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 UALA2011090204719Spoiler Sys · faultedNR 4 SPOILER FAULT, TRIED TO RESET, NO HELP. OK TO CONTINUE.Sep 1, 2011 · N440UA · Airbus A320232 · Drag Control SystemSDR UALA2011083104686Battery · failedEMERGENCY LIGHT TEST FAILED. SHOWS 33-51-38 EPSU BATTERY AFT LEFT. REPLACED EPSU BATTERY IN AFT LEFT POWER SUPPLY.Aug 31, 2011 · N473UA · Airbus A320232 · Emergency LightingSDR UALA2011090204734Stowage Box · defectiveCAPT O2 MASK CABINET STOWAGE DOOR NOT OPERATING NORMALLY CAUSING A LEAKY MASK. REPLACED O2 MASK STOWAGE BOX, FOUND DEFECTIVE SWITCH OP CHECKED & LEAK CHECKED OKAY.Aug 31, 2011 · N425UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2011082904621Bolt · defectiveDOOR 1L-GUST LOCK STICKS-HARD TO RELEASE DOOR TO CLOSE. REPLACED UPPER FWD ATTACH BOLT FOR SLIDE. OPERATES NORMALLY. ACCOMPLISHED RII INSPECTION AS REQUIRED REF MM. SLIDE PIN REMOVED AND STOWED PIN, VERIFIED BY MGMT.Aug 29, 2011 · N405UA · Airbus A320232 · Escape SlideSDR UALA2011083104692Tape · missingVIBRATION-NOISE ENCOUNTERED IN FLIGHT. NEED TO COMPLETE VIBRATION REPORTING CHECKLIST AND DEBRIEF MAINTENANCE (SAMC) ON ARRIVAL TO DESTINATION STATION. CREW COMMENTS: VIBRATION WITH FULL FLAPS. NONE WITH FLAPS 3 ON FINAL. FOUND TAPE FROM CF271 ON OVER WINGAug 29, 2011 · N480UA · Airbus A320232 · Trailing Edge Flap Control SystemSDR GTIA20110828241Cylinder · low pressureDOOR 2R ASSIST BOTTLE REQUIRES SERVICING. SERVICED 2R DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001.Aug 28, 2011 · N603NK · Airbus A320232 · Passenger/Crew DoorsSDR UALA2011082904639Valve · openNO WATER PRESSURE, FLIGHT DIVERTED. FOUND OVERFLOW VALVE OPEN ON ARRIVAL. CYCLED VALVE MANUALLY AND FROM SERVICE PANEL. ALL OP'S NOW NORMAL.Aug 28, 2011 · N447UA · Airbus A320232 · Water and Waste SystemSDR UALA2011082904600Safety Valve · faultyN-W-STRG FAULT. WILL REQUIRE TROUBLESHOOTING. ACCOMPLISHED TSM. REPLACED SERVO CONTROL NW STEERING, NO HELP. TS DATA GIVES FAULT CODE "53". UNABLE TO CLOSE L/G DOORS. RESET LGCIU'S, NO HELP. TRIED NEW LGCIU'S, NO HELP. ORIGINALS REINSTALLED. REPLACEDAug 27, 2011 · N471UA · Airbus A320232 · Landing Gear Door Retract SectionSDR UALA2011083104687Smoke Detector · faultySMOKE LAV - CRG DET ECAM. NO TIME DENMM. REPLACED LAV 'F' SMOKE DETECTOR, ALL TESTS PASS.Aug 27, 2011 · N417UA · Airbus A320232 · Smoke DetectionSDR UALA2011082604564Ballast · faultySMELL IN AFT GALLEY, FLIGHT DIVERTED. FOUND BAD COUNTER LIGHT BALLAST AND SOME BURNT DEBRIS ON COUNTER HOTPLATE. REMOVED DEBRIS FROM HOTPLATE AND REPLACE BALLAST. TALKED TO SAMC AND GOT OKAY.Aug 26, 2011 · N493UA · Airbus A320232 · Passenger Compartment LightingSDR UALA2011082604581Proximity Switch · faultyDOOR 2R SLIDE INDCATION ARMED WENT OUT IN FLIGHT DOOR 2R SLIDE INDICATED DISARMED AIRBORNE UNTIL F/A RE-ARMED IT. F/A REPORTED, INDICATION ON DOOR NOT LINED UP