IAE V2527-A5

Service difficulty reports · 8,009

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 CALA2016091995741Support Fitting · corrodedAFT CARGO FRAME 51, STRINGER 37R SUPPORT FITTING COMMON TO PROFILE PANEL WAS FOUND CORRODED. FITTING WAS REPLACED IAW SRM51-42-11.Sep 11, 2016 · N401UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016091995743Frame · damagedFRAME 51 INNER FLANGE DAMAGED BETWEEN STRINGERS 37 - 38R. REPAIRED IAW SRM53-00-12 TBL 201, PARA 4.A. FIG 201.Sep 11, 2016 · N401UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2016091995745Frame · damagedFRAME 51 INNER FLANGE DAMAGED BETWEEN STR 37R AND STR 38R. REPAIRED IAW SRM 53-00-12 TBL 201, PARA 4.A. FIG 201.Sep 11, 2016 · N401UA · Airbus A320232 · Fuselage Main, FrameSDR SOKF20160913008Carbon Seal · damagedDURING FLIGHT, THE ACFT DIVERTED DUE TO NR 2 ENGINE HAVING OIL LEAK AND WAS LANDED WITH 6.5 QT AND 10.5 WHEN SHUTDOWN, AT STATION PERFORMED TSM 79-30-00-810-806A AND FOUND SIGNS OF OIL LEAK FROM CARBON SEAL OF THE STARTER DRIVE. PERFORMED REPLACEMENT OF THE CSep 10, 2016 · N684TA · Airbus A320233 · Turbine Engine Oil SystemSDR CALA2016091995739Fitting · corrodedAFT CARGO BAY FRAME REINFORCEMENT FITTING COMMON TO THE PROFILE PANEL CORRODED, FRAME 52, STRINGER 37R. FITTING WAS REPLACED IAW SRM 51-42-11.Sep 10, 2016 · N401UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016091495729Skin · corrodedFWD CARGO BAY SKIN HAS CORROSION FRAME 33+3 BETWEEN STRINGERS 40 - 41R REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW A32053-21-11.Sep 7, 2016 · N401UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016091495730Stringer Splice · corrodedFWD CARGO BAY, FRAME 30+18 STRINGER SPLICE 42L CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11 PARA 6 AND 51-72-11.Sep 7, 2016 · N401UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016091495731Stringer · corrodedAFT CARGO BAY STRINGER 43L FLANGE HAS CORROSION BETWEEN FRAMES 53 - 54. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW 53-41-13. INSTALLED REPAIR IAW SRM 53-00-13 PARA 4 B FIG 202. SRI 53-00-13--2-002-00 TABLE 210.Sep 7, 2016 · N401UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016090895722Skin · corrodedEXTERNAL SKIN AT FRAME 69 HAS CORROSION AT WASTE TANK VENT. CUT OUT DAMAGED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-41-11 FIG 205.Sep 6, 2016 · N401UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2016090895723Web · corrodedAFT CARGO DOOR CUT-OUT THRESHOLD WEB AT FRAMES 53 - 56 CORRODED THROUGHOUT UPPER SURFACE. REMOVED AND REPLACED THE AFT CARGO DOOR THRESHOLD WEB IAW SRM53-42-11 PARA 6.Sep 6, 2016 · N401UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016090895725Strut · dischargedAIR TURNBACK DUE TO MLG SHOCK ABSORBER FAULT MESSAGE ON ECAM, NO RETRACTION. SWUNG NLG, NO FAULTS, GEAR SWING NORMAL. IAW TSM PERFORMED BOROSCOPE OF THE ALIGNMENT TANGS, FOUND ENGAGED AND NORMAL. FOUND NLG STRUT H DIMENSION APPROX ONE INCH LOW. SERVICED THE Sep 6, 2016 · N465UA · Airbus A320232 · Nose/Tail Landing