IAE V2527-A5

Service difficulty reports · 8,009

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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"

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SDR CALA2014052791147Start Valve · faultyCREW REPORTS DURING NR 2 ENG START APU BLEED PRESS SHOWS ONLY 22 PSI, ENG DID NOT START, CYCLED APU BLEED SWITCH, PRESS RECOVERED TO 30 PSI BUT LATER DROPPED TO 20 PSI. UNABLE TO START ENG WITH START VLV FAULT, RESET A05 & Q4 0 CROSS BLEED START RESULTED IN SMay 23, 2014 · N486UA · Airbus A320232 · Engine Start Valves/ControlsSDR CALA2014052791169Generator · malfunctionedDURING CLIMB LOST GENERATOR NR 2.May 23, 2014 · N451UA · Airbus A320232 · AC Generator-AlternatorSDR CALA2014052291122Skin · corrodedCORROSION AFT CARGO COMPARTMENT JUST AFT RT FRAME 57 UNDER FLOOR STRINGER 38. PERFORMED LT ANGLE REPAIR AT AFT CARGO STRINGER 42L BETWEEN FRAME 58 & FRAME 59 IAW SRM53-00-13 FIG 205 SHEET 3. REPAIR IS A CAT B REPAIR & REQUIRES RE-INSP AT 60000 FC & 75000 FH SMay 21, 2014 · N486UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2014052291124Structure · corrodedAFT CARGO COMPARTMENT SHOW SIGNS OF CORROSION AT STRINGER 42L JUST AFT OF FRAME 63. PERFORMED LT ANGLE REPAIR AT AFT CARGO COMPARTMENT STRINGER 42L JUST AFT OF FRAME 63 IAW SRM 53-0 0-13 FIG 203 SHEET 3. REPAIR IS A CATEGORY B REPAIR & REQUIRES RE-INSP AT 6May 21, 2014 · N486UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014052291125Structure · corrodedAFT CARGO COMPARTMENT SHOW SIGNS OF CORROSION AT STRINGER 42L BETWEEN FRAME 54 & FRAME 55. PERFORMED LT ANGLE REPAIR AT AFT CARGO COMPARTMENT STRINGER 42L BETWEEN FRAME 54 & FRAME 55 IAW SRM 53-00-13 FIG 205 SHEET 3. REPAIR IS A CATEGORY B REPAIR & REQUIRES May 21, 2014 · N486UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014052291126Structure · corrodedAFT CARGO COMPARTMENT SHOW SIGNS OF CORROSION AT STRINGER 42R 6 INCHES AFT OF FRAME 64. PERFORMED LT ANGLE REPAIR AT AFT CARGO COMPARTMENT AT STRINGER 42R AFT OF FRAME 64 IAW SRM 53-00-13 FIG 203 SHEET 3. REPAIR IS A CATEGORY B REPAIR & REQUIRES RE-INSP AT 6May 21, 2014 · N486UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014052291127Frame · corrodedCORROSION FOUND ON FWD FACE ON FRAME 68 BETWEEN STRINGER 23R & 24R. REMOVED CORROSION AT FWD FACE OF FRAME. PERFORMED REPAIR AT FRAME 68 BETWEEN STRINGER 23R & 24R. REPAIR REQUIRES RE-INSP AT 36294 FC OR 78006 TOTAL FH WHICHEVER COMES FIRST IAW ECRA 5311-01May 21, 2014 · N486UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2014052291128Battery · dischargedRIGHT OVERWING EXIT EMERGENCY LIGHTS FAILS EEL LIGHT TEST. FOUND RT OVERWING EXIT POWER SUPPLY BATTERY BAD. REPLACED BATTERY IAW MM 33-51-38. OPERATIONS CHECKED OK.May 21, 2014 · N461UA · Airbus A320232 · Emergency LightingSDR CALA2014052291129Battery · dischargedFOUND RT OVERWING EXIT POWER SUPPLY BATTERY BAD. REPLACED BATTERY IAW MM 