RIGHT. PRESSURIZED AIRCRAFT PER JRH NO DEFECTS FOUND ON ECAM FOR SLIDE INDICATION FOR DOOR 2R. VIAug 26, 2011 · N495UA · Airbus A320232 · Door Warning SystemSDR UALA2011082904631Switch · brokenCAPTAIN'S OXYGEN MASK PRESS TO TEST SWITCH BROKE OFF. REPLACED CAPT OXYGEN MASK BOX PER MM, OPS CHECKS GOOD.Aug 26, 2011 · N469UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2011082504559Filler · defectiveCREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SAMC TEXT: PRESS WAS 10 PSI WHEN LANDED, BUT READS ZERO NOW. REPLACED FILL PORT PER MM. SERVICED AND LEAK CHECK OK, INSPECTED AND STOWED CREW MASKS, NO LEAKS NOTED.Aug 25, 2011 · N425UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2011082404534Actuator · leakingLEFT WHEEL WELL HAS FLUID LEAK. FLUID LEAK FOUND ON PREFLIGHT WALKAROUND. REPLACED LT MLG RETRACT ACTUATOR. REPLACED PIN (P/N 201590900 - SERIAL# HP11183 - (POSIT LH). ACCOMPLISHED OPS CHECK. NO LEAKS NOTED.Aug 24, 2011 · N416UA · Airbus A320232 · Landing Gear Door Retract SectionSDR UALA2011082404539Fire Bottle · emptyAFT CABIN, FWD LAV, FIRE EXT BOTTLE PRESSURE EMPTY IN LAV WASTE BIN AREA. REPLACED FIRE EXTINGUISHER BOTTLE OFF S/N 28651 AND ON S/N 48498.Aug 24, 2011 · N405UA · Airbus A320232 · Fire Bottle, PortableSDR UALA2011082504550Unknown · malfunctionedLAV ISSUE, FLIGHT DIVERTED. CREW COMMENTS: ALL LAVS SHOW FULL WILL NOT FLUSH SAMC TEXT: BITE TEST THE CONTROLLER AND IF IT FAULTS THE 41MG SENSOR, THEN REMOVE AND CLEAN THE LIQUID LEVEL SENSOR (CAREFULLY) TO REACTIVATE THE LAVATORY FLUSH SYSTEM. SVC LAVS OAug 24, 2011 · N477UA · Airbus A320232 · Waste Disposal SystemSDR UALA2011082404533Sensor · faultyADR 1 ECAM, FLIGHT DIVERTED. SAMC TEXT: *UPDATE* CFDS SHOWS TAT SENSOR 11FP1 FAULT SEEN BY BOTH ADR1 AND ADR3. SENSOR PCN 484- 0084. REPLACED TAT SENSOR 1, REF TSM 34-11-00-810-863 AND AMM-34-11-18. ACP SENSOR TEST. NO FAULTS. CONCURRED WITH OPBLM.Aug 23, 2011 · N405UA · Airbus A320232 · Outside Air Temperature Indicator/SensorSDR UALA2011082204466Access Panel · leakingDURING WALK AROUND, FUEL LEAKING FROM INSPECTION PANEL AFT OF FUEL PANEL. MX FOUND THE LEAK TO BE LIGHT IAW AMM. REPLACED FUEL PLATE PER MM, NO LEAKS NOTED. FOUND FUEL STILL SEEPING THROUGH AFTER REPLACEMENT OF FUEL ACCESS PANEL . REPLACED DOME NUT. NO LEAKSAug 22, 2011 · N438UA · Airbus A320232 · Wing, Plate/SkinSDR UALA2011082404531Strut · defectiveFOUND NOSE STRUT FLAT ON WALK AROUND. SERVICED WITH NITRO. TO BE RECHECKED WITHIN 4 TO 7 DAYS. SERVICED NOSE STRUT PER AMM. NOW NEED TO BE RECHECKED 4-7 DAYS. TIME CHANGED TO 22AUG PER SAMC CONTROLLER. REMOVED NLG STRUT INNER CYLINDER AND REPACK SHOCK ABSAug 22, 2011 · N484UA · Airbus A320232 · Nose/Tail Landing Gear Strut/AxleSDR UALA2011082204454Relay · faultyEMERGENCY GENERATOR FAILED THE EQ3333 TEST. REPLACED RELAYS 12XE AND 20. REPLACED NR 3 TR BAD FROM STOCK, RE-INSTALLED ORIGINAL. FOUND RELAY 