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 2007UALA00577Wire · shortedFOUND SHORTED WIRE BETWEEN SEC AND ACTUATOR. [SUP 05-16-07] FLT RTBL WITH EFCS TEST 1 FAILURE MESSAGE. EFCS FAULTED SEC 2. INITIALLY SWAPPED SEC 2 WITH SEC 3 TO DETERMINE IF FAULT WAS WITH THE SEC UNIT ITSELF. POST SWAP OPS CHECK FAILED, SO STARTED TO PERFORFeb 25, 2007 · N401UA · Airbus A320232 · Electrical Power System WiringSDR 2007UALA00543Light · faultyFOUND DOOR EMERGENCY EXIT LIGHT ON AND WILL NOT EXTINGUISH. [5-1-07] REMOVED AND RESEATED CAM AND ACPD CFDS TEST. LIGHTS ARE EXTINGUISHED & TEST PASSED.Feb 19, 2007 · N449UA · Airbus A320232 · Emergency LightingSDR 2007UALA00489Actuator · malfunctionedRTFL DUE TO NR 2 ENGINE SURGE AT TAKEOFF. ENGINE WAS SHUTDOWN. [SUP 05-08-07] VSVA SETTING TRACK CHECK FAULTS ON BOTH CHANNELS SUGGESTING OPERATIONAL PROBLEMS. UNIT HAS BEEN SENT TO OSV FOR INVESTIGATION. UNIT HAS 31 HOURS SINCE SHOP VISIT AND REPAIR.Feb 17, 2007 · N457UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2007UALA00491Proximity Sensor · out of adjustON TAKEOFF, GEAR DID NOT RETRACT. RED AND GREEN LIGHTS STAYED ON. RECYCLED GEAR & GEAR CAME UP. FAULT TRACED TO OUT OF ADJUSTMENT NOSE LANDING GEAR PROXIMITY SENSOR. PROXIMITY SENSOR BRACKETS, TARGETS AND SPACERS WERE REMOVED FOR INSPECTION AND THEN REINSTFeb 17, 2007 · N426UA · Airbus A320232 · Landing Gear Position and WarningSDR 2007UALA00513Engine · inoperativeNR 1 ENGINE FAILED TO START. VALVE INDICATES OPEN. REPLACED STARTER DUE TO FAILURE. UPON FURTHER TEARDOWN, FOUND THAT THE TURBINE WHEEL BEARING HAD FAILED CAUSING DAMAGE TO THE INLET HOUSING, CAGE, TURBINE WHEEL AND CLUSTER GEARS. THE START VALVE WAS ALSO RFeb 17, 2007 · N460UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2007UALA00488Hydraulic System · leakingRTFL UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. A/C WAS TOWED TO GATE. FLUID LOSS DUE TO FAULTY RH MLG DOOR BYPASS VALVE. REPLACED THE DOOR BYPASS VALVE AND NR 1 ENGINE DRIVEN HYDRAULIC PUMP AS A PRECAUTIONARY MEASURE. CHECKED HYDRAULIC SYSTEM Feb 16, 2007 · N442UA · Airbus A320232 · Hydraulic System, MainSDR 2007UALA00497Connector · brokenCABIN EEL CONNECTORS HAVE BROKEN BACKSHELLS ON FLOOR BY SIDEWALL AT SEAT ROWS 6L, 7L, 15L, 18L AND 26L. [5-1-07] BACKSHELLS REPLACED.Feb 16, 2007 · N436UA · Airbus A320232 · Emergency LightingSDR 2007UALA00459Pin · bindsFWD RIGHT MED EMERGENCY EVACUATION SLIDE INFLATION BOTTLE SAFETY PIN INSERTION WAS EXTREMELY HARD. [SUP 05-16-07] FWD RT EMERGENCY SLIDE WAS REPLACED. IT WAS LATER DETERMINED THAT THE INFLATION BOTTLE REGULATOR VALVE WAS OUT OF POSITION, WHICH WAS CAUSING THFeb 15, 2007 · N436UA · Airbus A320232 · Escape SlideSDR 2007UALA00469Shear Tie · corrodedFWD CARGO PIT CORROSION AT FRAME 32 SHEAR TIES BETWEEN STR 43 & 44 LT, 41 & 42 LT, 40 & 41 LT, 42 & 