33-51-38. INSPECTED RT OVERWING EXIT POWER SUPPLY INSTALLATION & OPERATIONS CHECKED EEL LIGHTING IAW MM 33-51-38.May 21, 2014 · N461UA · Airbus A320232 · Emergency LightingSDR CALA2014051991061Support · corrodedFRAME 60 - FRAME 70 CIRCUMFERENTIAL SUPPORT FOUND CORRODED. R & R SUPPORT FRAME D5347112320200 IAW A320 51-72-11.May 19, 2014 · N483UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014051991064Spar · chafedNUMBER 1 PYLON LOWER SPAR HAD CHAFE MARK FROM CONTACT WITH THE CNA. BLENDED & WITHIN LIMITS IAW SRM 54-51-12 FIG 103. MAX MATERIAL LOSS IS 0.017, EXTENDED CHAFE PLATE INST IAW SRM 54-51-12 PARA 5 B FIG 202. REQUIRES INSPECTION IAW SRI54-51-12-2-001-00 PARA May 19, 2014 · N487UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/RibSDR CALA2014052291111Stringer · corrodedAFT CARGO BAY SHOWS SIGNS OF CORROSION ON STRINGER 42R, 9 INCHES AFT OF FRAME 63. PERFORMED ANGLE REPAIR IAW SRM 53-00-13 FIG 203 SHEET 3 REPAIR IS A CAT B.May 19, 2014 · N486UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2014051991065Light · intermittentOVERHEAD EMERGENCY LIGHTS INOPERATIVE. LIGHTS GO ON & OFF BY THEMSELVES. UNABLE TO DUPLICATE. EEL BITE TEST AT FAP OKAY. ALL LIGHTS OPERATIONAL NO HISTORY NOTED.May 18, 2014 · N490UA · Airbus A320232 · Emergency LightingSDR CALA2014051991062Connector · unknownCEILING EMERGENCY LIGHT AT ROW 1 INOPERATIVE. TROUBLESHOOTING CEILING EMERGENCY LIGHT AT ROW 1 FOUND CONNECTOR & OPERATION CHECKED CEILING EMERGENCY LIGHT IAW AMM 33-51-11-400-001-A OPERATIONS CHECKED NORMAL.May 17, 2014 · N486UA · Airbus A320232 · Light System WiringSDR CALA2014051991063Door Sill · corrodedL2 DOOR LOWER SILL L2 CORROSION FOUND, FRAME 68 BEAM. REMOVED CORROSION FROM MAIN CABIN L2 SILL BEAM. REPAIRED IAW SRM 53-41-14 REPAIR PRINCIPAL 5.May 17, 2014 · N487UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014051991066Warning System · activatedFORWARD CARGO DOOR ECAM ON TAKEOFF ROLL. RETURNED TO BLOCK.May 17, 2014 · N431UA · Airbus A320232 · Door Warning SystemSDR CALA2014051991067Battery · dischargedEMERGENCY LIGHT TEST FAILED. CIDS MSG, EPSU INT LOAD EMER LT & EPSU EXT LOAD EMER LT ATA 33-51-38. REPLACED EMERGENCY BATTERY AT LT OVERWING POWER SUPPLY.May 17, 2014 · N443UA · Airbus A320232 · Emergency LightingSDR CALA2014051691034Unknown · malfunctionedAUTO FLIGHT, A - THR OFF, DISPLAYED ON UPPER ECAM SCREEN. FIRST OFFICER`S SPEED FLASH XX THEN BACK. RESET FMGC 1 & 2 FOUND FAC1 MSG RESET FAC 1. ACCOMPLISHED AFS TEST ALL PASSED, ACCOMPLISHED AUTO THROTTLE TEST IAW AMM 22-30-00-040-004-A TEST PASSED. INSPMay 16, 2014 · N420UA · Airbus A320232 · Auto Throttle SystemSDR CALA2014051991060Door Sill · corrodedMAIN CABIN R2 LOWER SILL HAS CORROSION ON FRAME 68. CORROSION FOUND BEYOND OEM LIMITS. FABRICATED & INSTALLED REPAIR PLATE IAW SRM53-41-14 FIG 101 & 201. THIS REPAIR WAS CIR'D & ACCEPTED.May 16, 2014 · N483UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014051691031Structure · corrodedCORROSION AFT CARGO COMPARTMENT JUST AFT RT FRAME 57 UNDER FLOOR STRINGER 38. PERFORMED LT ANGLE REPAIR AT AFT CARGO STRINGER 42L BETWEEN FRAME 58 & FRAME 59 IAW SRM 53-00-13 FIG 202 SHEET 3. REPAIR IS A CAT B REPAIR & REQUIRES INSPECTION AT 60000 FC & 75000May 15, 2014 · N486UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014051691032Structure · corrodedAFT CARGO COMPARTMENT SHOWS SIGNS OF CORROSION AT STRINGER 42L BETWEEN FRAME 58 & FRAME 59. PERFORMED LT ANGLE REPAIR AT AFT CARGO STRINGER 42L BETWEEN FRAME 58 & FRAME 59. THIS IS A CAT B REPAIR & REQUIRES INSPECTION AT 60000C AFTER REPAIR EMBODIMENT SUBSEQMay 15, 2014 · N486UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014051691029O-Ring · damagedYELLOW HYD ECAM MSG LOW QTY. REPLACED BAD O RING ON BOTTOM OF YELLOW SYS FILTER MODULE ASSEMBLY, NR 2 ENG DRIVEN PUMP & CASE DRAIN FILTER. ALSO REPLACED REF ITEM 4192001 CHECKED ASSOCIATED FILTERS FOR METAL DEBRIS, NONE FOUND. SYS OPERATIONS CHECKED & LEAKMay 14, 2014 · N459UA · Airbus A320232 · Hydraulic System, MainSDR CALA2014051691033Slide · faultyEPSU EXT LOAD AFT LT, EPSU COMM EMER LT FAULTS ON EMERGENCY LIGHT TEST. ACCOMPLISHED TSM 33-51-00-810-808A FOUND SHORT IN DOOR 2 LT SLIDE PACK, FAULTS GO AWAY WITH SLIDE JUMPED. WILL NEED NEW SLIDE PACK MR25823. REPLACED DOOR 2 LT SLIDE IAW AMM 25-62-44-400May 14, 2014 · N495UA · Airbus A320232 · Escape SlideSDR CALA2014051391012Adiru · out of alignmentIR 2 & 3 FAULT. REALIGNED ADIRUS RESET FMGC 1 & 2 RETURNED TO NORMAL.May 11, 2014 · N448UA · Airbus A320232 · Integrated Flight SystemSDR CALA2014051391013Attach Fitting · chafedAFT CARGO DOOR AFT ACTUATOR ATTACH FITTING IS CHAFED. BLENDED CHAFED AREA. ORIGINAL THICKNESS WAS 0.200 & REMAINING THICKNESS IS 0.198. MATERIAL LOSS IS 0.002. THIS REPAIR REQUIRES SRI INSP IAW SRI 52-30-00-1-005-00 TABLE 105. FIRST INSPECTION IS DUE AT 6May 11, 2014 · N483UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2014051391014Skin · damagedLEFT ELEV UPPER SURFACE HAS 6 FINDINGS FROM THERMOGRAPHY. LOCATIONS ARE 48 FROM INBD END & 20 FROM TE, 56 FROM INBD END & 21.5 FROM TE, 58 FROM INBD END & 14.25 FROM TE, 99.38 FROM OTBD END & 18 FROM TE, 53.5 FROM OTBD END & 6.5 FROM TE, 17 FROM LE & 6.5 FROMMay 10, 2014 · N486UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014050990993Skin · damagedLEFT ELEV UPPER SURFACE HAS 6 FINDINGS FROM THERMOGRAPHY. LOCATIONS ARE 48 INCHES FROM INBD END & 20 INCHES FROM TE, 56 INCHES FROM INBD END & 21.5 INCHES FROM TE, 58 INCHES FROM INBD END & 14.25 INCHES FROM TE, 99.38 INCHES FROM OTBD END & 18 INCHES FROM TE May 7, 2014 · N486UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014050990994Skin · damagedRIGHT ELEV HAS 4 FINDINGS FROM THERMOGRAPHY INSPECTION. 