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 CALA2014122392835Warning System · false activationPACK 1 REG FAULT DISPLAYED ON UPPER ECAM SCREEN. DURING INITIAL CLIMB SYS APPEARED NORMAL. FAULT FOR NR 1 PACK NO LONGER DISPLAYED. NR 1 PACK RAM AIR DOOR CYCLES WITH PACKS ON.Dec 14, 2014 · N428UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2014122392842Skin · damagedRIGHT ELEV UPPER SKIN PANEL HAS TRAPPED WATER INDICATION IN 3 LOCATIONS. 133 INCHES FROM INBD END, 16 INCHES FROM TE & 2 INCHES IN DIAMETER. NEXT, 131 INCHES FROM INBD END, 10 INCHES FROM TE & 2 INCHES X 3 INCHES DIAMETER. LAST 117 INCHES FROM INBD END, 12Dec 13, 2014 · N446UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014121292827Warning System · false activationDIVERT TO PIT DUE LT REVERSER LIGHT EN ROUTE. ECAM FAULT ENG 2 REVERSER IAW AMM 78-31-00-710-041-A FOR CFDS OPERATIONAL TEST OF REVERSER. REVERSER FAULT CLEARED AT ENG SHUTDOWN ON ARRIVAL. ACCOMPLISHED OPERATIONAL REVERSER CHECK VIA CFDS. BOTH A & B CHANNEDec 9, 2014 · N466UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2014120992814Wire · brokenEMERGENCY LIGHT TEST FAILS WHILE ACCOMPLISHING SVC MSG, EXT LOAD AFT L FAILS. REPLACED BROKEN WIRE BETWEEN 2873VC PIN B & 2961VCA PIN K. WIRE BROKEN ON DOOR WHERE HINGE ARM CONNECTS TO DOOR. OPERATIONS CHECKED OK IAW AMM 33-51-00-710-001A.Dec 7, 2014 · N407UA · Airbus A320232 · Light System WiringSDR CALA2014120992809Door Sill · corrodedL2 DOOR SILL HAS CORROSION AT TWO EACH NUTPLATES AT FRAME 68. INSTALLED REPAIR IAW SRM 53-41-14 FIG 201 SHEET 3 REPAIR PRINCIPLE 4.Dec 6, 2014 · N447UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014120592794Skin · damagedMAJOR REPAIR & SDR. RT WING FUEL TANK PLATE 640JB LANDING HAS 1 EACH OUT OF ROUND FASTENER HOLE. REPAIRED HOLE IAW SRM 57-27-11 & SRM 57-21-11 PARA 5B.Dec 3, 2014 · N498UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2014120592795Skin · damagedMAJOR REPAIR & SDR. LT WING FUEL TANK ACCESS DOOR CUT OUT 540MB HAS 1 EACH ELONGATED HOLE. REPAIRED HOLE B IAW SRM 57-27-11 & SRM 57-21-11 PAGES 210 - 220 PARA 5B.Dec 3, 2014 · N498UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2014120292761Skin · damagedLEFT WING FUEL TANK ACCESS DOOR CUT OUT 540 LB HAS 5 OVERSIZED HOLES. REWORKED HOLES P, Q & R IAW SRM 57-21-11 PARA B & THE OTHER TWO HOLES L & K WORK IAW ECRA 5720-02620. ALL HOLES REAMED & HFEC ROTARY SCANNED IAW NTM 51-10-01 & NO DEFECT NOTED. COLD WORKENov 30, 2014 · N498UA · Airbus A320232 · Wing, Plate/SkinSDR CALA2014120292756Charger · inoperativeA CHECK TASK 23 ON JIC 4-2015 CABIN EMER LIGHTING CHECK FAILED ON THE CIDS PANEL. DISPLAYS EPSU BATTERY EMER RT. CHANGED THE BATTERY CHARGER ASSOCIATED WITH THIS FAULT IAW MM33-51-38. OPERATIONS CHECK IS GOOD. CIDS IS CLEAR OF ALL FAULTS AT THIS TIME.Nov 28, 2014 · N464UA · Airbus A320232 · Emergency LightingSDR YENA20141125265Actuator · failedDURING FINAL APPROACH , FIX AND ACFT FULLY CONFIGURED AT APPROACH SPEED, ENG 2 COMPRESSOR VANE FAULT AT APPROXIMATELY 2000 FT MSL. ENG 2 STALL FAULT WITH AUDIBLE ENGINE STALLS IN COCKPIT FOLLOWED BY ENG 2 FAIL. SHUTDOWN ENGINE 2 IAW ECAM AND WITH ENGINE 2 SECNov 25, 2014 · N706JB · Airbus A320232 · Compressor Bleed ControlSDR CALA2014112892747Skin Panel · damagedMAJOR REPAIR & SDR. LEFT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION AT 5 LOCATIONS AS FOLLOWS. 