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 2004UALA00367Line · looseRAM AIR TURBINE DEPLOYED BUT DID NOT PROVIDE BLUE HYDRAULIC PRESSURE DURING ROUTINE MAINTENANCE TEST. NO EMERGENCY GENERATOR POWER AVAILABLE VIA RAT. FOUND LOOSE B-NUT AT RAT MODULE, TIGHTEN LINE. REMOVED AND REPLACED RAT GROUND CHECK MODULE. OPERATIONS CHECApr 16, 2004 · N453UA · Airbus A320232 · Hydraulic System, AuxiliarySDR 2004UALA00355Wire · shortedON FINAL APPROACH WIRES UNDER SEAT 25B SPARKED ELECTRICAL SMOKE. HALON FIRE EXTINGUISHER USED. CAUSE OF ELECTRICAL SPARK WAS IDENTIFIED TO ORIGINATE FROM THE SEAT-TO-SEAT CABLE, WHICH CONNECTS BOTH PES AND PSS DATA. THIS CABLE ALSO CARRIES 110 VAC. PER AIRApr 14, 2004 · N428UA · Airbus A320232 · Electrical Power System WiringSDR 2004UALA00325Pressure Switch · malfunctionedGREEN HYDRAULIC SYSTEM RSVR LO LVL ECAM DISPLAYED. GREEN HYDRAULIC SYSTEM LOW LEVEL SWITCH FAILED, REPLACED GREEN HYDRAULIC SYSTEM LOW LEVEL SWITCH, OPERATIONS CHECK NORMAL.Apr 10, 2004 · N424UA · Airbus A320232 · Hydraulic System, MainSDR 2004UALA00321Skin · damagedDAMAGE TO SKIN ON INSIDE OF AFT CARGO DOOR DIRECTLY BEHIND DOOR HANDLE HUB. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED ON DOOR INNER SKIN.Apr 9, 2004 · N429UA · Airbus A320232 · Cargo/Baggage DoorsSDR 2004UALA00315Rib · damagedLEFT WING RIB 5 FITTING INBOARD REAR SPAR FASTENER 4 FROM THE TOP, NUT SHEARED OFF. BOLT LIKELY SHEARED AT THE TIME OF INSTALLATION. NO DAMAGE TO ADJACENT FASTENERS, FASTENER HOLES OR FITTING COMMON TO PROBLEM HOLE WAS NOTED INDICATING THAT SHEARING DID NOT OCApr 7, 2004 · N426UA · Airbus A320232 · Wing, Rib/BulkheadSDR 2004UALA00306Bleed Valve · failedRETURNED TO FIELD DUE TO FAILED BLEED VALVE. FAN AIR VALVE CONTROL THERMOSTAT FAILED. REPLACED FAN AIR VALVE CONTROL THERMOSTAT. OPERATIONS CHECK NORMAL.Apr 3, 2004 · N479UA · Airbus A320232 · Pneumatic Distribution SystemSDR 2004UALA00304Actuator · corrodedRIGHT MAIN LANDING GEAR LOCK STAY ACTUATOR CYLINDER FOUND WITH CORROSION ON THE PORT STATIC SEAL SURFACE. MAJOR REPAIR ACCOMPLISHED. CORROSION REMOVED BY MACHINING AREA AROUND PORT. FOUR LAYERS OF INTERFILL APPLIED TO REWORKED AREA.Apr 1, 2004 · N412UA · Airbus A320232 · Landing Gear ActuatorSDR 2004UALA00287Connector · damagedFWD CARGO DOOR OPEN INDICATION ON TAKEOFF. *S/D* REPAIRED DAMAGED CONNECTOR BACKSHELL ON DOOR WARNING SENSOR.Mar 29, 2004 · N479UA · Airbus A320232 · Door Warning SystemSDR 2004UALA00291Compressor · seizedNR 1 ENGINE COMPRESSOR STALLED AND SUBSEQUENTLY SEIZED. OIL PRESSURE AND N2 WENT TO ZERO. NR 3 BEARING FAILED. OUTER RACE FRACTURED, BEARING CAGE DISINTEGRATED, ALL BALL BEARINGS WORN APPROXIMATELY 25 PERCENT ON OPPOSING SIDES. REPLACED ENGINE. CORRECTIVEMar 29, 2004 · N473UA · Airbus A320232 · Turbine Engine Compressor SectionSDR 2004UALA00285Damper · leakingGREEN HYDRAULIC SYSTEM FAILURE. QUANTITY ZERO, PRESSURE LOW. *S/D* YAW DAMPER NR 1 SEAL WAS FOUND LEAKING. THE FAULTY YAW DAMPER WAS REPLACED.Mar 27, 2004 · N413UA · Airbus A320232 · Rudder ActuatorSDR 2004UALA00279Windshield · crackedWINDSHIELD ON CAPTAIN'S SIDE STARTED TO CRACK & GOT PROGRESSIVELY WORSE. FLIGHT DIVERTED. WEATHER SEAL DETERIORATION LEAD TO DELAMINATION OF WINDOW ALLOWING WATER INGRESION CAUSING ARCING AT THE BUS BAR RESULTING IN CRACKING OF THE WINDSHIELD. THE WINDSHIELDMar 25, 2004 · N447UA · Airbus A320232 · Flight Compartment WindowsSDR 