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 2008UALA02717Relay · failedEMERGENCY GENERATOR DOES NOT COME ON WHEN EMER GEN SW IS SELECTED. TRIED RELAY 12XE AND CONTROL UNIT 1XE, NO HELP. CK'D FOR VOLTAGE AT HYD FLOW SOLENOID ON TOP OF EMER GEN 8XE, NO VOLTAGE PRESENT. *S/D* RAT EXT INHIB COND RELAY BAD. REPLACED RAT EXT INHIBMay 10, 2008 · N421UA · Airbus A320232 · AC Generation SystemSDR 2008UALA02718Lanyard · out of positionNO LANYARD VISIBLE ALL 4 DOOR SLIDES. REPOSITIONED LANYARD ON AL L SLIDES, OK FOR SERVICE.May 9, 2008 · N422UA · Airbus A320232 · Escape SlideSDR 2008UALA02732Power Supply · failedEPSU INT LOAD EMER R MESSAGE AT CIDS DURING OPERATIONAL TEST OF EMERGENCY CABIN LIGHTS AND SIGN CK. FOUND EPSU FAILED. REPLACED RT O/W EPSU, CHECKS GOOD.May 9, 2008 · N463UA · Airbus A320232 · Emergency LightingSDR 2008UALA02716Sdac · malfunctionedF-CTL ELAC 1 FAULT AND ELAC 2 FAULT. REPLACED SDAC NR 2, OPS TESTS OK. NOMay 8, 2008 · N496UA · Airbus A320232 · Flight Control SystemSDR 2008UALA02695Light · inoperativeSEAT 8A EMERGENCY LIGHT INOP.May 8, 2008 · N451UA · Airbus A320232 · Emergency LightingSDR 2008UALA02668Battery · faultyEMERGENCY LIGHTS WILL NOT PASS SYSTEM TEST. "EPSU BATTERY AFT L" MESSAGE. REPLACED BATTERY. TESTS OKAY.May 7, 2008 · N485UA · Airbus A320232 · Emergency LightingSDR 2008UALA02687Unknown · odorODOR IN COCKPIT SMELLED ELECTRICALLY HOT TURNED BLOWER FAN TO OVRD, SMELL DISSIPATED. May 7, 2008 · N420UA · Airbus A320232 · Air Distribution SystemSDR 2008UALA02629Window · failedON APPROACH AT ABOUT 5000 FT, BIRD STRIKE ON F/O SIDE WINDOW. WINDOW CRACKED.May 6, 2008 · N437UA · Airbus A320232 · Flight Compartment WindowsSDR 2008UALA02630Slide · reads lowSLIDE PRESSURE AT DOOR 1R SHOWS ON RED. REPLACED SLIDE.May 6, 2008 · N426UA · Airbus A320232 · Escape SlideSDR 2008UALA02635Battery · failedRT OVERWING EMERGENCY LIGHT BATTERY FAILED TEST. REPLACED BATTERY. TEST OK.May 5, 2008 · N435UA · Airbus A320232 · Emergency LightingSDR 2008UALA02636Floor Support · corrodedFLOOR SUPPORT CORRODED FROM C66 TO C68 RBL 30. MAJOR REPAIR ACCOMPLISHED: REPLACED BEAM SUPPORT & SEAT TRACK.May 5, 2008 · N444UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02637Floorbeam · corrodedFLOORBEAM JUST INBD OF AFT LT MED IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOORBEAM.May 5, 2008 · N444UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02644Slide · low pressureSLIDE PRESS AT DOOR 1R SHOWS ON RED. REPLACED SLIDE.May 5, 2008 · N426UA · Airbus A320232 · Escape SlideSDR 2008UALA02598Warning Light · illuminatedF-CTL ELAC 2 PITCH FAULT ECAM AFTER ENG START. ELAC2 FAILING-INTERNAL RELAY FAILING TEST. REPLACED ELAC , ALL OPS CHECKS WERE NORMAL.May 4, 2008 · N445UA · Airbus A320232 · Central WarningSDR 2008UALA02577Bulb · inoperativeEXIT LIGHT UNDER AFT RIGHT OVERWING EXIT DOOR (90WL4) INOP. FOUND BULB INOPERATIVE. REPLACED LIGHT AT EXIT.May 3, 2008 · N445UA · Airbus A320232 · Emergency LightingSDR 2008UALA02578Structure · damagedDOOR 1L AREA IS GASHED. THIS IS A MAJOR REPAIR. CUT OUT DAMAGE AND REPAIRED PER SRM 53-11-11 ON NR D0453A DURING H MV VISIT. PERMANENT REPAIR.May 3, 2008 · N495UA · Airbus A320232 · Passenger/Crew DoorsSDR 2008UALA02572Window · faultyF/O SLIDING WINDOW HAS BUBBLES FORMING ON ENTIRE WINDOW. HOT TO TOUCH. REPLACED F/O SLIDING WINDOW.May 2, 2008 · N433UA · Airbus A320232 · Flight Compartment WindowsSDR 2008UALA02576Web · corrodedFLOOR WEB CORRODED BETWEEN C69 AND C70, UPPER AND LWR SURFACE, RT SIDE. MAJOR REPAIR ACCOMPLISHED, REPLACED FLOOR WEB.May 2, 2008 · N444UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02616Radar · inoperativeWEATHER RADAR SYSTEM INOP. FLIGHT DIVERTED. REPLACED CONTROL PANEL AND REPLACED SCANNER, OPS CHECKED NORMAL.May 2, 2008 · N401UA · Airbus A320232 · Weather Radar SystemSDR 2008UALA02532Line · leakingA/C LOSING OIL QUANTITY. FLIGHT DIVERTED. OIL SUPPLY PRESSURE TUBE FOUND DAMAGED AND LEAKING. TUBE REPLACED CORRECT THIS CONDITION.May 1, 2008 · N411UA · Airbus A320232 · Turbine Engine Oil SystemSDR 2008UALA02548Floor Support · corrodedFLOOR SUPPORT CORRODED IN TWO AREAS BETWEEN C69 AND C70, LBL 8". MAJOR REPAIR ACCOMPLISHED, REPLACED FLOOR SUPPORT.May 1, 2008 · N444UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02542Slide · damagedDOOR 1L SLIDE-RAFT GIRT RUBS ON FLOOR AFTER INSTALLATION AND GIRT IS FRAYED. FOUND WEAR AND IMPROPER LANYARD INSTALLATION. REPLACED SLIDE.Apr 30, 2008 · N405UA · Airbus A320232 · Escape SlideSDR 2008UALA02528Control Servo · failedPER CREW, AIRCRAFT PULLS TO LEFT AT TAXI SPEED, REQUIRES 2 DEGREES OF TILLER DEFLECTION. SUPPLEMENTAL DATA UPDATE, NOSE WHEEL STEERING CONTROL SERVO FAILING. REPLACED NOSE WHEEL STEERING CONTROL SERVO, TAXI TEST GOOD.Apr 30, 2008 · N413UA · Airbus A320232 · Steering UnitSDR 2008UALA02512Oxygen System · reads lowOXYGEN PRESSURE LOW.Apr 29, 2008 · N449UA · Airbus A320232 · Oxygen SystemSDR 2008UALA02527Oxygen Mask · faultyCAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. SWAPPED CAPTS AND 2ND OBS BOX. ALL LINES LEAK CHECKED GOOD. MASK AND RADIO OPS NORMAL AT CAPTAIN'S SPOT.Apr 29, 2008 · N470UA · Airbus A320232 · Crew Oxygen SystemSDR 2008UALA02513Unknown · odorUNIDENTIFIED PLASTIC BURNING SMELL FROM ROW 24. SMELL INTENSIFIED. FLIGHT DIVERTED. NO SMELL NOTICED ON AC ARRIVAL. TURNED RECIRC FANS BACK ON, RAN PACKS. TURNED ALL CABIN LIGHTS ON. RAN VIDEO SYS, NO SMELL NOTICED. CKD GALLEY AREA, NO SMELLS NOTICED. Apr 29, 2008 · N425UA · Airbus A320232 · Air Distribution SystemSDR 2008UALA02514Control Unit · failedELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS, MULTIPLE ELAC 2 FAULTS ON DESC INTO DEN. AP2 WAS ENGAGED AT THE TIME. SWITCH TO AP1 NO ELAC2. INTERNAL CARD Q4 FAILING CH 2 INITIALIZING TEST. ELAC FAULTING. REPLACED ELAC 2, OPS TESTING GApr 29, 2008 · N470UA · Airbus A320232 · Elevator Control SystemSDR 2008UALA02490Sill · corrodedCORROSION ON R2 DOOR FWD OF FRAME 66. REPLACED SILL.Apr 28, 2008 · N448UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02491Sill · corrodedCORROSION ON R2 DOOR SILL AT FRAME 68. REPLACED SILL.Apr 28, 2008 · N448UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02461Light · inoperativeEEL LIGHT INOP . REPLACED LIGHT ASSY.Apr 27, 2008 · N453UA · Airbus A320232 · Emergency LightingSDR 2008UALA02511Floor Support · corrodedFOUND CORROSION IN FLOOR SUPPORT STRUCTURE AT FRAME 68 UNDER DOOR 2R THRESHOLD. MAJOR REPAIR ACCOMPLISHED, REPLACED FLOORBEAM -Y1292 FROM FR 64-69.Apr 27, 2008 · N448UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02462Connector · looseFLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT OUT AT SEAT 26C. FOUND LOOSE PLUG. SECURED PLUG AND LIGHTS TEST OK. Apr 27, 2008 · N494UA · Airbus A320232 · Light System WiringSDR 2008UALA02445Control Unit · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED ELAC 1, OPS CHECKED NORMAL.Apr 26, 2008 · N401UA · Airbus A320232 · Central WarningSDR 2008UALA02446Harness · leakingFO'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). F/O`S O2 HARNESS LEAKING AT COUPLER. FOUND HARNESS COUPLER IS LEAKING O2. REPLACED F-O MASK STOWAGE BOX ASSY, NO LEAKS NOTED AFTER SERVICE.Apr 26, 2008 · N461UA · Airbus A320232 · Crew Oxygen SystemSDR 2008UALA02419Skin · wornSKIN WORN THROUGH TO FRAME AT FR 70 STGR 44 DAMAGE MEASURES APPROX 6 INCH BY 4 INCH FROM TAIL STRIKE. SKIN WORN THROUGH TO FRAME AT FR70 STGR 44 DAMAGE MEASURES APPROX 6"X 4" FROM TAIL STRIKE BY- 254125 :CUT DAMAGED SKIN FOR ACCES S TO FRAME 70 DAMAGE EVALUATApr 25, 2008 · N457UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA02432Skin · gougedSKIN IS GOUGED AT FR 67 STRINGER 44 FROM TAIL STRIKE. SKIN WORN THROUGH TO FRAME AT FR70 STGR 44 DAMAGE MEASURES APPROX 6"X 4" FROM TAIL STRIKE BY- 254125 :CUT DAMAGED SKIN FOR ACCES S TO FRAME 70 DAMAGE EVALUATION.BLENDED DAMAGE ON FRAME.Apr 25, 2008 · N457UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA02433Skin · wornSKIN IS WORN THROUGH AT FR 68 STR 44 AND MEASURES .5 INCH WIDE BY 2 INCH LONG. CUT DAMAGED SKIN FOR ACCES S TO FRAME 70 DAMAGE EVALUATION.BLENDED DAMAGE ON FRAME. CONT OF AMIS ITEM 8572009 :MFG FILLER FOR FR70 PER EVA71452.Apr 25, 2008 · N457UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA02434Skin · wornSKIN IS WORN THROUGH AT FR 68 STR 44 AND MEASURES .5 INCH WIDE BY 2 INCH LONG. CUT DAMAGED SKIN FOR ACCES S TO FRAME 70 DAMAGE EVALUATION.BLENDED DAMAGE ON FRAME. CONT OF AMIS ITEM 8572009 :MFG FILLER FOR FR70 PER EVA71452.Apr 25, 2008 · N457UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA02439Sill · corrodedL2 DOOR SILL HAS CORROSION FWD OF FR68. MAJOR REPAIR, CORROSION OUT OF LIMITS. REPAIRED PER SRM 53-41-14 NR 4.Apr 25, 2008 · N448UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02459Relay · failedAPU FIRE EXTINGUISHING CIRCUIT CHECK FAILS. FOUND FLIGHT GROUND RELAY 43WF FAILING. FLIGHT GROUND RELAY 43WF REPLACED, OPS TESTED SYSTEM NORMAL.Apr 25, 2008 · N404UA · Airbus