1) 16 INCHES FROM INBD, 17 INCHES FROM TE & 1.5 INCHES IN DIAMETER. 2) 73 INCHES FROM INBD, 21 INCHES FROM TE & 3.5 INCHES X 8 INCHES UNDER LIGHTNING Nov 25, 2014 · N451UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014112492744Hydraulic System · lowHYDRAULIC GREEN SYS LOW LEVEL DISPLAYED ON UPPER ECAM SCREEN. SERVICED HYDRAULICS IAW AMM 29-31-00-710-001-A. TAXI RUN ACCOMPLISHED, ALL NORMAL.Nov 24, 2014 · N422UA · Airbus A320232 · Hydraulic System, MainSDR CALA2014112492726Wire · damagedEMERGENCY LIGHT SYS NOT TESTING AT FAP. WIRE 5026-PF22 SPLICED APPROX 12 INCHES FWD OF CONNECTOR 120RH-A, STATION 700 LT SIDE BEHIND FWD LAVATORY ACCESS PANEL IAW ESPM 20-48-21 & AWM33-51-01.Nov 19, 2014 · N418UA · Airbus A320232 · Light System WiringSDR USAA2014112000007Scavenge Pump · leakingFLIGHT DIVERTED & AN EMER DECLARED DUE TO CABIN ODOR & A CTR FUEL TANK TRANSFER ISSUE. CLIMBING THROUGH 15,000FT FLIGHT ATTENDANT REPORTED A STRONG DIRTY SOCKS SMELL. ACCOMPLISHED JOB CARD 26L00021001, FOUND NR 2 ENG OIL LEAK IN NR 5 BEARING AREA. EXCESSIVENov 18, 2014 · N664AW · Airbus A320232 · Turbine Engine Oil SystemSDR CALA2014112492729Threshold · corrodedAFT CARGO DOORWAY THRESHOLD CORRODED FRAME 52 - 56 AT STRINGER 38R. REPLACED AFT CARGO THRESHOLD FROM FRAME 52 - 56 IAW SRM 51-42-11.Nov 18, 2014 · N496UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014112492732Stringer · corrodedAFT CARGO COMPARTMENT AT FRAME 56, STRINGER 4L CORRODED. SPLICED IN NEW STRINGER SECTION IAW SRM 53-00-13 FIG 201.Nov 17, 2014 · N498UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014112492733Stringer · corrodedFORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER 43L AROUND RIVET HOLE AS MARKED 1 TO 4 INCHES FWD OF FRAME 34. R & R WITH NEW STRINGER FROM FRAME 31 - 35 IAW SRM 51-42-11.Nov 17, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014112492734Door Sill · corrodedR2 LOWER DOOR SILL CORRODED BEYOND LIMITS IAW SRM 5 3-41-14. REMOVED DOOR SILL & INSTALLED NEW DOOR SILL IAW SRM 51-42-11.Nov 17, 2014 · N498UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014112492735Stringer · corrodedFORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER 43R AROUND RIVET HOLES AS MARKED 1 TO 4 INCHES FWD OF FRAME 34. R & R WITH NEW STRINGER FROM FRAME 30 TO 35 IAW SRM 51-42-11.Nov 17, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014112492736Stringer · corrodedFORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER AROUND RIVET HOLES AS MARKED 1 TO 6 