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 UALA2012101005769Control Unit · faultedLAVATORY AND CARGO DETECTOR FAULT DISPLAYED ON UPPER ECAM SCREEN, SMOKE. REPLACED SDCU PER AMM. OPS CHECKED GOOD, NO FAULTS AT THIS TIME.Oct 9, 2012 · N494UA · Airbus A320232 · Smoke DetectionSDR UALA2012100905726Engine · leakingNR 1 ENGINE OIL LEAK AT TOWERSHAFT. MAINTENANCE REPORTS OIL LEAK UNDER NR 1 ENG, OPENED FAN COWLS AN DID VISUAL CHECK, APPEARS TO BE COMING FROM ACOC DRAIN PORT ON DRAIN MAST. THERE IS CURRENTLY NO RELIEF FOR LEAKS AT TOWER SHAFT AREA. REFERENCE MT71-017 FOOct 9, 2012 · N492UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR UALA2012101005762Bottle · brokenLEFT OVERWING SLIDE BOTTLE BROKEN AT CABLE OUTLET. REMOVED AND REPLACED LT OVERWING SLIDE RESERVOIR. OP CHECKED GOOD.Oct 9, 2012 · N460UA · Airbus A320232 · Escape SlideSDR UALA2012101005754Control Unit · faultyREVERSE UNLOCKED DISPLAYED ON UPPER ECAM SCREEN IN FLIGHT ENGINE 1. LCL MAINTENANCE COMPLIED WITH MEL7830M, (DEACTIVED LEFT ENGINE THRUST REVERSER), REVIEW PREVIOUS HISTORY. ENGINE 1 REVERSE UNLOCKED. TS AND REPLACED HYD CONTROL UNIT.Oct 9, 2012 · N477UA · Airbus A320232 · Engine Thrust ReverserSDR UALA2012101005768Wire Harness · faultyNW STEER FAULT DISPLAYED ON UPPER ECAM SCREEN. INDICATED A DUAL FAILURE OF THE STEERING ELECTRO-HYDRAULIC MODULE (6GC). CFDS TEST FAILED THIS UNIT ON INITIAL EVALUATION. REPLACED NOSE WHEEL STEERING SERVO CONTROL. DURING MEGGER CHECK OF WIRES FROM NORMAL SOct 9, 2012 · N403UA · Airbus A320232 · Landing Gear System WiringSDR UALA2012101005771Flap · damagedRIGHT INBD TRAILING EDGE FLAP BIRD STRIKE OUTBD EDGE. INSPECTED AREA OF I/B FLAP FOR DAMAGE. FOUND DENT 1.25" X 1.75" X .055" LOCATED 10 INCHES FROM AFT EDGE AND 8.5" I/B OF THE CANOE. DENT IS LOCATED IN ZONE 2 AREA,TEMPORARY REPAIR NOT REQUIRED REF AIRBUS Oct 9, 2012 · N431UA · Airbus A320232 · Trailing Edge FlapsSDR UALA2012100805699Battery Pack · dischargedEMERGENCY LIGHT TEST FAILS AFT LEFT EPSU BATTERY. REPLACED BATTERY PACK.Oct 8, 2012 · N485UA · Airbus A320232 · Emergency LightingSDR UALA2012100805687Filter · leakingNR 2 ENGINE LEAKING OIL FROM THE PRESSURE PUMP AND FILTER ASSEMBLY. EVIDENCE OIL LEAKING NR 2 ENGINE FROM COWL. FOUND PRESSURE PUMP & FILTER ASSY LEAKING FROM TOP TRIANGLE PLATE. PACKING FOR PLATE DOESN'T BREAK DOWN WILL NEED ASSY. REPLACED OIL PUMP FILTEROct 8, 2012 · N490UA · Airbus A320232 · Turbine Engine Oil SystemSDR UALA2012100905718Battery · faultyCREW REPORTS NR 1 BATTERY SHOWS 24 VOLTS. REPLACED NR 1 SHIPS BATTERY.Oct 8, 2012 · N412UA · Airbus A320232 · Battery/Charger SystemSDR UALA2012100905716Computer · faultyREPLACE ELAC2 FOR T-S ACFT PITCH UP LOG. REPLACED ELAC2 PER AMM, OPS TEST PER MM CHECKED GOOD. ACCOMPLISHED CAT III AUTOLAND, TEST GOOD.Oct 