE DOOR 1R OBSCURED BY INSPECTION DATE STICKER. REPLACED DOOR 1R SLIDE ASSY IAW MM. INSPECTION DATE TAG INCORRECTLY PLACED BY VENDOR.Jan 26, 2011 · N470UA · Airbus A320232 · Escape SlideSDR UALA2011012400370Connector · arcedC/B POPPED, FLIGHT DIVERTED. COFFEEMAKER C/B POPPED. INSPECTED AFT GALLEY POWER PANEL 9002ML4 FOR EVIDENCE OF BURNING, ARCING, AT CONNECTORS AND WITHIN PANEL ITSELF. NO DEFECTS NOTED. REPLACED TR UNITS 9010ML3 AND AND 9021ML4 IAW WD, OPS NORMAL.Jan 24, 2011 · N489UA · Airbus A320232 · Electrical Power System WiringSDR UALA2011012400382Proximity Sensor · false indicationLANDING GEAR NOT UPLOCKED ON ECAM. ACCOMPLISHED TSM 32-31-00- 810-865 UP TO TASK 5. NO OBVIOUS DEFECTS FOUND. CHECKED RESISTANCE ON SENSORS 12GA, 13GA, 30GA AND 31GA. ALL READ 10.6 OHMS AT APPROX 10 DEGREES F. SLAVED IN NEW LGCIU 1 AND LGCIU 2, NO HELP. Jan 24, 2011 · N425UA · Airbus A320232 · Landing Gear Position and WarningSDR UALA2011012400391Stringer · dentedFOUND STRINGER 41 DENTED BETWEEN FRAME 61 AND 62 AT SKIN LAP. NO CRACK NOTED. ACCOMPLISHED DAMAGE AREA INSPECTION IAW SRM. NO CRACK NOTED. FOUND STR 40 DAMAGE BETWEEN FRAME 61 AND 62. REMOVED DAMAGE. NO DAMAGE TO STRINGERS FOUND AFTER SKIN REMOVAL. HFEC NJan 24, 2011 · N414UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2011012400401Wire · damagedFOUND BURNED & BROKEN WIRES 2825-5805 & 2825-5813 IN RT MAIN WHEEL WELL. REPLACED WIRE W2825-5805-20 FROM 10QU-A TO 6793VN. TERMINATED & SECURED WIRE W2825-5813-22 FROM 10QU-A UP TO PRESSURE SEAL 7502VP IN RT WW CEILING REF WD28-25-04 AND HOOK-UP LIST PG 141Jan 24, 2011 · N483UA · Airbus A320232 · Electrical Power System Wiring
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