INCHES FWD OF FRAME 34. R & R STRINGER 44 FROM FRAME 30 & 31 TO END FITTING AT FRAME 35 IAW SRM 5 1-42-11.Nov 17, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014112492738Skin Panel · damagedLEFT ELEVATOR UPPER SKIN PANEL HAS WATER INGRESS INDICATION AT 11.5 INCHES FROM INBD END, 5.0 INCHES FROM TE, 3.5 INCHES IN DIAMETER & AT 28 INCHES FROM INBD END, 8 INCHES FROM TE, 3 INCHES IN DIAMETER. CUT OUT TRAPPED WATER INDICATION IN BOTH AREAS APPLIED RNov 17, 2014 · N498UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014112892746Skin Panel · damagedLEFT ELEVATOR UPPER SKIN PANEL HAS WATER INGRESS INDICATION AT 11.5 INCHES FROM INBD END, 5.0 INCHES FROM TE, 3.5 INCHES IN DIAMETER & AT 28 INCHES FROM INBD END 8 INCHES FROM TE & 3 INCHES IN DIAMETER. CUT OUT TRAPPER WATER INDICATION IN BOTH AREAS APPLIED RNov 17, 2014 · N498UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014111492703Stringer · corrodedAFT CARGO FLOOR RT SIDE AT FRAME 63 TO 64 STRINGER 42 RT HAS CORROSION. R & R WITH NEW FACTORY STRINGER 42 RT FROM FRAME 60 TO 64 IAW SRM 51- 42-11.Nov 13, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014111492704Stringer · corrodedAFT CARGO FLOOR LT SIDE AT FRAME 63 TO 64 STRINGER 41 LT HAS CORROSION. R & R WITH NEW FACTORY STRINGER 41 LT FROM FRAME 60 TO 64 IAW SRM 51- 42-11.Nov 13, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014111492705Stringer · corrodedFORWARD CARGO INNER AFT BILGE AREA HAS CORROSION ON STRINGER 24L AROUND RIVETS HOLES AS MARKED 4 TO 8 INCHES FWD OF FRAME 34. R & R WITH NEW FACTORY STRINGER 24 LT FROM FRAME 30 TO 34 IAW SRM 51-42-11.Nov 13, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014111492698Skin · crackedFUSE SKIN FRAME 35 & CM 10 THE LT AFT LOWER HOLE NR 2 HAS CRACK INDICATION 5:00 POSITION. REPAIRED NR 2 HOLE & INSTALLED FASTENER LT FRAME 35 IAW ECRA 53 30-04940. REPAIR OF CRACKED & ELONGATED FASTENER HOLE FRAME 35 BELOW STRINGER 30LT HAS BEEN APPROVED AS Nov 12, 2014 · N494UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2014111092676Door Sill · corrodedRIGHT AFT CABIN DOOR SILL CORRODED AT NUTPLATE ATTACHMENT AT FRAME 68. CORROSION REMOVED & AREA REPAIRED IAW SRM 53-41-44 REPAIR PRINCIPAL 5.Nov 9, 2014 · N496UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014111092677Stringer · corrodedAFT PIT STRINGER 42L CORRODED BETWEEN FRAME 63 & 64. STRINGER 42L REPLACED BETWEEN FACTORY SPLICES AT FRAME 60 & 64 IAW SRM 51-42-11.Nov 9, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014111092678Door Sill · corrodedL2 DOORSILL CORRODED AT GIRT BAR ATTACH HOLES. L2 DOORSILL REPLACED IAW SRM 51-42-11.Nov 9, 2014 · N496UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014110792660Charger · malfunctionedEMERGENCY LIGHT SYS FAILED TEST. FAULTS ATA 33-51-38 BATTERY FED LT. RESET FWD CHARGING UNIT & SYS TESTED GOOD IAW MM 33-51-00.Nov 5, 2014 · N422UA · Airbus A320232 · Emergency LightingSDR CALA2014110792661Stringer · corrodedAFT CARGO STRINGER 41R AT FRAME 63 - 64 HAS CORROSION. REPLACED FACTORY STRINGER SECTION 41R FROM FRAME 58 - 64 IAW SRM51-42-11.Nov 5, 2014 · N496UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014110792662Fitting · corrodedL2 DOOR LOWER AFT CORNER FITTING HAS CORROSION AT LOWER FLANGE OF FRAME 68. REMOVED CORROSION & FOUND MATERIAL LOSS TO BE .018 INCHES. ORIGINAL THICKNESS WAS .070 INCHES, BEYOND LIMITS IAW SRM 51-73-11 PARA D 1. R & R L2 DOOR LOWER AFT CORNER FITTING IAW SRNov 5, 2014 · N494UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2014110492650Skin Panel · saturatedRIGHT ELEV UPPER SKIN PANEL HAS A TRAPPED WATER INDICATION 64.5 FROM INBD, 12 INCHES FROM TE, 2 INCH DIAMETER. REPAIRED ELEV UPPER SKIN BY REMOVING DAMAGE & REPAIRED IAW SRM 55-21-11 REPAIR 5 & FIG 205 CONFIG 1 ZONE L.Nov 2, 2014 · N496UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014103192645Door Sill · corrodedL2 DOOR SILL HAS CORROSION AT FRAME 68 UNDER NUTPLATE. INSTALLED ANGLE REPAIR IAW SRM 53-41-14 FIG 201.Oct 30, 2014 · N494UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014103192644Door Sill · corrodedR2 DOOR SILL CORRODED JUST AFT OF FRAME 68. R2 DOOR SILL WAS FOUND CORRODED OUT OF LIMITS BETWEEN FRAME 66 & 68 IAW SRM 53-41- 14 FIG 101. R & R R2 DOOR SILL BEAM IAW SRM 51-42-11.Oct 28, 2014 · N448UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014102792619Stringer · corrodedMAJOR REPAIR & SDR. STRINGER 41R HAS CORROSION BETWEEN FRAME 59 & 64 IN AFT CARGO COMPARTMENT. R & R STRINGER 41R & FACTORY INSTALLED SPLICE IAW SRM 51-72-11 PGS 1 - 2. NO REQUIREMENT FOR SRI INSPECTIONS.Oct 26, 2014 · N494UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014102792622Connector · not seatedEMERGENCY LIGHT TEST FAILED ON 2 SERVICE. RESEATED CONNECTOR & BATTERY ON EMER LIGHT POWER SUPPLY IAW 33-51-38, TEST PASSED.Oct 26, 2014 · N415UA · Airbus A320232 · Light System WiringSDR CALA2014102792612Epsu · inoperativeRIGHT EMER LIGHTS TEST FAIL WITH MSG EPSU EMER RT. REPLACED EPSU & BATTERY AT RT OVERWING DOOR IAW AMM 33-51-38. OPERATIONS CHECKED OK.Oct 25, 2014 · N483UA · Airbus A320232 · Emergency LightingSDR CALA2014102792613Skin Panel · contaminatedMAJOR REPAIR & SDR. RT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION 101.5 FROM INBD, 4.5 INCHES FROM TE, 3 INCHES DIAMETER. CUT OUT THE DAMAGED SKIN & CORE. REMOVED WATER APPLIED REPAIR & RESTORED FINISH IAW SRM 55-21-11 PARA 5E. REQUIRES RE-INSPOct 25, 2014 · N448UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014102392550Battery · failedEMERGENCY TEST FAILS AT 2 SERVICE, FAILS EMER LT BATTERY. REPLACED LT BATTERY AT SEAT 21A IAW AMM 33-51-38. OPERATIONS CHECKED GOOD.Oct 22, 2014 · N428UA · Airbus A320232 · Emergency LightingSDR CALA2014102392552Fan · malfunctionedEXTRACT FAULT DISPLAYED ON UPPER ECAM SCREEN. ELEC FUMES FOLLOWED BY VENT EXTRACT FAULT, TURNED OFF BLOWER EXTRACT CABIN FANS NO FUMES. REPLACED