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 CALA2014032490678Unknown · leakingGROUND UNDER ENG 2 IS WET WITH WHAT APPEARS TO BE OIL, DROPS HANGING OFF ENG.Mar 24, 2014 · N472UA · Airbus A320232 · Turbine Engine Oil SystemSDR CALA2014032490680Fitting · gougedLT MLG DOOR FWD FITTINGS FWD & AFT LUGS GOUGED. R & R FWD FITTING.Mar 24, 2014 · N485UA · Airbus A320232 · Landing Gear DoorsSDR YENA20140324064Eec · failedAIRCRAFT DIVERTED. AFTER LEVELING AT CRUISE, STATUS PAGE SHOWED STATUS INOPERATIVE SYS, WHEN SLATS OUT, REVERSER 2, ENG 2 AT IDLE ENG 2 THRUST ON GROUND MAX POWER IDLE. STATUS INDICATING DISPLAYED BUT NO ECAM FAULTS DISPLAYED OR RECALLABLE. R & R NR 2 EEMar 24, 2014 · N598JB · Airbus A320232 · Fuel Controlling SystemSDR CALA2014032690695Stall Warning · activatedSTALL DISPLAYED ON UPPER ECAM SCREEN DURING STEADY STATE CLIMB OR CRUISE. ENG NOT SHUTDOWN, ENG 1. ENG 1 STALL ECAM NO OTHER INDICATIONS.Mar 24, 2014 · N453UA · Airbus A320232 · Engine Indicating SystemSDR CALA2014032490676Flap · faultedFLAP SYS FAULT AFTER TAKEOFF, RETURN TO FIELD.Mar 23, 2014 · N407UA · Airbus A320232 · Trailing Flap Position Indicating SystemSDR CALA2014032490679Target · faultyDOOR 2R SLIDE ARMED, INTERMITTENT DURING FLIGHT. LOST SLIDE INDICATION ON ECAM DOOR OXY PAGE. REPLACED DOOR ARMED SENSOR TARGET IAW PTT 2992009.Mar 23, 2014 · N458UA · Airbus A320232 · Emergency EquipmentSDR CALA2014032490681Stringer · corrodedCORROSION AFT CARGO PIT STRINGER 42L, FRAME 58 TO FRAME 59. R & R STRINGER 42L FROM FRAME 53 - 59 IAW SRM 51-42-11.Mar 23, 2014 · N485UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014032490683Seat Track · damagedCABIN SEAT TRACKS DAMAGED AT 13 LOCATIONS FROM SEAT FWD ATTACH POINTS.Mar 23, 2014 · N485UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2014032490682Stringer · corrodedCORROSION AFT CARGO PIT STRINGER 42L, FRAME 62 TO FRAME 63. R & R STRINGER 42L FROM FRAME 59 TO FRAME 64 IAW SRM 51-42-11.Mar 22, 2014 · N485UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014032090648Skin · damagedLT WING FUEL PANEL LANDING 540MB HAS FOUR EACH SCREW HOLES GOUGED. REWORKED HOLES & INSTALLED BUSHINGS IAW SRM 57-27-11 FIG 102 & 57-21-11 FG 201.Mar 19, 2014 · N479UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2014032090649Skin · damagedRT WING FUEL TANK PANEL 640MB LANDING HAS ONE HOLE DAMAGED. REWORKED HOLES & INSTALLED BUSHINGS IAW SRM 57-27-11 FIG 102 & 57-21-11 FG 201.Mar 19, 2014 · N479UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2014032090650Fitting · corrodedR2 DOOR AFT FRAME 68 & STRINGER 23 HAS CORROSION. REMOVED CORROSION & FABRICATED REPAIR FITTING & INSTALLED IAW SRM 53-41-12 FG 202.Mar 19, 2014 · N479UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014032090651Idg · malfunctionedGEN 1 DID NOT COME ON AT START UNTIL GEN SWITCH CYCLED, WHEN GEN 1 CYCLED DURING GND CHECKS, IT DID NOT COME ON FIRST TIME & SHOWED VOLTS. R & R NR 1 ENG IDG. OPERATIONS CHECK & LEAK CHECKED GOOD AMM 24-21-00-72 0-042.Mar 19, 2014 · N480UA · Airbus A320232 · AC Generator-AlternatorSDR CALA2014032090652Skin · crackedAT LOCATION Q A CRACK WAS FOUND ON FUSELAGE SIDE SHELL AT FRAME 35 & STRINGER 30L. CRACK