A320232 · Fire Bottle, PortableSDR 2008UALA02460Module · failedTEST FLIGHT, PULLING CBZ25 AND Z26 DEPLOYED RAT BUT DID NOT SHOW HYD PRESSURE TO BLUE SYSTEM. EMERGENCY GEN DID NOT WORK SINCE NO HYD PRESSURE. PUSH MAN RAT BUTTONS BUT NO CHANGE. FOUND THE GROUND CHECK MODULE FAILED. REPLACED GROUND CHECK MODULE. OPS TESTEDApr 25, 2008 · N440UA · Airbus A320232 · Hydraulic Power SystemSDR 2008UALA02412Contactor · brokenEMERGENCY ELECTRICAL GENERATING SYSTEM FAILS OPS TEST. FOUND CONTACTOR RELAY BASE BROKEN. REPLACED TRANSFORMER AND CONTACTOR BASE, ALL TESTS ARE NORMAL.Apr 24, 2008 · N433UA · Airbus A320232 · Electrical Power System WiringSDR 2008UALA02430Wire Harness · inoperativeSEAT 20 ABC FLOOR PROXIMITY ESCAPE PATH LIGHT IS INOP. FOUND DAMAGED HARNESS. REPLACED HARNESS, OPS CHECKED OK.Apr 24, 2008 · N412UA · Airbus A320232 · Light System WiringSDR 2008UALA02393Sill · corrodedR2 DOOR SILL HAS CORROSION ON INBOARD FLANGE AT FRAME 68. ACCOMPLISHED MAJOR REPAIR. MAJOR REPAIR. R2 DOOR SILL HAS CORROSION ON I-B FLANGE AT FRAME.Apr 23, 2008 · N443UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02394Sill · corrodedCORROSION ON R2 DOOR SILL AT FRAME 66. ACCOMPLISHED MAJOR REPAIR. CORROSION, INSTALLED REPAIR PER SRM.Apr 23, 2008 · N443UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA02402Oxygen Mask · leakingSUSPECT O2 LEAK CAPTOR 1ST OBS MASK FITTING. FOUND 2ND OBS. MASK DISCONNECTED. SUSPECT LEAK FROM THERE. CONNECTED MASK AND CHECKED FITTINGS FOR LEAKS, NONE NOTED, SERVICED CREW O2 TO FULL. Apr 23, 2008 · N446UA · Airbus A320232 · Crew Oxygen SystemSDR 2008UALA02369Floorbeam · corrodedFLOORBEAM CORROSION WHERE BEAM Y254 CROSSES FRAME 68 THIS LOCATION IS JUST AFT OF LAV WASTE TANK AND TO LEFT OF AIRCRAFT CENTERLINE ON LEFT SIDE OF FLOORBEAM. REMOVED CORROSION IAW SRM 51-74-00. REMOVED FLOORBEAM IAW SRM 51-42-11. LOCATED , DRILLED AND DEBURRApr 22, 2008 · N448UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA02374Structure · damagedBOTTOM OF DOOR 1L DAMAGED. AFTER VISUAL INSPECTION FOUND DENT TO BE WITHIN LIMITS THICKER THEN .063 CANNOT BE DRESSED OUT. WILL REQUIRE DOUBLER REPAIR. SCHEDULED FOR A PERMANENT REPAIR.Apr 22, 2008 · N467UA · Airbus A320232 · Fuselage Main, StructureSDR 2008UALA02370Skin · wornSKIN IS WORN THROUGH AT FR 69 STRINGER 44 AND MEASURES .5 INCH WIDE BY 2 INCH LONG. SKIN WORN THROUGH TO FRAME AT FR70 STGR 44 DAMAGE MEASURES APPROX 6"X 4" FROM TAIL STRIKE: CUT DAMAGED SKIN FOR ACCES S TO FRAME 70 DAMAGE EVALUATION.BLENDED DAMAGE ON FRAME.Apr 21, 2008 · N457UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA02303Unknown · smokeAVIONICS SMOKE DISPLAYED ON UPPER ECAM SCREEN, SMOKE CREW COMMENTS, AVIONICS SMOKE ECAM. S/O BLOWERS ETC. RESET, ECAM GONE, BUT WE STILL ODOR OF FAINT SMOKE. AVIONICS SMOKE ECAM. S-OBLOWERS ETC. RESET. ECAM GONE. BUT WE STILL SMELL FAINT SMOKE. INSPECTED Apr 20, 2008 · N466UA · Airbus A320232 · Air Distribution System
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