Gear Strut/AxleSDR CALA2016090895726Power Supply · faultedDURING TEST, MESSAGE FOR LT FWD BATTERY. REPLACED POWER SUPPLY UNIT.Sep 6, 2016 · N421UA · Airbus A320232 · Emergency LightingSDR CALA2016090895727Connector · looseLIGHT OVER EMERGENCY EXIT WILL NOT SHUT OFF WITH REST OF LIGHTS. SECURED LOOSE CONNECTOR ON RT SIDE BALLAST, OPS OKSep 6, 2016 · N423UA · Airbus A320232 · Light System WiringSDR CALA2016090195708Shear Tie · corrodedFWD CARGO BAY AT FRAME 33 BETWEEN STRINGER 41 & 42R SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM51-42-11.Aug 31, 2016 · N449UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016090195709Shear Tie · corrodedFWD CARGO AT FRAME 33 BETWEEN STRINGERS 40 & 41R SHEAR TIE HAS CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM51-42-11.Aug 31, 2016 · N449UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016090195710Power Supply · malfunctionedEMERGENCY LIGHTS FAILED TEST . MESSAGE FOR EPSU BATTERY. RESET OVERWING LEFT POWER SUPPLY UNIT, RAN TEST AGAIN, NO FAULTSAug 31, 2016 · N495UA · Airbus A320232 · Emergency LightingSDR SOKF20160902006Servo Control · faultyDURING CLIMB, THE ACFT RETURN TO DEPARTURE DUE TO ECAM WARNING FLIGHT CONTROL ELAC 2 PITCH FAULT, AT STATION, PERFORMED TSM 27-93-00-810-867-A. R & R ELEVATOR SERVO CONTROL LT SIDE, 34 CE1 IAW AMM 27-34-51-000-001-A AND 27-34-51-400-001-A. ADJUSTMENT TEST OFAug 31, 2016 · N493TA · Airbus A320233 · Elevator Control SystemSDR CALA2016090195702Frame · corrodedFWD CARGO AT FRAME 32 BETWEEN STRINGERS 43L AND 43R HAS CORROSION ON THE SHEAR TIE. REPLACED THE SHEAR TIE IAW SRM 51-42-11.Aug 30, 2016 · N449UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2016090195703Stringer · corrodedFWD CARGO STRINGER 41R BETWEEN FRAMES 31 & 32 HAS CORROSION. REPLACED THE STRINGER IAW SRM 51-42-11.Aug 30, 2016 · N449UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016090195704Shear Tie · crackedFWD CARGO FRAME 29, STRINGER 43R - 43L SHEAR TIE HAS A CRACK. INSTALLED A NEW SHEAR TIE IAW SRM 51-44-11, SRM 51-42-11, AND SRM 53-21-12.Aug 30, 2016 · N449UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016090195705Door Sill · corrodedFRAME 68 CORROSION ON L2 DOOR SILL AROUND FAST HOLE. INSTALLED A NEW DOOR SILL IAW SRM 53-41-14, FIG 101, SH 1.Aug 30, 2016 · N401UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016090195706Door Sill · corrodedR2 DOOR SILL HAS HEAVY CORROSION AT AFT GIRT BAR FITTING. INSTALLED A NEW R2 DOOR SILL IAW SRM 53-41-14.Aug 30, 2016 · N401UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016083095700Warning Light · false activationRIGHT EMERGENCY EXIT OVERWING SLIDE LIGHT CAME ON DURING LANDING ROLLOUT. CHECKED THE EMERGENCY DOOR FOR SECURITY, ALL CLOSED AND SECUREDAug 28, 2016 · N417UA · Airbus A320232 · Door Warning SystemSDR CALA2016082695679Shear Tie · corrodedFWD CARGO AT FRAME 29, BETWEEN STRINGERS 42-43L SHEAR TIE HAS CORROSION. INSTALLED A NEW SHEAR TIE IAW SRM 51-42-11, AND SRM 53-21-12.Aug 26, 2016 · N449UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016082695680Shear