WAS REPAIRED IAW ECRA 5330-04721.Mar 19, 2014 · N434UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2014032090653Unknown · malfunctionedNO EGT INDICATION ON APU START. CYCLED CB'S L41 & L42. ACCOMPLISHED NORMAL APU START WITH EGT, NORMAL, INDICATION.Mar 19, 2014 · N456UA · Airbus A320232 · APU Indicating SystemSDR CALA2014031990635Sill · corrodedL1 DOOR SILL FWD & AFT GIRT BAR FITTINGS HAVE CORROSION ALL AROUND FASTENER HOLES. REMOVED CORROSION FROM ALL BOLT HOLES IAW SRM 53-11-14 FG 108 & ALL WITHIN LIMITS. PERFORMED SPOT FACE ON ALL HOLES IAW SRM 53-11- 14 & HFEC AROUND HOLES IAW NTM 51-10-08 P 6Mar 16, 2014 · N485UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014031490608Skin Panel · saturatedLT ELEVATOR LOWER SKIN PANEL HAS TRAPPED WATER INDICATION 25.5, FROM INBD END & 7 FROM TE, AREA IS 3.5 IN DIAMETER. DRILLED WITNESS HOLES & FOUND NO EVIDENCE OF MOISTURE PRESENT. CLEANED & APPLIED REPAIR, SEALED & RESTORED FINISH IAW SRM 55-21-11PARA 5D, FIGMar 14, 2014 · N485UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014031990636Unknown · odorELECTRICAL SMELL MID CABIN UNLOADED ACFT & CHECKED CABIN ELEC EQUIP INCLUDING SEU, READING POWER SUPPLIES & LIGHTING BALLASTS. NO NOTED EQUIP INOPERATIVE SUCH AS LIGHTING OR PASSENGER PSU'S. OPERATED PACKS, CHECKED AIR QUALITY ABOVE CEILING PANELS & E & E Mar 14, 2014 · N494UA · Airbus A320232 · Air Distribution SystemSDR CALA2014031490604Stringer · corrodedFWD CARGO PIT, FWD STRINGER 43R HAS CORROSION AT FRAME 34. R & R STRINGER 43 RT FROM FRAME 30 TO FRAME 35 IAW SRM 51-42-11 P 7 & 24.Mar 13, 2014 · N480UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014031490605Web · corrodedAFT CARGO WEB BETWEEN FRAME 52 TO FRAME 56 & STRINGER 9R TO STRINGER 41R HAS CORROSION. R & R AFT CARGO WEB FRAME 52 TO FRAME 56 IAW SRM 57-42-11 P7 - 9.Mar 13, 2014 · N480UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014031490600Smoke Detector · defectiveSMOKE LAVATORY SMOKE DETECTOR DEFAULT. REPLACED LAVATORY A SMOKE DETECTOR IAW AMM 26-17-15 PG 400 ALL TESTS PASSED.Mar 12, 2014 · N439UA · Airbus A320232 · Smoke DetectionSDR USAA2014031100003Stator Vane · malfunctionedABORTED TAKEOFF FOR ENG 2 COMPRESSOR VANE FAULT AT 60KTS. RTO & RETURNED TO GATE. REPLACED ACTUATOR VARIABLE STATOR VANE IAW JOB CARDS 26P32075006 & 26P32075009.Mar 10, 2014 · N677AW · Airbus A320232 · Compressor Bleed ControlSDR CALA2014031090565Fmc · malfunctionedFLIGHT MANAGEMENT GUIDANCE COMPUTERS 1 & 2 ARE INOPERATIVE. RESET BOTH FLIGHT MANAGEMENT GUIDANCE COMPUTERS POWER 90 SEC ALL FUNCTIONS & DISPLAYS RESTORED.Mar 9, 2014 · N451UA · Airbus A320232 · Flight Management Computing Hardware SystemSDR CALA2014031090566Skin · corrodedFWD PIT HAS CORROSION AROUND FASTENERS ON INNER SURFACE OF SKIN. REMOVED .014 OF.071 SKIN.Mar 9, 2014 · N480UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2014031090567Skin · corrodedFWD PIT FWD FRAME 34 BETWEEN STRINGERS 42L & 40L, CORROSION AROUND FASTENERS ON INNER SURFACE OF SKIN. REMOVED .012 OF .071 SKIN.Mar 9, 2014 · N480UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2014031090568Skin · corrodedFWD PIT FWD FRAME 34 BETWEEN STRINGERS 42R & 41R HAS CORROSION