17XE CONTACTS A2 TO A3 REMAINS OPEN WHEN DE-ENERGIZED. REPLACED RELAY 17XE - OPS CHECKS GOOD.Aug 21, 2011 · N422UA · Airbus A320232 · AC Generation SystemSDR UALA2011082204465Hinge Fitting · faultyDOOR 1L PRESSURE LEAK. IN PREPARATION FOR MAINT FERRY, PRESSURIZE THE AIRCRAFT AND ENSURE NO PRESSURIZATION LEAKS FROM DOOR 1L. ACCOMPLISHED PRESSURIZATION OF AIRCRAFT PER MM. NO LEAKS NOTED AT DOOR 1L; RAN AIRCRAFT UP TO 4.5 DPI. REMOVED L1 DOOR, ACP HIDAug 21, 2011 · N417UA · Airbus A320232 · Passenger/Crew DoorsSDR USAA2011082200021Seal · leakingCAPTAIN REPORTED DIRTY SOCK ODOR FROM PACKS WITH OR WITHOUT APU BLEED SOURCE, BUT MORE NOTICEABLE IN HIGH HUMIDITY CONDITIONS. ODOR NOTICED ON TAXI, TAKEOFF AND DESCENT BY FLIGHT CREW & PASSENGERS. MAINTENANCE FOUND EVIDENCE OF OIL IN NR 2 ENGINE FAN HUB ANDAug 20, 2011 · N658AW · Airbus A320232 · Turbine SectionSDR UALA2011082204440Structure · damagedNR 1 ENGINE COMPRESSOR SECTION HAS A 1X1 HOLE AT 6 O'CLOCK POS IN HONEYCOMB UNDER BLADES. MX DETERMINED THE DEPTH OF OF THE HOLE TO BE ONE-QUATRER OF AN INCH DEEP, IT IS NOT THRU THE GLASS REINFORCED COMPOSITE LAYER. REF AMM 72-32-85. OK. TO CONTINUE IN SERVICAug 20, 2011 · N498UA · Airbus A320232 · Turbine Engine Compressor SectionSDR UALA2011082204485Computer · faultyFLT CONTROL ELAC NR 1 PITCH FAULT. RESET ELAC NR 1 TWICE, COMES BACK ON FLT CONTROL CHECK. REPLACED ELAC NR 1 PER MM AND CAT III AUTOLAND PER MM. OPS CHECKED OKAY.Aug 20, 2011 · N401UA · Airbus A320232 · Flight Control SystemSDR UALA2011082404549Frangible Link · improper partRECEIVED SLIDE MR25822-2051 IN PACKED CONDITION. UPON DISASSEMBLY FOUND ONE INCORRECT FRANGIBLE LINK INSTALLED AT THE SILL SUPPORT LOG. FRANGIBLE LINK INSTALLED WAS P/N C19347-103 (NATURAL), SHOULD BE P/N C19749-103 (BLACK/ORANGE). DUE TO THE DIFFERENT BREAAug 20, 2011 · N418UA · Airbus A320232 · Escape SlideSDR UALA2011082204486Rub Strip · damagedLT WING OUTBOARD AFT FLAP METAL RUBSTRIP TORN & PEELING OFF ON TOP AFT INNER SECTION OF FLAP, OUTBOARD OF NR 1 ENG. 1' X 2' SECTION. ACP INTERIM REPAIR WITH METAL SPEED TAPE. REFERENCE MT 57-003 TO USE B AND 1-6TH SEALANT TO REINSTALL STRIP. RUBSTRIP PCN 11Aug 20, 2011 · N486UA · Airbus A320232 · Trailing Edge FlapsSDR UALA2011082204469Smoke Detector · false activationSMOKE LAV DET FAULT. REPLACED LAV 'A' SMOKE DETECTOR, TESTED OKAY.Aug 19, 2011 · N469UA · Airbus A320232 · Smoke DetectionSDR UALA2011081904409Shutoff Valve · inoperativeNR 1 ENG HYD FIRE SHUT-OFF VALVE INOPERATIVE. ACCOMPLISHED ON DOCK WU E6244G AND OPS CHECKED OKAY.Aug 18, 2011 · N495UA · Airbus A320232 · Hydraulic System, MainSDR UALA2011081904426Audio Panel · faultyACP 3 HAS A HOT MIKE. REPLACED OBSERVERS AUDIO PANEL.Aug 18, 2011 · N431UA · Airbus A320232 · Audio Integrating SystemSDR GTIA20110817231Cylinder · low pressureR1 DOOR ASSIST REQUIRES SERVICING. SERVICED R1 PASS DOOR ASSIST IAW AMM 