Tie · corrodedFWD CARGO, CORROSION ON SHEAR TIE AT FRAME 31, BETWEEN STRINGERS 40-42R. INSTALLED NEW SHEAR TIE IAW SRM 53-21-12, AND SRM 51-73-00.Aug 26, 2016 · N449UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016082695681Shear Tie · corrodedFWD CARGO AT FRAME 31, STRINGERS 41-42R, SHEAR TIE IS CORRODED. INSTALLED A NEW SHEAR TIE IAW SRM 53-21-12, AND SRM 51-21-11.Aug 26, 2016 · N401UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016082695682Shear Tie · corrodedFWD CARGO AT FRAME 32, STRINGERS 41-42R SHEAR TIE IS CORRODED. INSTALLED A NEW SHEAR TIE IAW SRM 53-21-12, AND SRM 51-21-11.Aug 26, 2016 · N401UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016082695683Cleat · corrodedCORROSION ON CLEAT, FRAME 28, STRINGERS 43R-43L. INSTALLED NEW CLEAT IAW SRM 53-21-12, AND SRM 51-21-12.Aug 26, 2016 · N449UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016082695684Cleat · corrodedFWD CARGO AT FRAME 28 BETWEEN STRINGERS 42-43R HAS CORROSION ON CLEAT. INSTALLED NEW CLEAT IAW SRM 53--21-12, AND SRM 51-42-11.Aug 26, 2016 · N449UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016083095692Shear Tie · corrodedFWD CARGO BAY FRAME 28, STRINGERS 42 - 43R, SHEAR TIE HAS CORROSION. INSTALLED A NEW SHEAR TIE IAW SRMAug 26, 2016 · N449UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016083095693Slide · malfunctionedEMERGENCY LIGHTS TEST FAILED FOR EXTERNAL LOADS FAULTY AFT LT. L2 DOOR AND R2 DOOR SLIDES REPLACED IAW AMM 25-62-44.Aug 26, 2016 · N417UA · Airbus A320232 · Emergency EquipmentSDR CALA2016083095694Shear Tie · corrodedFWD CARGO BAY, SHEAR TIE CORRODED FRAME 30, STRINGERS 41 & 42R, REPLACED THE SHEAR TIE IAW SRM 51-42-11.Aug 26, 2016 · N449UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016083095695Shear Tie · corrodedFWD CARGO BAY AT FRAME 32, STRINGERS 42-43R, CORROSION ON SHEAR TIE. INSTALLED NEW A SHEAR TIE IAW SRM 53-21-12, AND SRM 51-72-11.Aug 26, 2016 · N449UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2016083095696Shear Tie · corrodedFWD CARGO BAY FRAME 32, STRINGERS 41 - 42R HAS CORROSION ON SHEAR TIE. INSTALLED NEW SHEAR TIE IAW SRM 53-21-12, AND SRM 51-72-11.Aug 26, 2016 · N449UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016083095698Battery Pack · no testLEFT OVERWING EMERGENCY LIGHT BATTERY FAULT DURING 2SVC, REPLACED THE BATTERY, TEST PASSEDAug 26, 2016 · N442UA · Airbus A320232 · Emergency LightingSDR CALA2016082695685Engine · stalledAT FL 360, ECAM INDICATION LEFT ENGINE STALLED. DIVERTED, ENGINE DISPLAYED STALL INDICATIONS TWICE AT ALTITUDE BUT PERFORMED NORMAL REST OF FLIGHT. TROUBLESHOOT IAWTSM. REPLACED EEC AS A PRECAUTION. LEAK CHECK AND PURGE OF PB SENSE LINE, INSPECTED FOR DEAug 25, 2016 · N406UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2016082695689Light · malfunctionedCABIN EMERGENCY LIGHTS TESTED WITH A FAULT MESSAGE. RESET SYSTEM, ALL CHECKED GOODAug 25, 2016 · N416UA · Airbus A320232 · Emergency LightingSDR CALA2016082695688Light · malfunctionedCABIN EMERGENCY LIGHTS CAME