43 RT, 41 & 42 RT, 40 & 41 RT AND 39 & 40 RT. REPAIR ACCOMPLISHED: REPLACED SHEAR TIES.Feb 15, 2007 · N430UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR 2007UALA00470Stringer · corrodedSTRINGER 41 RT HAS 3 EACH AREAS OF CORROSION AT FRAME 29, UNDER FRAME 32 AND BETWEEN FRAMES 33 & 34. MAJOR REPAIR ACCOMPLISHED: INSTALLED 3 EACH SPLICE REPAIRS.Feb 15, 2007 · N430UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2007UALA00471Stringer · corrodedFWD PIT STRINGER 39 LT HAS CORROSION 3 INCHES FWD OF FR 33. MAJOR REPAIR ACCOMPLISHED: INSTALLED SPLICE REPAIR.Feb 15, 2007 · N430UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2007UALA00451Shear Tie · corrodedFWD CARGO PIT CORROSION AT FRAME 27 SHEAR TIES BETWEEN STR 43 & 44 LT, 42 & 43 RT, 41 & 42 RT AND FRAME 24 SHEAR TIE BETWEEN STR 42 & 43 RT. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIES.Feb 14, 2007 · N430UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR 2007UALA00452Shear Tie · corrodedFWD CARGO PIT CORROSION AT FRAME 29 SHEAR TIES AT STR 43 & 44 LT, 41 & 42 LT, 40 & 41 LT AND 41 & 42 RT. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIES.Feb 14, 2007 · N430UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR 2007UALA00453Shear Tie · corrodedFWD CARGO PIT CORROSION AT FRAME 28 SHEAR TIES BETWEEN STR 43 & 44 LT, 42 & 43 LT, 41 & 42 RT, 42 & 43 RT AND 43 & 44 RT. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIES.Feb 14, 2007 · N430UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR 2007UALA00454Shear Tie · corrodedFWD CARGO PIT CORROSION AT FRAME 31 SHEAR TIES BETWEEN STR 43 & 44 LT, 41 & 42 LT, 40 & 41 LT, 42 & 43 RT, 41 & 42 RT, 40 & 41 RT, 39 & 40 RT. REPAIR ACCOMPLISHED: REPLACED SHEAR TIES.Feb 14, 2007 · N430UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR 2007UALA00455Shear Tie · corrodedFWD CARGO PIT CORROSION AT FRAME 33 SHEAR TIES BETWEEN STR 43 & 44 LT, 41 & 42 LT, 40 & 41 LT, 41 & 42 RT AND 40 & 41 RT. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIES.Feb 14, 2007 · N430UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR 2007UALA00456Attach Angle · crackedKEEL BEAM LWR LEFT WEB UPPER ATTACH ANGLE IS CRACKED JUST FWD OF FR 47. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE.Feb 14, 2007 · N430UA · Airbus A320232 · Fuselage Main, KeelSDR 2007UALA00465Hose · kinkedRIGHT OVERWING SLIDE INFLATION HOSE KINKED NEAR REGULATOR END. [SUP 05-16-07] REPLACED OVERWING SLIDE INFLATION BOTTLE. INSTALLATION ERROR FROM PREVIOUS REPLACEMENT.Feb 14, 2007 · N436UA · Airbus A320232 · Escape SlideSDR 2007UALA00468Smoke Warning · activatedWHILE STARTING NR 1 ENGINE GOT SMOKE AFT CARGO SMOKE ECAM. DISCHARGED FWD AND AFT BOTTLES. MOMENTARILY GOT AN AFT SQUIB FAULT AND AFT BOTTLE DISCHARGE LIGHT NEVER ILLUMINATED. INSPECTED CARGO COMPARTMENTS AND DID NOT FIND ANY