AROUND FASTENERS ON INNER SURFACE OF SKIN. REMOVED .011 OF .091 SKIN.Mar 9, 2014 · N480UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2014031090569Sensor · faultedLANDING GEAR SENSOR FAULT ON DESCENT.Mar 9, 2014 · N463UA · Airbus A320232 · Landing Gear Position and WarningSDR CALA2014030790548Smoke Warning · false indicationAVIONICS SMOKE ECAM MESSAGE DISPLAYED AFTER STARTING FIRST ENG. REMAINED AFTER SECOND ENG STARTED. SHUTDOWN ENGS & RETURNED TO GATE. RESET AEVC SYSTEM, NO FAULTS FOUND, AEVC TESTED OK. RAN BOTH ENGS, NO MESSAGE OR FAULTS. NO SMOKE NOTED IN AVIONICS OR CARMar 6, 2014 · N466UA · Airbus A320232 · Smoke DetectionSDR YENA20140305050Eec · failedDURING LEVEL OFF AT 11,000FT, NR 1 ENGINE HAD RAPID, UNCOMMANDED ACCELERATION TO MCT THRUST. ECAM, AUTOFLIGHT, ATHR OFF, ENG 1 EPR MADE FAULT, ENG 1 FADEC A FAULT. CLEARED BRIEFLY, THEN RE OCCURED DURING APPROACH AND LANDING. PERIODIC LOSS OF ENG 1 FUEL FLOW Mar 5, 2014 · N624JB · Airbus A320232 · Fuel Controlling SystemSDR CALA2014030790536Frame · corrodedFWD CARGO PIT FWD FRAME 34 CORROSION AROUND FASTENERS ON STRINGER 42R. R & R STRINGER 42.Mar 5, 2014 · N480UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2014030790538Skin · wornNR 1 PYLON LOWER SURFACE WORN AT RIB FROM CNA SEAL. AREA WAS BLENDED IAW SRM51-73-00 WITH MAX WEAR OF .007 & WITHIN SRM54-51-12 FIGURE 103 LIMIT. INSTALLED ANTI CHAFING PLATE REPAIR IAW SRM 54-51-12 FIGURE 202.Mar 5, 2014 · N480UA · Airbus A320232 · Nacelle/Pylon, Plate/SkinSDR CALA2014030790539Skin · corrodedLT OVERWING REFUEL HOLE LANDING HAS MINOR CORROSION ON COMPLETE LANDING, 8.32 TOTAL SQ INCHES. CORROSION WAS REMOVED IAW SRM 51-74-00 & FLAP PEENED, PRECAUTIONARY IAW SR M51-29-11. WITHIN SRM 57-21-11 P244 PARA 5FD LIMIT OF .020, MAX MATERIAL REMOVED AT FWD EMar 5, 2014 · N480UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2014030790540Skin · corrodedRT OVERWING REFUEL HOLE LANDING HAS MINOR CORROSION ON COMPLETE LANDING, 8.32 TOTAL SQ INCHES. CORROSION WAS REMOVED IAW SRM 51-74-00 & FLAP PEENED PRECAUTIONARY IAW SR M51-29-11. WITHIN SRM 57-21-11 PAGE 244 PARA 5FD LIMIT OF .020, MAX MATERIAL LOSS WAS .01Mar 5, 2014 · N480UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2014030390507Connector · not seatedEMERGENCY LIGHT TEST FAILED ON 2 SERVICE. RE SEATED CONNECTOR ON LT EMERGENCY EXIT POWER SUPPLY, OPERATIONS CHECKED GOOD IAW 33-51-38.Mar 3, 2014 · N448UA · Airbus A320232 · Light System WiringSDR CALA2014030390506Seal · unsecureSEAL HANGING OUT OF NR 1 ENG REVERSER SHROUD. OPENED FAN COWL, ABLE TO MANUALLY EXTEND THE REVERSER ENOUGH TO RE SEAT THE BULB SEAL IN ITS TRACK. RETRACED REVERSER TO PROPER OPERATING POSITION, HCU IN NORMAL FUNCTION MODE. FAN COWLING CLOSED & SECURED, OK TMar 2, 2014 · N472UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2014030390508Unknown · malfunctionedAPU WILL NOT START, SECOND ATTEMPT TO START, NO GOOD. CYCLED APU CONTROL & ECB CB'S NO HELP. OK TO DEFER, APU INOPERATIVE IAW MEL 4910B.Mar 1, 2014 · N474UA · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR CALA2014030390509Actuator · faultyFWD FLIGHT ATTENDANT OXYGEN COMPARTMENT WILL NOT OPEN DURING MANUAL DROP