7, 2012 · N452UA · Airbus A320232 · Flight Control SystemSDR UALA2012100805690Unknown · malfunctionedCABIN EMERGENCY LIGHTING CHECK FAIL. REF A320 3SV STEP 2. CYCLED AND RESET CIDS POWER. CABIN EMERGENCY LIGHT TEST OKAY.Oct 7, 2012 · N483UA · Airbus A320232 · Emergency LightingSDR UALA2012100805709Oxygen Mask · faultyF/O O2 MASK PRESS TO TEST 100 PERCENT BUTTON BROKE. REPLACED 1ST OFFICER'S O2 MASK, OPS CHECKS OKAY.Oct 6, 2012 · N497UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012100805703Eiu · faultyDUE TO REPORTED HIGH IDLE FAULT AND NR 2 REVERSER FAULT, REPLACED NR 2 EIU. PCN: 482-9526, MR73252. REPLACED PER TOMC, PRECAUTIONARY. CFDS TEST OF EIU, OK.Oct 6, 2012 · N468UA · Airbus A320232 · Central ComputersSDR UALA2012100805708Computer · faultyCHRONIC SLAT-FLAP ISSUES. REPLACED SFCC 1, GROUND TESTS OK. A-C TESTED TO 'FULL AUTOLAND' STATUS.Oct 6, 2012 · N468UA · Airbus A320232 · Trailing Edge Flap Control SystemSDR UALA2012100905715Switch · faultyF/O SIDESTICK PUSH TO TALK SWITCH STICKS-CREATES HOT MIKE. REPLACED F/O'S PTT SWITCH PER AMM, PERFORM OPS TEST OKAY.Oct 6, 2012 · N441UA · Airbus A320232 · Communications SystemSDR UALA2012100505662Director · defectiveCREW REPORTS: FWD CABIN CIDS CAUTION LIGHT ILLUMINATED AGAIN. REPLACED NR 2 CIDS DIRECTOR PER AMM. BITE TEST WAS NORMAL. NO FAULTS AND CIDS CAUTION LIGHT CLEARED.Oct 5, 2012 · N426UA · Airbus A320232 · Audio/Video MonitoringSDR UALA2012100505661Target · looseDOOR 1L IND NOT ARMED ON DOOR-OXY PAGE WITH DOOR HANDLE IN ARMED POS. FOUND PROX SWITCH 4WN1 TARGET LOCK NUT AND LOCKING TAB NOT INSTALLED. FOUND PARTS LOOSE IN DOOR. ADJUSTED TARGET AND INSTALLED TARGET NUT AND LOCKING TAB-WASHER PER AMM. OPERATIONAL TESTOct 5, 2012 · N419UA · Airbus A320232 · Door Warning SystemSDR UALA2012100805671Circuit Breaker · faultyL WING LEAK EICAS, FLIGHT DIVERTED. RESET CB D11, D12.Z22, Z23, F1, Q 7. NO FAULTS NOTED. PERFORMED BITE TEST OF BMC 1 & 2. NO FAULTS NOTED. PERFORMED IDLE RUN ON ENGINE 1 AND 2 FOR 5 MINS, RUNNING BOTH BLEED SYS. NO FAULTS NOTED.Oct 5, 2012 · N401UA · Airbus A320232 · Airfoil Anti/De-ice SystemSDR UALA2012100505641Control Unit · faultyNR 2 ENGINE TLA FAULT. DUE TO CHRONIC NR 2 ENGINE TLA FAULT "ENGINE 2 ONE TLA FAULT" HITTING SINCE 8-8-12 ACP TSM 76-00-00-810-802-B. THIS FAULT IS INTERMITTENT SO HARNESS MAY BE SUSPECT. POS PART TCU PCN 565-0099, EEC PCN 482-9588 (MR73908). REPLACED NR 2Oct 5, 2012 · N441UA · Airbus A320232 · Power LeverSDR UALA2012100805706Acoustic Panel · damagedNR 2 ENGINE HAS MISSING ACOUSTIC MATERIAL IN ENGINE INLET. PERFORMED REPAIR PER MT71 -006 REF CF9044 FOR PERM REPAIR AT 7 O'CLOCK POSITION.Oct 5, 2012 · N467UA · Airbus A320232 · Turbine Engine Air Inlet SectionSDR UALA2012100805707Unknown · odorFOUL ODOR IN CABIN ELECTRICAL PERHAPS. INSPECTED