DEFECTS WITH SMOKE DETECTION SFeb 14, 2007 · N423UA · Airbus A320232 · Smoke DetectionSDR 2007UALA00436Elevator · damagedLEFT AND RIGHT ELEVATORS WERE FOUND TO HAVE SUSPECTED AREAS OF WATER INGRESSION. [SUP 05-16-07] A THERMOGRAPHIC INSPECTION FOUND 3 AREAS ON UPPER SURFACE AND 1 AREA ON LOWER SURFACE OF LEFT ELEVATOR WITH SUSPECTED WATER INGRESSION. SIMILAR INSPECTION OF RIGHFeb 13, 2007 · N430UA · Airbus A320232 · Elevator StructureSDR 2007UALA00437Attach Angle · crackedKEEL BEAM LWR RIGHT WEB UPPER ATTACH ANGLE IS CRACKED JUST FWD OF FR 47. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE.Feb 13, 2007 · N430UA · Airbus A320232 · Fuselage Main, KeelSDR 2007UALA00438Shear Tie · corrodedFWD CARGO PIT CORROSION AT FRAME 30 SHEAR TIES BETWEEN STR 43 & 44 LT, 41 & 42 LT, 41 & 42 RT AND 40 & 41 RT. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIES.Feb 13, 2007 · N430UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR 2007UALA00442Fastener · corrodedFWD PIT STRINGER ATTACH FASTENERS ARE CORRODED FROM FRAME 29 TO 34 BETWEEN STR 38R AND 38L. REPLACED 562 CORRODED FASTENERS.Feb 13, 2007 · N430UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2007UALA00420Wire Harness · misroutedDOOR 1R MED EVACUATION SLIDE ELECTRICAL HARNESS IS INCORRECTLY ROUTED. [SUP 05-16-07] REINSTALLED ELECTRICAL HARNESS CORRECTLY. SLIDE IS ORIGINAL EQUIPMENT FROM WHEN AIRCRAFT WAS DELIVERED AND THERE IS NO EVIDENCE OF THE SLIDE EVER BEING SERVICED TO THE EXTEFeb 12, 2007 · N441UA · Airbus A320232 · Equipment/Furnishings WiringSDR 2007UALA00421Fastener · corrodedFWD PIT STRINGER ATTACH FASTENERS ARE CORRODED FROM FRAME 24A TO 29 BETWEEN STR 38R & 38L. REPLACED 1029 CORRODED RIVETS.Feb 12, 2007 · N430UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2007UALA00422A/C Pack · overheatedPACK 2 OVERHEAT DISPLAYED ON UPPER ECAM SCREEN. AIR CREW COMMENTS: FLIGHT ATTENDANT OBSERVED VERY FAINT SMOKE IN BACK AS WELL AS ODOR. [SUP 05-16-07] DETERMINED THAT AIR CYCLE MACHINE IN PACK 2 HAD SEIZED DUE TO FAILED BEARINGS.Feb 12, 2007 · N404UA · Airbus A320232 · Cabin Cooling SystemSDR 2007UALA00398Battery · faultyEMERGENCY LIGHT TEST FAULTED AFT LEFT BATTERY. REPLACED AFT LEFT BATTERY. EMERGENCY LIGHT TESTS NORMAL.Feb 12, 2007 · N418UA · Airbus A320232 · Emergency LightingSDR 2007UALA00386Warning System · activatedRTFL DUE TO A MAIN LANDING GEAR INDICATION. [SUP 05-16-07] ALL DOOR INDICATORS WERE AMBER. ALL INDICATORS GREEN AFTER SECOND ATTEMPT. CREW STATED THAT IT SEEMED THAT ALL GEAR RETRACTED BUT DOORS REMAINED OPEN SUPPLEMENTAL DATA UPDATE FAULT TRACED TO OUT OF AFeb 11, 2007 · N411UA · Airbus A320232 · Landing Gear Position and WarningSDR 2007UALA00399Charger · failedEMERGENCY LIGHTS CHARGER UNIT AT DOOR 1L HAS FAILED. REPLACED CHARGER.Feb 11, 2007 · N411UA · Airbus A320232 · Emergency LightingSDR 