TEST. REPLACED COMPARTMENT DOOR LATCH ACTUATOR.Mar 1, 2014 · N435UA · Airbus A320232 · Crew Oxygen SystemSDR CALA2014022790489Housing · wornRT MLG UPPER BEARING HOUSING RETAINING PINS HOLES, ALL 6 ARE WORN.Feb 27, 2014 · N447UA · Airbus A320232 · Main Landing GearSDR CALA2014022790494Stringer · corrodedSTRINGER 42L IN AFT CARGO COMPARTMENT IS CORRODED FROM FRAME 57 TO FRAME 60.Feb 27, 2014 · N480UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014022590465Door Frame · corrodedR2 DOOR AFT FRAME 68 & STATION 23 HAS CORROSION. REMOVED CORROSION, FABRICATED REPAIR FITTING & INSTALLED IAW SRM 53-41-12 FG 202.Feb 25, 2014 · N479UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2014022790493Unknown · smokeAFT CARGO SMOKE DISPLAYED ON UPPER ECAM. RAMP REPORTS SMOKE COMING FROM AFT CARGO.Feb 25, 2014 · N409UA · Airbus A320232 · Air Distribution SystemSDR CALA2014022590476Unknown · malfunctionedINITIAL APU START WAS SLOW WITH LP FUEL VLV FAULT, FAULT CLEARED. DUCT PRESS RECOVERED, ENG STARTS NORMAL, SYS RECOVERED. OPERATIONS NORMAL, OK TO CONTINUE.Feb 23, 2014 · N467UA · Airbus A320232 · APU Core EngineSDR CALA2014022590462Frame · damagedLT AVIONICS COMPARTMENT NLG DOG HOUSE CROSS BEAM FRAME 16 HAS ELONGATED SLOT ATTACH HOLE. REWORKED HOLE LT SIDE NLG COMPARTMENT BETWEEN LT AVIONICS DOOR & DOG HOUSE FAME 16. REAMED ELONGATED HOLE, FABRICATED & INSTALLED INSERT & REPAIRED WASHERS IAW ECRA 531Feb 22, 2014 · N479UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2014022590463Skin · gougedLT WING FUEL PANEL LANDING 540 MB HAS FOUR EACH SCREW HOLES GOUGED. HOLES REWORKED & BUSHING INSTALLED IAW A320 SRM 57-27-11 FIG 102 & 57-21-11 FG 201.Feb 22, 2014 · N479UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2014022590464Skin · gougedRT WING FUEL TANK PANEL 640MB LANDING HAS ONE HOLE DAMAGED. HOLE REWORKED & BUSHING INSTALLED IAW A320 SRM 57-27-11 FIG 102 & 57-21-11 FG 201.Feb 22, 2014 · N479UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2014022190410Light · malfunctionedEMERGENCY EXIT LIGHTING BY FWD 5 ROWS DID NOT COME ON WITH PWR LOSS. CYCLED EMERGENCY EXIT LIGHTS CONTROL CB & COMPLETED NORMAL CFDS LIGHTING TESTS. GREEN TEST PASSED DISPLAYED.Feb 20, 2014 · N444UA · Airbus A320232 · Emergency LightingSDR CALA2014022190413Yaw Damper · malfunctionedYAW DAMPER 1 INOPERATIVE AUTO FLT. CYCLED BREAKERS B 3 & 4, RESET FAC1. PERFORMED AFS TEST IAW MM22-96-00, CHECKED GOOD.Feb 19, 2014 · N409UA · Airbus A320232 · Autopilot SystemSDR CALA2014022190414Unknown · malfunctionedALTERNATE LAW PROT LOST DISPLAYED ON UPPER ECAM SCREEN, FLIGHT CONTROL. CYCLED BREAKERS B 3 & 4. PERFORMED AFS TEST IAW MM22-96-00, CHECKED GOOD.Feb 19, 2014 · N409UA · Airbus A320232 · Flight Control SystemSDR CALA2014022190415A/C Pack · faultedPACK 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, AIR. RESTARTED ENGS AT THE GATE. PACK 2 OPERATED NORMAL, NO FAULTS.Feb 19, 2014 · N409UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2014022190411Sill · corrodedR2 DOOR SILL HAS CORROSION AT FRAME 66, REPLACED R2 DOOR SILL.Feb 18, 2014 · N479UA · Airbus A320232 · Fuselage Miscellaneous Structure
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