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 UALA2008120106686Frame · damagedAFT PRESSURE BULKHEAD FRAME (LWR) IS CREASED AT FR70 BETWEEN STR 42L AND STR 43R. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME.Nov 26, 2008 · N448UA · Airbus A320232 · Fuselage Main, FrameSDR UALA2008120106687Frame · damagedTWENTY ONE (21) STRINGERS CUT FOR REMOVAL ACCESS TO REAR PRESSURE BULKHEAD LOWER FRAME 70 SECTION 5.25 INCHES AFT OF FRAME 70 BETWEEN STRINGERS 24L AND STRINGER 24R. MAJOR REPAIR ACP'D: ALL STRINGERS REINSTALLED.Nov 26, 2008 · N448UA · Airbus A320232 · Fuselage Main, FrameSDR UALA2008112506665Plate · corrodedSHEAR PLATE AFT OF DOOR 2R LOCATED BETWEEN FRAMES 69 AND 70 HEAVILY CORRODED. CONTINUED INSTALLATION OF SHEAR PLATE.Nov 25, 2008 · N403UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2008112406641Light · missingSEAT 4A IS MISSING ONE OF TWO SEAT MOUNTED ELECTROLUMINESCENT. RELAMPED 4A, OPS CHECK OKAY.Nov 24, 2008 · N486UA · Airbus A320232 · Emergency LightingSDR UALA2008112406642Lanyard · out of positionLT OVERWING EXIT, EMERGENCY EXIT SIGN INOP. LENS LANYARD OBSTRUCTING ELECTRICAL CONNECTION RE-ADJUSTED. OPS CHECK OK.Nov 24, 2008 · N461UA · Airbus A320232 · Emergency LightingSDR UALA2008112506664Battery Pack · inoperativeFWD BATTERY PACK INOP ON PSU 10WL. REPLACED BATTERY PACK, CHECKED OK.Nov 24, 2008 · N486UA · Airbus A320232 · Emergency LightingSDR UALA2008112406631Wire Harness · shortedEMERGENCY LIGHTS FAIL TEST. SHOWS EPSU INT LOAD EMER L. FOUND SHORT O GROUND CONNECTOR 11WL SOCKET "T" REF AWM 33-51-04, CHASING WIRES. FOUND HARNESS SHORTED AT SEAT 22. REPLACED LIGHT ASSY, CHECKED OK.Nov 23, 2008 · N486UA · Airbus A320232 · Light System WiringSDR UALA2008112406632Plate · corrodedPLATE UNDER SHEAR PLATE LOCATED BETWEEN FRAME 69 AND 70 RIGHT SIDE OF AIRCRAFT CORRODED. REMOVED PLATE AND FWD ATTACH ANGLE.Nov 23, 2008 · N403UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2008112406638Bottle · low pressureTHE 2R DOOR ASSIST BOTTLE PRESS LOW. SERVICED BOTTLE.Nov 23, 2008 · N461UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2008112406656Valve · faultyPRESSURIZATION PROBLEM. RTFL. REPLACE SKIN OUTLET VALVE 22HQ, AEVC COMPUTER 10HQ AND NR 2 SDAC. OPS CHECKS NORMAL.Nov 23, 2008 · N482UA · Airbus A320232 · Cabin Pressure Control SystemSDR UALA2008112406630Bulkhead · bentAFT PRESSURE BULKHEAD WEB AT FR70 IS BENT BETWEEN STRINGERS 42L TO 43R, (K8847B). MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED AFT PRESSURE BULKHEAD LOWER CENTER SECTION WEB BETWEEN STR 42L & 43R.Nov 22, 2008 · N448UA · Airbus A320232 · Fuselage Main, BulkheadSDR UALA2008112406645Doubler · crackedLT DOOR SILL DOUBLER OUTBOARD HAS 2 CRACKS (MARKED). MAJOR REPAIR ACCOMPLISHED. REPLACED SILL SHAPE (DOUBLER), AT DOOR 2L.Nov 22, 2008 · N403UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2008112406647Floorbeam · corrodedFLOORBEAM 200 HAS TWO SMALL SPOTS OF CORROSION (MARKED). MAJOR REPAIR ACCOMPLISHED. STARTED REPLACING BEAM.Nov 22, 2008 · N403UA · Airbus A320232 · Fuselage Main, Floor BeamSDR UALA2008112406617Skin · damagedMAJOR REPAIR. REPLACE BELLY SKIN FR 64-70 STR 40R-31L ACCT TAIL STRIKE ON LANDING. MAJOR REPAIR ACCOMPLISHED. REMOVED AFT POTABLE WATER SERVICE PANEL. REMOVED & REPLACED DAMAGED SKIN WITH HEAT TREATED FASTENERS WHERE REQUIRED. 