E AND E COMPARTMENTS AND PITS CABIN SEEMED TO HAVE URINE TYPE SMELL. DISCONNECTED PC AIR RAN PACKS CABIN SMELLS NORMAL.Oct 5, 2012 · N469UA · Airbus A320232 · Air Distribution SystemSDR UALA2012100805705Seal · displacedUPPER RIGHT WING TO BODY FAIRING FWD OF WING A PANELS 192BT AND 192AT HAS A 1 INCH SECTION OF SEAL MISSING. FLIGHT CREW FOUND ON PRE FLIGHT WALK AROUND. ACCOMPLISHED VISUAL INSPECTION OF PANEL AND SEAL. NO DAMAGE FOUND APPLIED 2 LAYERS OF SPEED TAPE PER EC-Oct 5, 2012 · N426UA · Airbus A320232 · Aerodynamic FairingsSDR UALA2012100505660Life Vest · missingLIFE VEST MISSING AT SEAT 8D. INSTALLED MISSING LIFE VEST AT SEAT 8D.Oct 4, 2012 · N453UA · Airbus A320232 · Life JacketSDR UALA2012100505653Power Supply · inoperativeCABIN EMERGENCY LIGHT TEST FAILED. SHOWS EPSU INT LOAD AFT LEFT AND EPSU EXT LOAD AFT LEFT. REPLACED AFT EPSU AND EPSU BATTERY, OP CHECK NORMAL.Oct 4, 2012 · N458UA · Airbus A320232 · Emergency LightingSDR UALA2012100505654Epsu · faultyFOUND UNIT FAULT ON FWD EMERGENCY POWER SUPPLY UNIT. REPLACED FWD EPSU AND EPSU BATTERY PER MM.Oct 4, 2012 · N458UA · Airbus A320232 · Emergency LightingSDR UALA2012100405634Wire · brokenEEL LIGHT AT LEFT CABIN WINDSCREEN BROKEN. REPIN WIRE IAW A319 -320 ESPM 20-48-25 WIRE #D002-20 LOCATION AT BOTTOM LEFT CORNER OF LEFT CABIN WINDSCREEN.Oct 3, 2012 · N460UA · Airbus A320232 · Light System WiringSDR UALA2012100305611Heat Exchanger · defectiveLEFT HEAT EXCHANGER DEFECTIVE. LEFT HEAT EXCHANGER INSTALLED.Oct 3, 2012 · N482UA · Airbus A320232 · Cabin Cooling SystemSDR UALA2012100405626Drain · not seatedSUSPECTED FUEL LEAK, RTFL. FOUND SUMP DRAIN LEAKING, RESEATED AND LEAK STOPPED.Oct 3, 2012 · N418UA · Airbus A320232 · Fuel StorageSDR UALA2012100405627Module · unsecureO2 MASKS OVER 29DEF DROPPED. O2 MODULE WAS DROOPING. THE O2 COMPARTMENT DOOR WAS NEVER OPEN, MASKS DID NOT DROP. RE-SECURED O2 MODULE.Oct 3, 2012 · N464UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2012100305614Power Supply · inoperativeLEFT AND AISLE EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WITH LOSS OF POWER. REMOVED AND REPLACED POWER SUPPLY UNIT AT LEFT EMERGENCY EXIT AND INSTALLED ROBBED BATTERY PACK.Oct 3, 2012 · N496UA · Airbus A320232 · Emergency LightingSDR UALA2012100305603Elt · faultyEMERGENCY LOCATOR TRANSMITTER CHECK & SERVICE. REMOVED ELT UNIT INSTALL NEW ELT UNIT.Oct 2, 2012 · N482UA · Airbus A320232 · Emergency Locator BeaconSDR UALA2012100305619Turbine Blades · crackedENGINE FAILED BORESCOPE INSPECTION DUE TO REPORTED 3EA T1 BLADES WITH RADIAL TIP CRACKS AND 1 EA T1 BLADE WITH AXIAL CRACK IN AREA "C" ON CONCAVE SIDE OF BLADES. REPLACED ENGINE.Oct 2, 2012 · N455UA · Airbus A320232 · Turbine SectionSDR UALA2012100505655Battery · failedEMERGENCY LIGHT TEST FAILS (SHOWS EMERGENCY