3 ARE ON UPPER SURFACE & 1 ON LWR SURFACE. UPPER SURFACE, 23.5 INCHES FROM INBD END & 8.5 INCHES FROM TE, 66.50 INCHES FROM OTBD END & 13 INCHES FROM TE, 18 INCHES FROM LE & 7.5 INCHES FROM TE & 1 LOWERMay 7, 2014 · N486UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2014050690961Unknown · faultyO2 SERVICED TO FULL IN DENVER, SHOWED 1500 AT DULLES. NOW SHOWING 1360 IN FLT. BOTTLE PRE-SERVICE READING WAS 1600 PSI, SERVICE TO 2000 PSI. COCKPIT INDICATION SHOWED 1900 PSI. CREW WILL MONITOR PRESS INFLIGHT.May 5, 2014 · N484UA · Airbus A320232 · Crew Oxygen SystemSDR CALA2014050690962Warning System · activatedCOND AFT CARGO HEAT FAULT DISPLAYED. UPDATE CREW ABORTED TO LESS THAN 60 KTS DUE TO ECAM DISPLAYED ON ROLL.May 5, 2014 · N423UA · Airbus A320232 · Heating SystemSDR CALA2014050690958Smoke Warning · false activationSDCU ON SHUT DOWN, CYCLED SDCU CB'S & OPERATIONS CHECKED IAW AMM26-16-00 & 26-17-00 ALL TESTS PASSED.May 4, 2014 · N446UA · Airbus A320232 · Smoke DetectionSDR CALA2014050690960Windshield · defectiveFIRST OFFICER'S WINDSHIELD HEAT IS INOPERATIVE. PLACED FIRST OFFICER'S WINDSHIELD R1 INOPERATIVE IAW MEL. CHECKED CAPTAIN'S WINDSHIELD HEAT OPERATIONS CHECKED NORMAL. REPLACED 2DG2 WHC-2, NR 2 WINDOW HEAT COMPUTER IAW AMM TASK 30-42-34-400-001-A & 000-00 1-AMay 4, 2014 · N465UA · Airbus A320232 · Flight Compartment WindowsSDR CALA2014050690957Warning System · false activationDURING GO AROUND, ECAM WARNING LG DOORS NOT CLOSED ECAM WARNING. GO AROUND INITIATED DUE TO TAILWIND CAUSING EXCESSIVE AIRSPEED. RECEIVED ECAM WHEN GEAR UP SELECTED, THROTTLES WERE ADVANCED, BUT NOT IN TO GO POSITION. MOVED GEAR HANDLE TO DOWN & NORMAL THREMay 3, 2014 · N445UA · Airbus A320232 · Landing Gear Position and WarningSDR CALA2014050690959Handle · defectiveCAPTAIN'S PTT ON STICK CONSTANTLY TRANSMITS. REPLACED CAPTAIN'S SIDE STICK HANDLE IAW AMM 27-92-91. PTT OPERATIONS TEST OK IAW AMM 23-12-00. PRIORITY TEST OK IAW AMM 27-96-00. SIDE STICK OPERATIONS TEST OK IAW AMM 27-92-41.May 3, 2014 · N452UA · Airbus A320232 · Flight Control SystemSDR CALA2014050690964Doubler · debondedAFT LT FUSE AFT OF FR 77 STRINGER 29L - 30L PREVIOUS REPAIR DOUBLER DISBONDED. INSTALLED NEW REPAIR DOUBLER IAW SRM 53-51-11 NO SRI IAW 53-51-11 TBL 202.May 3, 2014 · N412UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014050290948Flap · faultedFLAP CONTROL FLAPS LOCKED ALIGNMENT FAULT ON ECAM.May 2, 2014 · N411UA · Airbus A320232 · Trailing Flap Position Indicating SystemSDR CALA2014050290946Connector · not seatedEMERGENCY LIGHTS TEST FAULTS. RESEATED CONNECTORS ON 30 0RH, CIDS TEST & EMERGENCY LIGHTS TESTED OK.May 1, 2014 · N414UA · Airbus A320232 · Light System WiringSDR CALA2014050290947Smoke Detector · faultyLAVATORY & CARGO SMOKE DETECTION FAULT UPPER ECAM DISPLAYED. REPLACED SCDU, NO HELP. REPLACED AFT CARGO PIT SMOKE DETECTOR 3WH, TEST OK IAW AMM 26-16-00 & AMM 26-17-00, TESTED OK.May 1, 2014 · N446UA · Airbus A320232 · Smoke DetectionSDR CALA2014043090933Control Panel · defectiveEMERGENCY LIGHTS STUCK ON, WILL NOT TURN OFF WHEN