EXTRACT FAN 18HQ IAW AMM 21-26-51. COMPLETED OPERATIONAL TEST OF EXTRACT & BLOWER FANS IAW AMM 21-26-51-710-001-Oct 21, 2014 · N412UA · Airbus A320232 · Air Distribution FanSDR CALA2014102192546Door Sill · corrodedR2 DOOR SILL HAS CORROSION AT FRAME 68 AT PREVIOUS REPAIR. REPLACED DOOR SILL IAW SRM 51-42-11.Oct 20, 2014 · N466UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014102192543Light · malfunctionedEMERGENCY LIGHT TEST FAILED, EPSU BATTERY AFT. CYCLED EMER LIGHT CB`S CHECKED OK IAW AMM 33-51-00-710-001-A.Oct 19, 2014 · N472UA · Airbus A320232 · Emergency LightingSDR USAA2014102000003Compressor · stalledENGINE NR 2 COMP STALL. 1ST STALL AT 600FT AGL, ENG QUICKLY RECOVERED ENG STALLED 2ND TIME AT 2500FT WHILE CLIMBING, ALSO RECOVERED QUICKLY. ENG WAS AT TOGA THRUST FOR THE 1ST COMP STALL, WAS AT CLIMB THRUST WHEN 2ND COMP STALL OCCURRED. ENG FAILED BORESCOPEOct 17, 2014 · N672AW · Airbus A320232 · Turbine Engine Compressor SectionSDR CALA2014121692829Skin · damagedLEFT ELEV UPPER SKIN HAS A WATER INGRESS INDICATIONS AT THE FOLLOWING LOCATIONS, 27.5 INCHES FROM INBD END 15 INCHES FROM TE & 2 INCHES IN DIAMETER. NEXT 17 INCHES FROM INBD END 29 INCHES FROM TE & 2 INCHES IN DIAMETER. NEXT 41 INCHES & 43 INCHES FROM INBD EOct 11, 2014 · N447UA · Airbus A320232 · Horizontal Stabilizer, Plate/SkinSDR CALA2014101392397Spar · mechanic errorNUMBER 2 PYLON LOWER SPAR WEB MIS DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. ACCOMPLISHED INSPECTION REQUIREMENTS IAW RDAS, SPAR HAS INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR HAS BEEN APPROVED AS INTERIM FOR 1 MONTH IAW RDAS 80003171-003-20Oct 10, 2014 · N492UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/RibSDR CALA2014101692442Stringer · corrodedMAJOR REPAIR & SDR STRINGER 39L CORRODED AT FRAME 59. FOUND NO LIMITS IAW SRM 53-00-13 PG 101. FABRICATED NEW STRINGER, SPLICE & INSTALLED BETWEEN FRAME 58 & 60 IAW SRM 53-00-13 PG 212 FIG 201 SHEET 1 & 2. THIS REPAIR REQUIRES SRI INSPECTIONS IAW SRI 53-00-Oct 10, 2014 · N497UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014101692444Fitting · mechanic errorFRAME CLIP MIS DRILLED AT FRAME 32 STRINGER 39 - 40R. REPLACED CLIP IAW SRM 51-4 2-11.Oct 10, 2014 · N497UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014101692447Skin · gougedFUSELAGE SKIN GOUGE AT FRAME 32 BETWEEN STRINGER 38 -39R. DAMAGE REMOVED & DOUBLER REPAIR INSTALLED IAW SRM 53-00-11 FIG 240.Oct 10, 2014 · N497UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2014101392398Door Sill · corrodedMAJOR REPAIR & SDR. R2 DOOR SILL HAS CORROSION UNDER GIRT BAR PLATE BETWEEN FRAME 66 & 68. REMOVED CORROSION FROM DOOR SILL & FOUND MATERIAL LOSS TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. R & R R2 DOOR SILL WITH NEW SILL IAW SRM 51-42-11. NO REQUIREMENOct 8, 2014 · N497UA · Airbus A320232 · Fuselage Miscellaneous Structure
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