ON FOR 8 MINUTES. OCCURRED SAME TIME AS CABIN PRESSURIZED. GROUND CHECKED NORMALAug 24, 2016 · N422UA · Airbus A320232 · Emergency LightingSDR CALA2016082695690Switch · stickingAFT ATTENDANT EMERGENCY LIGHT TEST SWITCH STICKS IN ON POSITION. REPLACED THE PANEL, GROUND TESTED, NO DEFECTS.Aug 24, 2016 · N428UA · Airbus A320232 · Emergency LightingSDR CALA2016082395677Control Panel · malfunctionedAFT ATTENDANT EMERGENCY LIGHT TEST SWITCH STICKS IN ON POSITION. REPLACED THE CONTROL PANEL . GROUND TEST OK, NO DEFECT NOTED IAW 23-00-00.Aug 23, 2016 · N428UA · Airbus A320232 · Emergency LightingSDR CALA2016082695691Light · inoperativeEMERGENCY LIGHT TEST FAILED. REPLACED L1 SLIDE.Aug 23, 2016 · N428UA · Airbus A320232 · Emergency LightingSDR CALA2016082395664Stringer Splice · corrodedFWD CARGO BAY FRAME 30+18, STRINGER 41L SPLICE CORRODED. REMOVED DAMAGED STRINGER SPLICE AND INSTALLED NEW IAW SRM 51-42-11.Aug 22, 2016 · N401UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016082395667Door Sill · corrodedR2 DOOR SILL CORRODED AT FRAME 68. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11.Aug 22, 2016 · N449UA · Airbus A320232 · Fuselage Structure (General)SDR AALA201608239006Engine · smokeAIRCRAFT WAS GROUNDED, HEAVY SMOKE COMING OUT OF NR 1 ENGINE TAIL PIPE AT SHUTDOWN. REPLACED NR 1 ENGINE IAW TASK CARD 26L40071004 AND 26L00071015.Aug 22, 2016 · N651AW · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2016082395665Door Sill · crackedBELOW DOOR R2 DOOR SILL, FRAME 67 CRACKED AT DOOR SILL ATTACH POINT. REMOVED DAMAGED FRAME. MANUFACTURED NEW FRAME IAW DWG D53480076 & INSTALLED IAW SRM 51-42-11.Aug 21, 2016 · N401UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016082395666Skin · dentedEXTERNAL FUSELAGE SKIN DENTED 2 FT AFT OF THE L2 DOOR. DENT FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE & INSTALLED EXTERNAL DOUBLER IAW SRM 53-41-11.Aug 21, 2016 · N401UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016082395672Door Sill · corrodedAFT CARGO DOORWAY INNER SILL WEB CORRODED, FR52-F R56. REMOVED DAMAGED WEB. INSTALLED NEW INNER SILL WEB IAW A320 SRM 51-42-11.Aug 21, 2016 · N449UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016082395675Door Sill · corrodedAFT CABIN WET AREA R2 DOOR SILL HAS CORROSION AT AFT GIRT BAR FITTING. REMOVED DAMAGED SILL. INSTALLED NEW DOOR SILL IAW SRM 51-42-11.Aug 21, 2016 · N417UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016082395676Door Sill · corrodedR2 DOOR SILL LOWER FWD FRAME AT FRAME 66 HAS CORROSION ON FRAME WEB FACE & AROUND NUTPLATE. BLENDED CORROSION AND IS OUT OF LIMITS. CUT OUT CORRODED AREA IS 1.4 INCH WIDE & 1.3 INCH TALL & INSTALLED A RPR FITTING IAW SRM 53-41-12 FIG 202. SRI 53-41-12 -2-002Aug 21, 2016 · N417UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016082395668Frame · damagedFRAME 67 HAS OUT OF ROUND HOLES AT STRINGERS 23 - 32R. INSTALLED A NEW FRAME AND SPLICE IAW SRM 51-72-11, & 51-42-11.Aug 20, 2016 · N449UA · Airbus A320232 · Fuselage Structure (General)
Back to IAE V2527-A5