2004UALA00265Proximity Switch · out of adjustLEFT FWD OVERWING EXIT SHOWED OPEN ON ECAM. FLIGHT DIVERTED. THE SUBJECT DOOR'S PROXIMITY SWITCH WAS ADJUSTED.Mar 21, 2004 · N447UA · Airbus A320232 · Door Warning SystemSDR 2004UALA00300Skin · damagedUPPER RUDDER TIP MISSING. UPPER RIGHT & LEFT PANELS DAMAGED IN GFRP AREA. MAJOR REPAIR ACCOMPLISHED. REPLACED RUDDER TIP. INSTALLED NEW UPPER RIB, ATTACH ANGLE & FAIRING CAP TO RIGHT & LEFT PANELS.Mar 19, 2004 · N485UA · Airbus A320232 · Rudder, Plate/SkinSDR 2004UALA00261Annunciator · failedABORTED TAKEOFF AT 110 KNOTS DUE TO LOSING BOTH FLIGHT MODE ANNUNCIATORS. PROBLEM COULD NOT BE DUPLICATED ON GROUND. POST FLIGHT REPORT DID NOT INDICATE ANY FAULT. FMGC1 WAS REPLACED AS A PRECAUTION. OPERATIONS CHECK NORMAL.Mar 18, 2004 · N416UA · Airbus A320232 · Central WarningSDR 2004UALA00252Floor Support · corrodedAFT CABIN FLOORBOARD SUPPORT STRUCTURE AT RBL 46 IS CORRODED AT 2 LOCATIONS BETWEEN FRAMES 69 & 70. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SUPPORT STRUCTURE.Mar 17, 2004 · N411UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2004UALA00240Stringer · corrodedSTRINGER 42L CORRODED FROM FRAME 53 TO FRAME 59. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER, INSTALLED ATTACHING HARDWARE AND RESTORED FINISH.Mar 16, 2004 · N411UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2004UALA00241Stringer · corrodedSTRINGER 43L CORRODED FROM FRAME 58 TO 59. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR.Mar 16, 2004 · N411UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2004UALA00242Stringer · corrodedSTRINGER 43L CORRODED FROM FRAME 54 TO 55. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR.Mar 16, 2004 · N411UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2004UALA00236Floor Support · corrodedCABIN FLOOR SUPPORT CORRODED AT FRAME 66 AT RBL 42. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT.Mar 15, 2004 · N825UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR 2004UALA00237Floor Support · corrodedCABIN FLOOR SUPPORT CORRODED AT FRAME 66 AT RBL 40. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT.Mar 15, 2004 · N825UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR 2004UALA00238Floor Support · corrodedCABIN FLOOR SUPPORT CORRODED AT FRAME 68 AT RBL 40. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT.Mar 15, 2004 · N825UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR AWXA200400278Engine · overtempON APPROACH, NR 2 ENG EGT 890 DEGREES, FUEL FLOW 1300 LBS & OIL PRESS & TEMP NORM. DISCONN AUTOTHROT & MOVED POWER LEVER, EGT REMAINED ABOVE 800 DEGREES FOR 4 MIN, SHUTDOWN ENG & DECLARED EMERGENCY. MX FOUND ENG 4TH STAGE VARIABLE STATOR VAIN ACT LINKAGE BRAMar 14, 2004 · N657AW · Airbus A320232 · Compressor Bleed ControlSDR 2004UALA00226Control Unit · failedFLIGHT DIVERTED DUE TO AFT CARGO SMOKE ECAM MESSAGE. REPLACED SMOKE DETECTOR CONTROL UNIT (SDCU) AND FOUR AFT CARGO SMOKE DETECTORS.Mar 10, 2004 · N408UA · Airbus A320232 · Smoke DetectionSDR 2004UALA00257Skin · bird strikeBIRD STRIKE DAMAGE. LEFT O/B FLAP REPAIRED LOWER SKIN AND SPAR.Mar 10, 2004 · N457UA · Airbus A320232 · Trailing Edge FlapsSDR 2004UALA00221Floorbeam · corrodedCABIN FLOOR FRAME SUPPORT AT FR 12.24 CORRODED AT RIGHT O/B AREA. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME.Mar 9, 2004 · N452UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2004UALA00222Floorbeam · corrodedFLOORBEAM BETWEEN FR 19-20 IS CORRODED LBL 6. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM.Mar 9, 2004 · N452UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2004UALA00223Floor Support · corrodedAFT CABIN FLOOR SUPPORT RBL 34 FROM FRAME 64 TO 66 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME FLOOR SUPPORT.Mar 9, 2004 · N452UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2004UALA00224Floor Support · corrodedFLOOR SUPPORT CORRODED BETWEEN FR 19-20 RBL 6. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM.Mar 9, 2004 · N452UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2004UALA00225Floor Support · corrodedFLOOR SUPPORT CORRODED BETWEEN FR 66-70 RBL 34. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT.Mar 9, 2004 · N452UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2004UALA00197Uplock · damagedRETURN TO FIELD DUE TO LEFT MAIN GEAR NOT LOCKED INDICATION. REPLACED MLG UPLOCK ASSEMBLY AND PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE LANDING GEAR.Mar 7, 2004 · N414UA · Airbus A320232 · Landing Gear Position and WarningSDR 2004UALA00196Seal · failedDURING APPROACH WINDSHIELD CRACKED AND BEGAN TO ARC. WEATHER SEAL DETERIORATION LED TO DELAMINATION OF WINDOW ALLOWING WATER INGRESION CAUSING ARCING AT THE BUS BAR AND HEAT FILM RESULTING IN CRACKING OF THE WINDSHIELD. THE WINDSHIELD WAS REPLACED.Mar 6, 2004 · N449UA · Airbus A320232 · Flight Compartment WindowsSDR 2004UALA00171Flap · failedFLIGHT LANDED SAFELY WITH ZERO FLAPS. ECAM FCTL FLAPS LOCKED WITH CFDS MSG FLP 1 OVERSPEED RT CHECK FLP MECH DRIVE. RT NR 1 FLAP ACTUATOR 6255CM SHAFT WAS FOUND LOOSE AND HAD MORE THAN 0.25 INCH OF RADIAL PLAY. THE CONNECTING U-JOINTS WERE ALSO FOUND LOOSE AFeb 26, 2004 · N410UA · Airbus A320232 · Trailing Edge Flap Control SystemSDR CA040223001Wire · burned(CAN) WHILE TROUBLE SHOOTING THE NON-DEPLOYMENT OF A VIDEO MONITOR IT WAS FOUND THAT THE JUNCTION BOX FOR THIS MONITOR HAD FAILED. THE UNIT SMELLED OF BURNED ELECTRICAL MATTER. THERE WHERE SIGNS OF ARCING SHOWING ON THE OUTSIDE CASE. THE ASSOCIATED MONITOR DIDFeb 21, 2004 · Airbus A320232 · Equipment/Furnishings WiringSDR 2004UALA00148Sill · corrodedAFT PASSENGER ENTRY DOOR (L2) DOOR SILL PLATE AT FRAME 68 IS CORRODED AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NESTED ANGLE & FILLER REPAIR.Feb 20, 2004 · N410UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2004UALA00149Support Beam · corrodedAFT CABIN STRUCTURE SUPPORT BEAM AT FRAME 67 RBL 50 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FLOOR SUPPORT.Feb 20, 2004 · N410UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2004UALA00122Check Valve · overheatedRETURN TO FIELD DUE TO YELLOW HYDRAULIC SYSTEM OVERHEAT. REPLACED THE YELLOW ELECTRIC PUMP CHECK VALVE 3083GM. CHECK VALVE WAS BROKEN INTERNALLY.Feb 13, 2004 · N448UA · Airbus A320232 · Hydraulic System, MainSDR 2004UALA00113Connector · damagedAFT RT, LWR DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED CONNECTOR. CHECKS OK.Feb 10, 2004 · N479UA · Airbus A320232 · Emergency LightingSDR 2004UALA00103Actuator · malfunctionedRETURN TO FIELD UNDER AMBER ALERT DUE TO YELLOW HYDRAULIC SYSTEM PROBLEM. REPLACED THE NUMBER ONE THRUST REVERSER ACTUATOR.Feb 8, 2004 · N424UA · Airbus A320232 · Engine Thrust ReverserSDR 2004UALA00105Light · inoperativeWHITE EEL LIGHTS ARE INOPERATIVE AT ROWS 6 ABC AND 20 