11/24/2008 REINSTALLED POTABNov 21, 2008 · N448UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2008112406644Sill · corrodedRT AFT DOOR SILL HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED 2R DOOR SILL. PICKING UP FASTENER HOLES, STARTED ASSY CLIPS AND PARTS. ASSEMBLED CLIPS AND CORNER CASTINGS, AND SERRATED PLATES TO SILL PAN. INSTALLED FASTENERS IN UPPER ROW OF SKIN, AND FNov 21, 2008 · N403UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2008112406646Sill · corrodedLT DOOR SILL HAS SEVERAL AREAS OF CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SILL SHAPE FROM SILL PLATE AT DOOR 2L. INSTALLED NEW SILL SHAPE ON SILL PLATE. NEEDS 2 FASTNERS DRILLED AND INSTALLED ON SHAPE. REPLACED 3 FASTENERS ON SILL SHAPE. RNov 21, 2008 · N403UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2008111806544Filter · dirtyELECTRICAL BURNING ODOR IN COCKPIT. RTFL. AFTER CONFER WITH CAPT, REMOVED CAPTS SIDE PFD & ND, CHECKED AREA FOR ELECT BURN ODOR & DAMAGE, NONE FOUND, EQUIPT COOLING NORMAL. REPLACED AND TESTED CRTS, CKS GOOD. FOUND AVIONICS COOLING FILTER HEAVILY SOILED. Nov 17, 2008 · N423UA · Airbus A320232 · Air Distribution SystemSDR UALA2008111806550Plate · corrodedSKID PLATES FOUND FLOOR PANELS DELAMINATED. CORROSION FOUND UNDER FLOOR PANELS.Nov 17, 2008 · N424UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2008111706542Warning System · activatedGEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM SCREEN - L-G.Nov 16, 2008 · N409UA · Airbus A320232 · Landing Gear Position and WarningSDR UALA2008111706522Microphone · faultyCAPT OXYGEN MASK MIKE IS WEAK, UNREADABLE ACCORDING TO ATC. REPLACED O2 MASK.Nov 14, 2008 · N466UA · Airbus A320232 · Audio Integrating SystemSDR 2008UALA06494Slide · defectiveEMERGENCY LIGHT TEST FAILED EXT LOAD L, TESTED AND FOUND DOOR 1R SLIDE PACK AT FAULT. REMOVED DOOR 1R SLIDE. REPLACED SLIDE. STILL HAVE ORIGINAL PROBLEM FAILED EXT LOAD L. VERIFIED ALL EMERGENCY LIGHTS ARE OPERATIVE EXCEPT DOOR 1R SLIDE LIGHTS. ACCMP EMERNov 12, 2008 · N415UA · Airbus A320232 · Escape SlideSDR 2008UALA06472Sill · corrodedDOOR 2R SILL PLATE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED DOOR 2R SILL PLATE.Nov 11, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06473Structure · corrodedRT SHEAR TRAY HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. TRAY REPLACED. Nov 11, 2008 · N404UA · Airbus A320232 · Passenger/Crew DoorsSDR 2008UALA06474Beam · corrodedBEAM 205 HAS CORROSION AT FRAME 68. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. REMOVED BRACKETS AND TRANSFER DRILLED ONTO NEW BEAM. CONNECTED BEAM 205 TO BEAM 200. READY TO INSTALL IN AC. INSTALLED BEAM.Nov 11, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06482Beam · corrodedRT BEAM LABELED - Y1292 HAS CORROSION AT FR66 AND IS MARKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED BEAM TO AIRCRAFT. NEEDS SUPPORTS BETWEEN FR64 - FR65 INSTALLED.Nov 11, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06483Skin · dentedAPPROX STA 1325 FRAME 74 + 5 INCHES, 10 INCHES TO THE RIGHT OF THE BELLY CENTER LINE IS DENTED. DRESSED OUT DENT, NDT INSP FOR FURTHER