2007UALA00376Unknown · smokeCREW REPORTED SMOKE/SMELL IN CABIN & COCKPIT FOLLOWED BY A EXTRACT FAN FAULT. [SUP 05-08-07] VERIFIED THAT AVIONICS AIR EXTRACT FAN WAS FAULTY AND WAS REPLACED. SMOKE/ELECTRICAL SMELL DUE TO BEARING FAILURE.Feb 9, 2007 · N405UA · Airbus A320232 · Air Distribution SystemSDR 2007UALA00377Fcu · malfunctionedAUTO FLT -FCU 1 FAULT- DISPLAYED ON UPPER ECAM SCREEN. CREW COMMENTS, WITH SMOKE FROM FCU. [SUP 05-08-07] REPLACED FCU AFTER VERIFYING THAT FCU WAS FAULTY AND WAS SOURCE OF SMOKE. FURTHER FAULT TRACING DETERMINED THAT THE PSU WAS DEFECTIVE.Feb 9, 2007 · N444UA · Airbus A320232 · Flight ControllerSDR 2007UALA00434Slide · faultyFOUND AT PTP PANEL TEST LEFT INTER EXTERNAL FAULTS. [SUP 05-16-07] REPLACED THE LT OVERWING SLIDE ASSEMBLY. AT OVERHAUL, DETERMINED THAT THE PACK BOARD WAS FAULTY.Feb 9, 2007 · N404UA · Airbus A320232 · Escape SlideSDR 2007UALA00385Battery · faultyEPSU BATTERY FWD L FAULT ON CABIN EMERGENCY LIGHT TEST. REPLACED FWD LT EPSU BATTERY.Feb 9, 2007 · N418UA · Airbus A320232 · Emergency LightingSDR 2007UALA00342Angle · crackedRIGHT AFT BELLY FAIRING SUPPORT STRUCTURE ANGLE CRACKED AT ATTACH TO FUSELAGE SKIN BELOW KEEL BEAM AT FRAME 46. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGE SECTION OF ANGLE.Feb 8, 2007 · N419UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2007UALA00343Angle · crackedLEFT AFT BELLY FAIRING SUPPORT STRUCTURE ANGLE CRACKED AT ATTACH TO FUSELAGE SKIN BELOW KEELBEAM AT FRAME 46. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGE SECTION OF ANGLE.Feb 8, 2007 · N419UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2007UALA00363Compressor · stalledRTFL DUE TO NR 2 ENGINE COMPRESSOR STALL. [5-1-07] STALL OCCURRED AT TOP-OF-CLIMB AFTER TURNING-OFF THE ANTI-ICE VALVE. ALL CHECKS WERE PERFORMED PER THE AIRBUS TSM WITH NO FINDINGS. THE ENGINE PASSED POWER ASSURANCE RUN AND WAS RETURNED TO SERVICE. SUSPEFeb 8, 2007 · N482UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2007UALA00365Battery Pack · dischargedEMERGENCY LIGHTS INOP AT DOOR 1L AND 1R, SEATS ROW 1, 2 AND 3 ABC. REPLACED BATTERY PACK AT DOOR 1L.Feb 8, 2007 · N449UA · Airbus A320232 · Emergency LightingSDR 2007UALA00366Cable · faultyAFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT UP TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. REPLACED EEL CABLE (560-0809) AND STRIP (560-0857).Feb 8, 2007 · N312UA · Boeing 737322 · Light System WiringSDR 2007UALA00374Frame · crackedNR 2 INBOARD REVERSER AT 7:00 POS FRAME IS CRACKED IN HALF. AFT END OF CASCADE VANES ATTACH TO FRAME. [5-1-07] REPLACED FRAME DURING HMV. FRAME HAS HISTORY IN THE INDUSTRY OF CRACKING, SERVICE BULLETIN IAE V2500-NAC-78-0209 ADDRESSES PART OF THE ISSUE . THE Feb 8, 2007 · N431UA · Airbus A320232 · Engine Thrust ReverserSDR 2007UALA00344Lever · faultyDOOR 