ACFT IS UNPOWERED. REPLACED AFT FLIGHT ATTENDANT ANT PANEL IAW MM23-73-13-000-001-A, OPERATIONS CHECKED GOOD.Apr 29, 2014 · N493UA · Airbus A320232 · Emergency LightingSDR CALA2014043090934Control Unit · faultedSMOKE DETECTION FAULT ON UPPER ECAM, SDCU WILL NOT RESET. REPLACED SDCU IAW AMM TASK 26-17-34-400-001-A, OPERATIONS CHECKED OK.Apr 29, 2014 · N490UA · Airbus A320232 · Smoke DetectionSDR CALA2014043090936Mount Bolt · corrodedLEFT MLG FIXED DOOR B FTG MT BOLT TO GEAR CORRODED, REPLACED BOLT.Apr 29, 2014 · N417UA · Airbus A320232 · Landing Gear DoorsSDR CALA2014043090907Skin · dentedAFT FUSELAGE BELLY SKIN DENTED APPROX 8 INCHES FWD OF APU INLET. EVALUATED THE ARCHIVED ITEM & FOUND A PERMANENT DOUBLER REPAIR INSTALLED IAW SRM 53- 00-11 PG 567-568 FIG 238. THIS REPAIR REFERS TO SRI INSPECTION IAW SRI 53-00-11-2-017-00 PARA 3L TABLE 224. Apr 28, 2014 · N414UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2014043090910Attach Bolt · corrodedRIGHT MLG FIXED DOOR C MT FITTING, 1 ATTACH BOLT TO GEAR CORRODED. R & R HARDWARE REF AID BOOK IAW IPC 52-18-13-01.Apr 28, 2014 · N417UA · Airbus A320232 · Landing Gear DoorsSDR CALA2014043090911Attach Bolt · corrodedLEFT MLG FIXED DOOR C MT FITTING BOLTS TO GEAR CORRODED, REPLACED BOLT.Apr 28, 2014 · N417UA · Airbus A320232 · Landing Gear DoorsSDR CALA2014043090908Light · inoperativeEMERGENCY EXIT PATH LIGHTING INOPERATIVE STARTING AT SEAT - ROW 1B. FWD FLOOR PROXIMITY LIGHT ASSEMBLY INOPERATIVE ON SEAT 1 A - B, ALL OTHER FLOOR PROXIMITY LIGHTS CHECK OK.Apr 27, 2014 · N485UA · Airbus A320232 · Emergency LightingSDR CALA2014043090938Light · inoperativeEMERGENCY EXIT PATH LIGHTING INOPERATIVE. STARTING AT SEAT ROW 1B. FWD FLOOR PROXIMITY LIGHT ASSEMBLY INOPERATIVE ON SEAT 1 A - B. REPLACED LIGHT AT 1B.Apr 27, 2014 · N485UA · Airbus A320232 · Emergency LightingSDR CALA2014043090909Control Panel · defectiveEMERGENCY LIGHTS WILL NOT TURN OFF WITH POWER OF ACFT. WHILE TEST OF PTP PANEL SHOWING EPSU COM FWD LT. TESTED EMERGENCY LIGHTS. REPLACED AFT ATTENDANT PANEL & FWD LT POWER SUPPLY 10WL. EMERGENCY LIGHTS TESTED OK.Apr 26, 2014 · N493UA · Airbus A320232 · Emergency LightingSDR CALA2014043090912Door Seal · damagedLOUD SQUEAL AT DOOR 1L FL 200 & BELOW. REPLACED MAIN ENTRY DOOR 1L SEAL ASSEMBLY IAW AMM 52-11-18-000-001-A & 52-11-18-400-001 -A.Apr 26, 2014 · N424UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2014043090913Mechanism · brokenFORWARD CARGO DOOR LOCKING HANDLE MECHANISM BROKEN.Apr 26, 2014 · N434UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2014043090914Strut · out of rigAIR RETURN DUE TO INABILITY TO RETRACT FLAPS AFTER TAKEOFF IAW TSM27-51-00-810, PERFORMED STEP 6 PG 3. LT & RT INTERCONNECTING STRUTS TO BE OUT OF RIG. RIGGED IAW MM27-51-44-820-001-A. ALL CHECKED NORMAL.Apr 26, 2014 · N411UA · Airbus A320232 · Trailing Edge Flap Control System
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