DAMAGE INSIDE AND OUTSIDE OF SKIN, NO CRACKS DETECTED. PAINT TO MATCH REWORK AREA.Nov 11, 2008 · N423UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA06497Structure · crackedRT TRAY (AFT OF DOOR 2R) IS CRACKED AND MARKED. FABRICATED TRAY FROM 2024T3.063 THICK. INSTALLED TRAY.Nov 11, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06470Threshold · corrodedRT DOOR 2R THRESHOLD CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. STARTED REMOVING FASTENERS. REMOVED DOOR SILL AND STARTED TO MFG NEW SILL. INSTALLING FASTENERS. CONTINUED INSTALLING FASTENERS AND MFG NEW FWD SPLICE ANGLES. INSTALLING FASTENERS, SNov 9, 2008 · N404UA · Airbus A320232 · Passenger/Crew DoorsSDR 2008UALA06429Shear Plate · corrodedRIGHT AFT SHEAR PLATE CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REPLACED RT AFT SHEAR PLATE.Nov 8, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06430Support · corrodedRT AFT SHEAR PLATE SUPPORT HAS CORROSION ON BOTTOM SIDE. SUPPORT NEEDS REPLACED. MAJOR REPAIR ACCOMPLISHED. REPLACED RT AFT SHEAR PLATE SUPPORT.Nov 8, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06432Wire · brokenEMERGENCY EXIT LIGHTING INOP SEAT ROWS 12, 13 AND 14. BROKEN WIRE FOUND AT 13ABC. REPAIRED BROKEN WIRE. OP CHECKS GOOD.Nov 8, 2008 · N419UA · Airbus A320232 · Light System WiringSDR 2008UALA06433Cover · missingTHE 6ABC EMERGENCY EXIT PATH LIGHT COVER MISSING. REPLACED LENS COVER FOR SEAT 6C EMERGENCY EXIT PATH LIGHT.Nov 8, 2008 · N419UA · Airbus A320232 · Emergency LightingSDR 2008UALA06406Beam · corrodedBEAM 200 HAS CORROSION AT FRAME 67. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. REMOVED BRACKETS AND TRANSFER DRILLED ONTO NEW BEAM. CONNECTED BEAM 200 TO BEAM 205. READY TO INSTALL IN ACFT. INSTALLED BEAM 200 TO ACFT.Nov 7, 2008 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2008UALA06410Attach Fitting · disconnectedFOUND DOOR 1L SLIDE UPPER AFT ATTACH FITTING DISCONNECTED (SPRING TYPE). REPLACED FITTING.Nov 7, 2008 · N401UA · Airbus A320232 · Escape SlideSDR 2008UALA06425Shear Plate · crackedLT TRAY AFT OF DOOR 2L CRACKED AND MARKED. MAJOR REPAIR ACCOMPLISHED. FINISHED DRILLING NEW SHEAR PLATE AND STARTED INSTALLING. INSTALLED REMAINING FASTENERS LT TRAY AFT OF DOOR 2L. ACCOMPLISHED INSPECTION OF FASTENER INSTALLATION.Nov 7, 2008 · N404UA · Airbus A320232 · Passenger/Crew DoorsSDR 2008UALA06402Slide · faultyEMERGENCY LIGHTS FAILS TEST. FAULTS EXT LOAD AFT L. REPLACED DOOR 2L SLIDE.Nov 6, 2008 · N433UA · Airbus A320232 · Escape SlideSDR 2008UALA06403Stringer · damagedFUSE STR 43RT AT FR67 + 2 HAS EXCESSIVE MAT'L LOSS FROM GRINDING. MAJOR REPAIR. STRINGER TO BE REPLACED.Nov 6, 2008 · N448UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2008UALA06405Stringer · damagedDAMAGE FOUND AT FRAME 69 STRINGER 20 DIMENSION ARE D=.030 A=.500 B=.311 OF STRINGER 20. CREASE IS ON STRINGER. SIZE OF DENT IS 2 INCH BY 2 INCH BY .030 DEEP. THIS IS AFT OF DOOR 2LT. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER 20 NEAR FRAME 69. ANov 6, 2008 · N426UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2008111306403Stringer · damagedFUSELAGE STR 43RT AT FR67 + 2 HAS EXCESSIVE MAT'L LOSS FROM GRINDING. MAJOR REPAIR. STRINGER TO BE REPLACED. REPLACE BELLY SKIN FRAME 64-70 STR 40R-31L. REMOVED DAMAGED STRINGER & REPLACED WITH NEW.Nov 6, 2008 · N448UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR 2008UALA06375Floorbeam · corrodedBEAM 235 HAS CORROSION AT AFT END OF FRAME 68. REMOVED FASTENERS BEAM STILL NEEDS REMOVED. REMOVED BEAM 235. NEW BEAM IS ON BENCH AND IS DRILLED OUT, MOUNTS ARE HELD IN PLACE. PLACED SEALANT AND HARDWARE BY BEAM. REPLACED BEAM.Nov 5, 2008 · N404UA · Airbus A320232 · Fuselage Main, Floor BeamSDR 2008UALA06370Battery · dischargedFAILED EMERGENCY LIGHT SYSTEM TEST REF MM 33-51-00-710-001. MESSAGE: EMER SYSTEM ATA 33-51-38 BATTERY EMER R. REPLACED BATTERY FOR RIGHT MID CABIN. OP'S CHECK GOOD. EMER LIGHT SYS TEST PASSED.Nov 4, 2008 · N427UA · Airbus A320232 · Emergency LightingSDR 2008UALA06354Line · leakingACRID SMELL RETURNED ON TAKEOFF AND CLIMB GOT BETTER AT ALTITUDE NOW JUST MILD. SMELL GETS BETTER WITH CABIN FANS OFF AND PACK IN HIGH FLOW. FOUND BRAIDED OIL LUBE LINE AFT SIDE OF GEARBOX ON APU LEAKING OIL INTO AREA OF APU INLET, AND CAUSING OIL SMELL. ACNov 1, 2008 · N447UA · Airbus A320232 · APU Oil SystemSDR UALA2008111306354Line · leakingACRID SMELL RETURNED ON TAKEOFF AND CLIMB GOT BETTER AT ALTITUDE NOW JUST MILD. SMELL GETS BETTER WITH CABIN FANS OFF AND PACK IN HIGH FLOW. FOUND BRAIDED OIL LUBE LINE AFT SIDE OF GEARBOX ON APU LEAKING OIL INTO AREA OF APU INLET, AND CAUSING OIL SMELL. ACNov 1, 2008 · N447UA · Airbus A320232 · APU Oil SystemSDR 2008UALA06309Unknown · odorELECTRICAL SMELL IN CABIN. FLIGHT DIVERTED.Oct 30, 2008 · N480UA · Airbus A320232 · Air Distribution SystemSDR 2008UALA06319Skin · damagedFOUND LIGHTNING STRIKE HOLE THROUGH SKIN ABOVE F/O STATIC PORT, REQUIRES PLUG REPAIR. STRINGER HAS DAMAGE WILL REQ REPLACEMENT.Oct 29, 2008 · N441UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR 2008UALA06320Smoke Detector · faultySMOKE LAV & CARGO DET FAULT MESSAGE PRESENT ON UPPER ECAM BY. REPLACED DETECTOR 1WQ, VERIFIED NO FAULTS, OP CHECKS OK.Oct 29, 2008 · N474UA · Airbus A320232 · Smoke DetectionSDR USAA920081989Eec · failedFLT NR 245 BWI-PHX EMERGENCY LANDING CREW REPORTED LOSS OF POWER EXPERIENCED ON NR 2 ENGINE SEVERAL TIMES. ECAM INDICATED ENG 2 STALL. THERE WAS NO ASSOCIATED NOISE OR FAILURE. CREW DECLARED AN EMERGENCY AND RETURNED TO BWI LANDING WITHOUT INCIDENT. ECAM IOct 29, 2008 · N662AW · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2008UALA06295Engine · fireNR 1 ENG - FIRE IN TAIL PIPE AFTER SHUTDOWN. SUSPECT OIL LEAK.Oct 28, 2008 · N449UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR UALA2008111306295Seal · defectiveNR 1 ENGINE REPORTED FIRE IN TAIL PIPE AFTER SHUTDOWN. SUSPECT OIL LEAK AS SOURCE OF IGNITION. REPLACED NR 1 ENGINE. REPLACED SEAL NR 5 BEARING/ASSY. REPLACED NR 5 BEARING COMPARTMENT PULLER/COVER.Oct 28, 2008 · N449UA · Airbus A320232 · Turbine Engine Oil SystemSDR 2008UALA06275Skin · damagedFRAME 67 TO FRAME 71 AND FROM STR 42R TO STR 42L HAS DAMAGE. REPAIR WAS MADE FROM FRAME 67 TO FRAME 71 AND FROM STR 42R TO STR 42L. RAS-DAHAM-4800505-2008 ISSUE C RELEASED 25SEP08 APPROVING THIS REPAIR AS PERMANENT. Oct 23, 2008 · N457UA · Airbus A320232 · Fuselage Main, Plate/Skin
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