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 2007UALA01778Power Supply · improper partDURING EMERGENCY LIGHT EEL TEST, HALF OF THE SEATS FAILED TO ILLUMINATE.Jun 1, 2007 · N460UA · Airbus A320232 · Emergency LightingSDR 2007UALA01737Oxygen Bottle · low pressurePORTABLE O2 BOTTLE AFT LT LOW.May 31, 2007 · N493UA · Airbus A320232 · Portable Oxygen SystemSDR 2007UALA01746Bottle · unserviceableLOW BOTTLE PRESSUREMay 31, 2007 · N481UA · Airbus A320232 · Escape SlideSDR 2007UALA01747Skin · damagedLEFT AND RIGHT LWR WING SKINS HAD DAMAGED FASTENER HOLES AT MOUNTING FLANGE OF PANELS 540NB, 540PB, AND 640NB, 1EA HOLE AT EACH PANEL.May 31, 2007 · N416UA · Airbus A320232 · Wing, Plate/SkinSDR 2007UALA01732Mask · malfunctionedCREW REPORT: FIRST OFFICER`S 02 MASK PUSH TO TEST INOP. OBS MASK OKAY.May 30, 2007 · N408UA · Airbus A320232 · Crew Oxygen SystemSDR 2007UALA01729Controller · malfunctionedCAPTAIN'S SLIDING WINDOW HOT TO TOUCH AND HAS MANY DELAMINATED BUBBLES. [06-26-07] REPLACED CAPTAIN SLIDING WINDOW. ALSO NR 1 WINDOW HEAT CONTROLLER REPLACED FOR OVERHEATED LT SLIDING WINDOW. ACCOMPLISHED TESTS AFTER WINDOW REPLACEMENT AND NO CLASS 3 MSG May 29, 2007 · N469UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR 2007UALA01659Light · malfunctionedEMERGENCY EXIT LIGHTS ON W-SWITCH IN ARM. RESET CIDS AND ACCOMPLISHED EMERGENCY LIGHTING SYSTEM TEST. TEST PASS, EMERGENCY LIGHTS CHECK NORMAL.May 28, 2007 · N489UA · Airbus A320232 · Emergency LightingSDR 2007UALA01660Connector · disconnectedEMERGENCY ESCAPE PATH LIGHTING INOP AT SEAT 1-ABC. RECONNECTED UNPLUGGED EMERGENCY LIGHT CONNECTOR. OPS CHECK GOOD.May 28, 2007 · N489UA · Airbus A320232 · Light System WiringSDR 2007UALA01651A/C Pack · overheatedRTFL DUE TO PACK OVERHEAT PROBLEM.May 27, 2007 · N417UA · Airbus A320232 · Cabin Cooling SystemSDR 2007UALA01721Control Unit · faultedNW STEERING FAULT DISPLAYED WHEN PUTTING GEAR DOWN. [06-26-07] REPLACED STEERING SEVO CONTROL 6GC AND BSCU STEERING. DETERMINED A FAILED SENSOR 22GA, AFTER RING OUT SENSOR ON RT MAIN TRUCK INITIAL READING WAS 15 OHMS THEN SENSOR READ OPEN. SENSOR MUST READMay 27, 2007 · N462UA · Airbus A320232 · Landing Gear Steering SystemSDR 2007UALA01657Skin · damagedTHERMOGRAPHIC INSPECTION OF THE LEFT ELEVATOR UPPER SKIN AN INDICATION OF POSSIBLE LIGHTNING STRIKE DAMAGE WAS NOTED AT 25.25 INCHES FROM I/B EDGE AND 18.5 INCHES FROM AFT EDGE OF ELEVATOR. [06-26-07] UPPER SKIN WAS CUT OUT IN AREA OF INDICATION FOR EVALUATIMay 26, 2007 · N420UA · Airbus A320232 · Elevator, Plate/SkinSDR 2007UALA01720Wire · damagedCIDS DISPLAY LEFT EMERGENCY SLIDE BOTTLE LOW PRESSURE. [06-26-07] FOUND OPEN WIRE DEU-B (300RH4) PIN 36 TO PLUG 7555VC-A PIN A. BOTH CONNECTORS VERIFIED OK. SUSPECT LOST CONNECTION AT TERMINAL BLOCK 7225VT OR 7223VT. RESEATED PINS 3CD AT TERMINAL BLOCK 7May 26, 2007 · N417UA · Airbus A320232 · Equipment/Furnishings WiringSDR 2007UALA01658Door Frame · corrodedCORROSION AT R2 DOOR SILL FRAME 68 AND AT FWD END OF R2 DOOR SILL FR 66. MAJOR REPAIR ACCOMPLISHED: INSTALLED 2EA DOUBLER REPAIRS.May 25, 