52-10-00-614-001.Aug 17, 2011 · N606NK · Airbus A320232 · Passenger/Crew DoorsSDR UALA2011081704376Plate · corrodedCORROSION ON SILL PLATE AT DOOR 2R BETWEEN FRAMES 66 AND 68 AT FLOOR LEVEL. MAJOR REPAIR. INSTALLED REPAIR AT FR 68 PER SRM53-41-14 ON NR D3700Y.Aug 17, 2011 · N479UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2011081904425Servo Valve · malfunctionedNW STRNG FAULT DISPLAYED-NOSE WHEEL STEERING INOP. ATTEMPTED RESET OF NWS SWITCH AND BOTH BSCU 1&2, NO HELP. MAINT TEXT: BOTH BSCU 1 & 2 FAULT STEERING ELECTRO HYDRAULIC MODULE 6GC. REPLACED NOSE WHEEL STEERING SERVO VALVE.Aug 17, 2011 · N414UA · Airbus A320232 · Landing Gear Steering SystemSDR UALA2011081804394Tire · vibrationNOSE WHEEL VIBRATION AFTER ROTATION AT 145 KTS. REPLACED BOTH NOSE TIRES. REQUEST CREW COMMENTS ON VIBRATION. ABNORMALLY HEAVY VIBRATION FROM NOSE GEAR AFTER LIFTOFF AND PRIOR TO RAISING GEAR. T/S PER TSM. FOUND NR 1 MLG TIRE OUT OF ROUND AS PER TSM. REMOAug 16, 2011 · N457UA · Airbus A320232 · TireSDR UALA2011081604350Light · inoperativeMAINTENANCE MESSAGE ON CIDS PANEL EPSU INT LOAD EMER L AFTER EMERGENCY LIGHTING TEST AT PTP PANEL. RELAMPED EMERGENCY LIGHT AT SEAT 26 ABC, CIDS TEST PASSED OKAY PER MM.Aug 16, 2011 · N487UA · Airbus A320232 · Emergency LightingSDR UALA2011081604344Valve · leakingFUEL TRANSFERRING FROM CENTER TO RIGHT TANK AT RATE OF 20LB EVERY 3 MIN. OPENED & VENTED RIGHT TANK, FOUND RIGHT TANK SUCTION VALVE LEAKING WITH CENTER PUMPS ON. REPLACED RT SUCTION VALVE.Aug 15, 2011 · N436UA · Airbus A320232 · Aircraft Fuel Distribution SystemSDR UALA2011081604345Apu · making metalWHILE CHANGING APU GENERATOR, FOUND BOTH OIL FILTER DPI'S EXTENDED AND EXCESSIVE METAL CONTAMINATION ON CHIP DETECTOR. DRAINED MOST OF OIL FROM APU. REPLACED APU PER MM.Aug 15, 2011 · N440UA · Airbus A320232 · APU Core EngineSDR UALA2011081504295Skin · corrodedCORROSION FOUND BETWEEN FR69 AND FR70 RT SIDE AT OVERBOARD EXH PORT AFT OF OUTFLOW VALVE. SKIN CORROSION IS APPROX 50-60% OF SKIN THICKNESS. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING FASTENERS AND CORRODED SKIN FABRICATED DAMAGE FILLER, USING SRM. ACP HFAug 14, 2011 · N460UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2011081504306Skin Panel · delaminatedFOUND DELAM ON PANEL 191DB AIR START PANEL LT SIDE. TAPED DAMAGE IN ACCORDANCE WITH SRM. NR 2 REPAIR WITHIN 1000 FH.Aug 13, 2011 · N439UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2011081504273Placard · inaccurateDOOR 2R DOOR ARMING PLACARDS ARE NOT CORRECT. REMOVED INCORRECT PLACARDS AND INSTALLED CORRECT SLIDE ARMED PLACARDS ON SLIDE COVER.Aug 13, 2011 · N452UA · Airbus A320232 · Placards and MarkingsSDR UALA2011081504307Unknown · malfunctionedFUEL SYSTEM PROBLEM, FLIGHT DIVERTED. CENTER TANK PUMP 1 DID NOT COME ON 15 MINUTES INTO FLIGHT UNTIL AFTER THE AUTO FEED FAULT PROMPTED FLT CREW TO DESELECT AUTO FEED, PUTTING