ABC. REPLACED EEL LIGHTS. OPS CHECKED NORMAL.Feb 6, 2004 · N822UA · Airbus A319131 · Emergency LightingSDR 2004UALA00107Lever · malfunctionedWHILE TRYING TO DROP GEAR ON APPROACH, ECAM MSG SHOWED LGCIU 1 AND 2 FAILURE. THIS WAS A POSITIONING FLIGHT. REPLACED LANDING GEAR LEVER.Feb 6, 2004 · N412UA · Airbus A320232 · Landing Gear SelectorSDR 2004UALA00087Valve · failedFLIGHT EXPERIENCED A GREEN HYDRAULIC SYSTEM FAILURE. REPLACED THE HYDRAULIC SAFETY VALVE.Jan 30, 2004 · N822UA · Airbus A319131 · Hydraulic System, MainSDR 2004UALA00090Stringer · corrodedAFT PIT STRINGER 43L IS CORRODED FROM FRAME 54 TO FRAME 56. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER SECTION AND SPLICE REPAIRS.Jan 30, 2004 · N408UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2004UALA00065Computer · failedRETURN TO FIELD DUE TO DUAL FMS FAILURE. FMGC1 WAS FAULTED ON THE POST FLIGHT REPORT. REPLACEMENT OF THE FMGC1 WAS ACCOMPLISHED AND SUBSEQUENT OPERATIONS TEST REVEALED NO FURTHER ANOMALY.Jan 27, 2004 · N452UA · Airbus A320232 · Flight Management Computing Hardware SystemSDR 2004UALA00069Yoke · failedFLIGHT DIVERTED TO DEN AND CANCELLED DUE TO BLUE HYDRAULIC SYSTEM OVERHEATING. REPLACED BLUE SYSTEM HYDRAULIC PUMP. THE GUIDE YOKE BEARING FAILED IN THE MOTOR.Jan 27, 2004 · N457UA · Airbus A320232 · Hydraulic System, MainSDR AWXA200400082Bleed Valve · malfunctionedON CLIMBOUT, ECAM INDICATED NR 2 ENG STALL, A/C SHUDDERED, A LOUD THUMP HEARD, & LT WING DIPPED, NO ABNORMAL ENG READING INDICATIONS NOTED. TURNED BACK & LANDED WITHOUT EVENT. MAINT TROUBLESHOT IAW TSM. R & R 7TH STAGE BLEED VALVE IAW AMM, & 7TH STAGE BLEEDJan 26, 2004 · N656AW · Airbus A320232 · Compressor Bleed ValveSDR 2004UALA00057Valve · defectiveRETURN TO FIELD DUE TO A PRESSURIZATION PROBLEM. INABILITY TO PRESSURIZE WAS RESULT OF A MALFUNCTIONING SKIN AIR OUTLET VALVE. THE DEFECTIVE UNIT WAS REPLACED AND VERIFIED FAULTY. NO FURTHER PRESSURIZATION PROBLEMS REPORTED SINCE UNIT REPLACEMENT.Jan 24, 2004 · N439UA · Airbus A320232 · Pressure Regulator/Outflow ValveSDR 2004UALA00046Stringer · corrodedSTRINGER 43L CORRODED BETWEEN FRAMES 56 AND 57. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED STRINGER SECTION. FABRICATED & INSTALLED NESTED STRINGER SPLICE REPAIR PER SRM 53-0013 FIG 201.Jan 21, 2004 · N409UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2004UALA00050Adiru · failedFLIGHT DIVERTED DUE TO LOSS OF MULTIPLE NAVIGATION FUNCTIONS. ADIRU 3 WAS REMOVED AND TESTED. ADIRU 1 WAS MOVED TO NR 3 POSITION AND A REPLACEMENT UNIT INSTALLED IN POSITION NR 1. NR 1 IDG WIRING WAS CHECKED AS POSSIBLE CAUSE WITH NO FAULTS FOUND. ADIRU SYJan 21, 2004 · N425UA · Airbus A320232 · Inertial Guidance SystemSDR 2004UALA00034Link Assy · bentFLIGHT DIVERTED DUE TO PROBLEM WITH THE LANDING GEAR. FOUND LINK ON PROXIMITY SENSOR ASSEMBLY BENT. STRAIGHTENED LINK AND PERFORMED OPERATIONAL CHECK OF GEAR RETRACTION. OPERATIONS CHECK NORMAL.Jan 13, 2004 · N475UA · Airbus A320232 · Nose/Tail Landing GearSDR 2005UALA00050Sensor · malfunctionedNR 2 ENGINE REVERSER FAULT LIGHT ILLUMINATED. THE CAUSE WAS THE MAIN LANDING GEAR SENSOR 22GA. SENSOR 22GA WAS REPLACED. THE FLIGHT MANUAL PROCEDURES FOR ABNORMAL AND EMERGENCY SECTION 3.03.70 PG 1 SEQ 035 REV 24 WAS REVIEWED AND IT WAS FOUND THAT THE REVERJan 11, 2004 · N410UA · Airbus A320232 · Engine Thrust Reverser
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