2R ARM LEVER WON'T GO ALL THE WAY DOWN WHEN IN THE ARMED POSITION. [SUP 05-08-07] LOOSE EMERGENCY SLIDE COVER WAS INTERFERING WITH MOTION OF DOOR LEVER. FULL MOTION RESTORED AFTER SLIDE COVER WAS SECURED.Feb 7, 2007 · N422UA · Airbus A320232 · Passenger/Crew DoorsSDR 2007UALA00352Proximity Switch · faultyDOOR 1 ARMS, BUT WILL NOT INDICATE ARMED ON COCKPIT. [SUP 05-08-07] FAULT TRACED TO OUT OF ADJUSTMENT PROXIMITY SWITCH. MORE SPECIFICALLY, A LOOSE LOCK WASHER ON THE PROXIMITY TARGET. REPLACED LOCK WASHER AND READJUSTED PROXIMITY SWITCH TO PROPER CLEARANCE.Feb 7, 2007 · N402UA · Airbus A320232 · Door Warning SystemSDR 2007UALA00353Proximity Switch · out of adjustLEFT AFT SLIDE INDICATION INOP ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY. [SUP 05-08-07] OUT OF ADJUSTMENT PROXIMITY SWITCH.Feb 7, 2007 · N427UA · Airbus A320232 · Escape SlideSDR 2007UALA00333Attach Fitting · corrodedFWD PIT HAS CORROSION ON STRINGER AND FRAME CLIP FASTENERS FROM FRAME 24 THRU 31 AND FROM STRINGER 39R TO 40L. REPLACED 1098 RIVETS.Feb 6, 2007 · N431UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR 2007UALA00318Wire · shortedFOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 1, 2, 3, 6. REPAIR SHORTED WIRES UNDER SEAT 6ABC. ALL EMERGENCY LIGHTS TESTED OK.Feb 5, 2007 · N402UA · Airbus A320232 · Light System WiringSDR 2007UALA00319Wire · faultyFOUND EMERGENCY EXIT PATH LIGHT IS INOP AT SEAT 18. REPAIRED WIRING UNDER SEAT 18ABC, AT PATH LIGHT CONNECTOR. OPS CHECKED OK.Feb 5, 2007 · N402UA · Airbus A320232 · Light System WiringSDR 2007UALA00320Keelbeam · crackedFOUND LEFT AND RIGHT KEELBEAM TO BELLY FAIRING SUPPORT FAIRING ATTACH ANGLES ARE CRACKED AT FRAME 46. MAJOR REPAIR ACCOMPLISHED: MFG'D & INSTALLED REPAIR ANGLE SECTION.Feb 5, 2007 · N410UA · Airbus A320232 · Fuselage Main, KeelSDR 2007UALA00332Attach Fitting · corrodedFWD FRAME CLIP AND STRINGER FASTENERS HAVE CORROSION FROM FRAME 31 TO 35 AND FROM STR 38R TO 38L. REPLACED 752 CORRODED RIVETS.Feb 5, 2007 · N431UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR 2007UALA00295Wire · shortedEPSU UNIT FWD LEFT FAILS EMERGENCY LIGHT TEST. REPLACED EPSU AND REPAIRED WIRING SHORTED TO SEAT TRACK.Feb 4, 2007 · N487UA · Airbus A320232 · Light System WiringSDR 2007UALA00294Unknown · unknownRTFL WITH A LANDING GEAR DOOR WARNING MESSAGE. PROBLEM REOCCURED ON SUBSEQUENT FLIGHT. [SUP 05-08-07] AFTER RTFL OF FLIGHT 543, FAULT WAS ORIGINALLY TRACED TO A LOOSE PROXIMITY SWITCH. SWITCH WAS SECURED AND OPS CHECKED OK. ON NEXT FLIGHT, SAME WARNING MESSFeb 3, 2007 · N429UA · Airbus A320232 · Landing Gear Position and WarningSDR 2007UALA00296Battery · failedAFT EMERGENCY LIGHT BATTERY FAILED 3SVC TEST. REPLACED AFT EMERGENCY LIGHT BATTERY. OPS CHECKED GOODFeb 2, 2007 · N491UA · Airbus A320232 · Emergency Lighting
Back to IAE V2527-A5