2007 · N440UA · Airbus A320232 · Fuselage Main, StructureSDR 2007UALA01618Sill · corrodedCORROSION ON DOOR L2 DOOR SILL AT FRAME 68.May 23, 2007 · N440UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2007UALA01630Flap System · malfunctionedCREW REPORTS THAT ON APPROACH FLAPS LOCKED OUT AT 1 UNIT, UNABLE TO RESET. AMBER ALERT DECLARED. LANDED WITH LEADING EDGE DEVICES UP AND FLAPS AT 1 DEGREE.May 23, 2007 · N433UA · Airbus A320232 · Trailing Edge Flap Control SystemSDR 2007UALA01596Unknown · vibrationVIBRATION FELT DURING CLIMB IN MID-AFT CABIN AREA. AFTER LEVEL-OFF VIBRATION STOPPED. VIBRATION WAS FELT IN CLIMB AND DESCENT AND IT WAS A SIDE TO SIDE MOTION THAT GOT MORE PRONOUNCED WITH INCREASE IN SPEED.May 22, 2007 · N481UA · Airbus A320232 · Aircraft StructuresSDR 2007UALA01584Engine · unknownCREW REPORT: BIRD STRIKE LEFT ENGINE. EPR ROLLED BACK HALFWAY AND CAME BACK NORMAL. BIRD REMAINS IN ENGINE. [07-24-07] BIRDSTRIKE AFTER TAKE-OFF RESULTED IN RTF.May 21, 2007 · N455UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2007UALA01550Tab · brokenRIGHT ELEVATOR HINGE FITTING NR 1 LWR ANTI-ROTATION TAB IS BROKEN OFF. MAJOR REPAIR ACCOMPLISHED: INSTALLED T-ANGLE REPAIR TO REPLACE ANTI-ROTATION TAB.May 20, 2007 · N412UA · Airbus A320232 · Elevator Miscellaneous StructureSDR 2007UALA01557Cover · unsecureCREW REPORT: 2 RT DOOR HANDLE COVER SEPARATED FROM A-C. [06-26-07] RESECURED SLIDE COVER.May 20, 2007 · N456UA · Airbus A320232 · Escape SlideSDR 2007UALA01560Unknown · vibrationAIRFRAME VIBRATIONS BEGIN IN CLIMB FL185 AND FADES OUT APPROX FL.May 20, 2007 · N443UA · Airbus A320232 · Aircraft StructuresSDR 2007UALA01558Tape · peelingSTRONG VIBRATION IN AFT GALLEY REPORTED BY FLT ATTENDANTS. STRONG ENOUGH TO VIBRATE ITEMS OFF COUNTER. SUPPLEMENTAL DATA UPDATE PERFORMED RUDDER FREEPLAY CHECK AND FOUND WITHIN LIMITS. FOUND EROSION PROTECTOVE TAPE PEELING FROM LEADING EDGE OF VERTICAL STABILMay 20, 2007 · N476UA · Airbus A320232 · Vertical Stabilizer, Plate/SkinSDR 2007UALA01548Angle · crackedLEFT WHEEL WELL LOWER FUSELAGE BELLY FAIRING SUPPORT ANGLE 5 IN LBL IS CRACKED AT FRAME 46. MAJOR REPAIR ACCOMPLISHED: REPLACED KEEL BEAM ANGLE.May 19, 2007 · N412UA · Airbus A320232 · Fuselage Main, KeelSDR 2007UALA01549Angle · crackedRIGHT WHEEL WELL LOWER FUSELAGE BELLY FAIRING SUPPORT ANGLE 5 IN RBL IS CRACKED AT FRAME 40. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE.May 19, 2007 · N412UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2007UALA01552Connector · damagedRIGHT INBOARD AND OUTBOARD FUEL QTY IND 2 AMBER DASHES ON FUEL PAGE. UNRELIABLE DATA. [06-26-07] FAULT TRACING FOUND FAULTY FUEL BOOST PUMP FUSE CONNECTOR. REPLACED 4044VCA FUSE CONNECTOR.May 19, 2007 · N421UA · Airbus A320232 · Fuel System WiringSDR 2007UALA01526Butt Joint · damagedREINSTALLED DOUBLER REPAIR AFTER AFT SKIN REPLACEMENT. DOUBLER LOCATED AT FR 70 BUTT JOINT STR 34. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW DOUBLER AT BUTT JOINT.May 17, 2007 · N417UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2007UALA01528Wire · detachedSEAT 1C EEL LIGHT INOP. FOUND 2 WIRES DETACHED UNDER SEAT RAIL. [SUP 06-06-07] REPAIRED EEL LIGHT WIRES UNDER SEAT 1C.May 17, 2007 · N483UA · Airbus A320232 · Light System WiringSDR 2007UALA01502Oxygen Mask · wrong partCABIN SEAT 6ABC OXYGEN MASKS (4 EA) HAVE WRONG PART NUMBERS ON THEM. INSTALLED 4 EA CORRECT MASKS.May 14, 2007 · N454UA · Airbus A320232 · Passenger Oxygen SystemSDR 2007UALA01506Relay · inoperativeON CARGO SMOKE TEST AGENT 2 DISCHARGE LIGHT DOES NOT ILLUMINATE. [06-29-07] FAULT TRACED TO A FAULTY RELAY. REPLACED 17WX DISCHARGE 2 LIGHT RELAY.May 12, 2007 · N446UA · Airbus A320232 · Fire Protection System WiringSDR 2007UALA01483Wire · brokenDURING 3 SVC, CABIN EMERGENCY LIGHT TEST DID NOT PASS. [SUP 06-06-07] REPAIRED BROKEN WIRE AT DOOR HINGE.TESTED OK.May 11, 2007 · N415UA · Airbus A320232 · Light System WiringSDR 2007UALA01484Stringer · corrodedSTRINGER 43 LEFT HAS CORROSION FRAME 57 AND 58. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE DOUBLER REPAIR.May 11, 2007 · N433UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2007UALA01485Lanyard · improper partCABIN SEAT 7ABC OXYGEN MASKS HAVE WRONG PARTS. GENERATOR IS MISSING FOAM AT FWD END AND LANYARDS ARE THE WRONG TYPE.May 11, 2007 · N454UA · Airbus A320232 · Passenger Oxygen SystemSDR 2007UALA01486Angle · crackedLOWER KEEL BEAM FRAME 47 FAIRING ATTACH ANGLE LEFT SIDE IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE.May 11, 2007 · N411UA · Airbus A320232 · Fuselage Main, KeelSDR 2007UALA01487Angle · crackedLOWER KEEL BEAM FAIRING SUPPORT ANGLE RIGHT SIDE AT FRAME 46 IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE.May 11, 2007 · N411UA · Airbus A320232 · Fuselage Main, KeelSDR 2007UALA01488Battery · failedEMERGENCY LIGHT TEST FAILED. THE -EPSU INT LOAD EMER L- DISPLAYED. REPLACED BATTERY.May 11, 2007 · N481UA · Airbus A320232 · Emergency LightingSDR 2007UALA01461A/C Pack · failedRTFL DUE TO NR 2 PACK FAILURE & NR 1 PACK'S CURRENT DEFERRAL. AFTER ATB, ON GROUND TESTING INDICATING NORMAL SINGLE PACK OPS-PERFORMED PACK TEMP CONTROL TEST- OK, REPLACED TURBINE BYPASS VALVE - ALL OPS TESTS ARE NORMAL- NO REPEATS SINCE ORIGINAL.May 10, 2007 · N421UA · Airbus A320232 · Cabin Cooling SystemSDR 2007UALA01465Stringer · corrodedCORROSION IN AFT PIT LEFT SIDE AT STRINGER 43L, FRAME 57. MAJOR REPAIR ACCOMPLISHED: INSTALLED SPLICE REPAIR.May 10, 2007 · N474UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2007032Engine · surgesENG NR 1 STALL ON CLIMB. ONE SURGE. EXAMINED THE INLET, EXHAUST AND BLEED VALVES FOR FOREIGN MATERIAL AND EVIDENCE OF INTERNAL ENGINE DAMAGE IAW AMM TASK 71-00-00-810-808. NO DEFECTS NOTED. PERFORMED BOROSCOPE INSPECTION OF HPC STAGES ENG 1, 3, 6 AND 12 IAMay 8, 2007 · N561JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2007UALA01447Switch · malfunctionedFLIGHT DIVERTED DUE TO YELLOW HYD RESERVOIR LOW LEVEL. REPLACED LOW LEVEL SWITCH.May 8, 2007 · N437UA · Airbus A320232 · Hydraulic System, MainSDR 2007UALA01449Battery · faultedEMERGENCY LIGHT TEST FAILED DURING 3SVC. EPSU BATTERY AFT L IS