FEED SYS IN MANUAL. AUTO FEED FAULT ON ECAM AND PFR. DF STICKER APPLIED. ACCOMPAug 13, 2011 · N431UA · Airbus A320232 · Aircraft Fuel Distribution SystemSDR UALA2011081504313Lever · faultyCOULD NOT RAISE THE LANDING HANDLE INITIALLY AFTER T/O. AFTER 3-5 MIN HANDLE COULD BE RAISED. SAMC TEXT: ACP MM FUNCTION TEST WHICH WILL REQUIRE NORMAL RETRACT AND EXTEND. REPLACED GEAR LEVER (6GA). JACKED A/C AND ACCOMPLISHED FUNCTIONAL TEST OF THE NORMALAug 13, 2011 · N424UA · Airbus A320232 · Landing Gear SelectorSDR UALA2011081204252Engine · bird ingestionNR 1 ENG BIRD STRIKE. NR 1 FEC, STG 6 HPT 60% AIRFOIL MISSING. SUBSEQUENT WRITEUP FOR REMOVAL ACCT HPC STAGE 6 AIRFOIL DAMAGE. NR 1 ENG NOSE COWL 1 & 6 O'CLOCK APPEARS TO HAVE GONE INTO ENGINE AND LT WING PANEL 521AB NEAR FUSELAGE. BIRD STRIKE INSPECTION CAug 12, 2011 · N419UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR UALA2011081204254Panel · erodedBELLY PANEL 191BB LE EROSION. APPLIED FILLER TO AREA OF EROSION.Aug 12, 2011 · N441UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2011081504264Bottle · dischargedDOOR 1L EMERGENCY CYLINDER PRESSURE LOW. SERVICED DOOR EMERGENCY ACCUMULATOR.Aug 12, 2011 · N405UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2011081204258Computer · faultyELAC 2 FAULT. REPLACED ELAC 2 PER AMM. TESTS OKAY. ACCOMPLISHED CAT3 TEST. TESTS SATISFACTORILY.Aug 11, 2011 · N469UA · Airbus A320232 · Flight Control SystemSDR UALA2011081004185Panel · looseRETORQUED FUEL PANEL 640NB ON RT WING. FUEL SEEPING APPROX 6 INCHES INBD FROM FLAP FAIRING ON AFT EDGE. TORQUED PANEL IN ACCORDANCE WITH MM.Aug 10, 2011 · N423UA · Airbus A320232 · Wing, Plate/SkinSDR UALA2011081004192Servo Control · malfunctionedN-W STR FAULT DISPLAYED. SAMC TEXT: CONTACT SAMC, REF TSM 32-51-00 TASK 836. REPLACE NWS SERVO VALVE 6GC. REMOVED & REPLACED NOSE STEERING SERVO CONTROL, OPS GOOD.Aug 10, 2011 · N466UA · Airbus A320232 · Steering UnitSDR GTIA20110809225Cylinder · low pressureR2 ACCUMALATOR NEEDS SERVICED. SERVICED R2 DOOR TO PROPER PRESSURE IAW 52-10-00-614-001.Aug 9, 2011 · N607NK · Airbus A320232 · Passenger/Crew DoorsSDR UALA2011081004182Apu · malfunctionedBURNING SMELL IN AFT CABIN ON TAKEOFF AND LANDING. LAST 2 LEGS REPEAT WRITEUP. ACP HIGH POWER RUNS ISOLATING PACKS AND ENGINE BLEED SOURCES. TESTED LIGHTS AT ALL SETTINGS TESTED COFFEMAKERS, NO ABNORMAL SMELLS. FOUND OIL IN APU COMPARTMENT AND COMPRESSOR IAug 9, 2011 · N465UA · Airbus A320232 · APU Core EngineSDR UALA2011081004205Skin · damagedGOUGE ABOUT 8" LONG ON LEFT SIDE OF VERTICAL STAB ABOUT 6' UP FROM FUSELAGE. DAMAGE IS EXPOSED COMPOSITE DUE TO PAINT SEPARATION ON VERTICAL STAB AT ZONE 323 STA 299 DAMAGE IS AN UNEVEN AREA EXTENDED OVER 10" LONG AND 4" WIDE. MADE TEMPORRAY REPAIR PER SRM. Aug 9, 2011 · N455UA · Airbus A320232 · Vertical Stabilizer, Plate/Skin
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