FAULTED. REPLACED EPSU BATTERY FOR 13WL.May 8, 2007 · N460UA · Airbus A320232 · Emergency LightingSDR 2007UALA01436Blades · failedRTFL WITH NR 1 ENGINE SHUT DOWN. LOUD BAND HEARD ON CLIMBOUT. REPLACED NR 1 ENGINE. [06-26-07] ENGINE INGESTED COWLING ACOUSTIC PANELS DURING CLIMBOUT CAUSING DAMAGE TO A STAGE 3 COMPRESSOR BLADE.May 7, 2007 · N428UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2007UALA01415Seat Track · gougedCABIN OUTBOARD RIGHT SEAT TRACK HAS GOUGED LUG FWD ON FRAME 47. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOORBEAM.May 5, 2007 · N433UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR 2007UALA01380Sill · corrodedL2 DOOR SILL HAS CORROSION AT AFT SIDE NEAR FRAME 68. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE REPAIR.May 2, 2007 · N433UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2007UALA01389Bearing · failedBLOWER FAN INOPERATIVE. UPON ARRIVAL TO AIRCRAFT FOUND C/B`S AD10 AND AE02 OPEN AND ELECTRICAL ODOR ON FLIGHT DECK. [06-26-07] REPLACED BLOWER FAN. SUSPECT FAILED BEARINGS.May 2, 2007 · N442UA · Airbus A320232 · Air Distribution FanSDR 2007UALA01390Girt Bar · dirtyAFT LEFT DOOR WILL NOT ARM. [06-26-07] CLEANED DEBRIS FROM GIRT BAR AREA.May 2, 2007 · N409UA · Airbus A320232 · Emergency EquipmentSDR 2007UALA01363Servo · vibrationVIBRATION AT 300KT APPEARS TO GO AWAY WITH RIGHT RUDDER INPUT STOPS AT 275 WITH NO SAMC TEXT: CREW REPORTING VIBRATION WHILE CLIMBING AT SPEEDS ABOVE 275 WITH NOTICEABLE VIBRATIONS FELT IN SEAT AND RUDDER PEDALS THAT WOULD BE CORRECTED WITH RIGHT RUDDER INPUTApr 30, 2007 · N490UA · Airbus A320232 · Rudder Control SystemSDR 2007UALA01369Unknown · sparksCREW REPORTS, DURING ENG 1 START NO N2 ROTATION WITH GOOD START VALVE OPEN INDICATION. RAMP REPORTED SPARKS FROM STARTER AREA. [06-26-07] REPLACED THE STARTER AND START VALVE. PRESENCE OF SPARKS INDICATES PROBABLE INTERNAL BEARING FAILURE RESULTING IN TURBINApr 30, 2007 · N483UA · Airbus A320232 · Engine StarterSDR 2007UALA01329Battery · dischargedEEL LIGHT TEST FAIL: -BATTERY FWD LT. REPLACED EEL LIGHT BATTERY AT DOOR 1L. TESTS NORMALLY NOW.Apr 28, 2007 · N422UA · Airbus A320232 · Emergency LightingSDR 2007UALA01246Compressor · stalledCREW RECEIVED NR 1 ENG STALL ECAM AT FL380 IN LIGHT CHOP & LIGHT MTN WAVE ACTIVITY. LOUD BANG HEARD BY F/A. [06-14-07] REPLACED NR 1 ENGINE DUE TO STALL HISTORY.Apr 21, 2007 · N454UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2007UALA01260Transducer · faultyPITCH TRIM KEEPS HUNTING NOSE UP ATTITUDE. *S/D* FAULT TRACED TO FAULTY THS ACTUATOR POSITION TRANSDUCER. REPLACED BOTH COMMAND AND MONITOR TRANSDUCERS AS A PRECAUTIONARY MEASURE.Apr 20, 2007 · N490UA · Airbus A320232 · Stabilizer Position IndicatingSDR 2007UALA01230Oxygen System · reads lowCREW O2 EMPTY ONLY 50 PSI AT SHUTDOWN. [06-22-07] "PRESS TO TEST" SLIDE SWITCH ON CAPTAIN'S O2 MASK STOWAGE BOX STICKS, ALLOWING SLOW LEAK THROUGH TEST FUNCTION. REPLACED OXYGEN MASK STOWAGE BOX.Apr 19, 2007 · N420UA · Airbus A320232 · Crew Oxygen System
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