AFT LEFT). REPLACED BATTERY. SYSTEM TEST OKAY, NO FAULTS NOTED.Oct 2, 2012 · N495UA · Airbus A320232 · Emergency LightingSDR GTIA20121001490Slide · low pressureR2 DOOR SLIDE PACK PRESSURE INDICATOR IS IN THE RED. R & R R2 DOOR ESCAPE SLIDE PACK ASSY IAW 25-62-44-000-012 AND AMM 25-62-44-400-007-A.Oct 1, 2012 · N611NK · Airbus A320232 · Escape SlideSDR UALA2012100105567O-Ring · leakingG RSVR LO LEVEL EICAS, FLT DIVERTED. PER CREW GROSS LANDING WEIGHT EXCEEDED BY 800 LBS. SAMC TEXT: CREW REPORTED SMOOTH TOUCHDOWN ABOUT 180 FT-MIN. ACCOMPLISH A OVERWEIGHT LANDING INSP. NO FAULTS NOTED RLAR AT 6 NOTIFIED. FOUND O-RING DAMAGED & LEAKING ONOct 1, 2012 · N462UA · Airbus A320232 · Hydraulic System, MainSDR UALA2012100305590Wire Harness · crushedEGT HARNESS CRUSHED (REF IPC 71-52-45 ITEM 83 OR 84) 6 INCHES FWD OF JUNCTION BOX IN CORE AREA. ON ENGINE NR 1, INSTALLED NEW EGT CORE HARNESS. HARNESS CLAMPS FROM JUNCTION BOX TO HALF WAY POINT ON HARNESS NEED TO BE INSTALLED AND HARNESS NEEDS TESTING PER MOct 1, 2012 · N440UA · Airbus A320232 · Engine Indicating System WiringSDR UALA2012100205568Controller · malfunctionedFUEL IMBALANCE OF 1200 LBS. REPLACED FQIC PER MM 28-42-34-400-001-A OPS CHECKED GOOD PER 28-46-00-740-001-AOct 1, 2012 · N483UA · Airbus A320232 · Fuel Quantity IndicatorSDR UALA2012093005546Skin · dentedMAJOR REPAIR: LEFT WING NR 4 SLAT DENTED ON LEADING EDGE NEAR OUTBOARD TRACK. MAJOR REPAIR ACCOMPLISHED: EVALUATED DENT & FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE. FABRICATED & INSTALLED FLUSH DOUBLER REPAIR REF SRM 57-40-00 FIG 225.Sep 30, 2012 · N460UA · Airbus A320232 · Leading Edge DevicesSDR UALA2012100105562Unknown · odorCIGARETTE SMOKE SMELL OFF AND ON IN AFT GALLEY. CHECKED ALL APPLIANCES IN AFT GALLEY AND BOTH LAVS FOR ELEC SYSTEM DISCREPANCIES. CHECKED APU INLET-EXH. CHECKED PACK INLETS AND ENGINES INLET-EXH. CHECKED AFT CARGO COMPT, NO MECH OR ELEC DISCREPANCIES OR EVSep 30, 2012 · N491UA · Airbus A320232 · Air Distribution SystemSDR UALA2012100205575Sliding Window · lack of lubeBOTH CAPT AND F/O SLIDING WINDOWS STUCK OPEN LUBED BOTH CAPT AND F/O SLIDING WINDOWS. OPS CHECK OK ON BOTH.Sep 30, 2012 · N417UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2012100105563Unknown · malfunctioned500 LBS OF FUEL MIGRATED BACK INTO CENTER FUEL TANK AFTER 4 HRS OF FLT TIME. DEBRIEFED CAPT & F/O AND BOTH BELIEVED FUEL IS TRANSFERRING FROM LEFT TANK TO CTR TANK DUE LEFT FUEL USAGE IS ABOUT 50 LBS AN HOUR GREATER. THEY BURNED THE 500 LBS TO 0 BUT ONE HOUR Sep 30, 2012 · N436UA · Airbus A320232 · Fuel Transfer ValveSDR GTIA20120929488Bottle · misinstalledL1 DOOR ASSIST BOTTLE FOUND UNARMED AND UNSAFETIED. DURING WEEKLY INSPECTION. ARMED AND SAFETIED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-860-002.Sep 29, 2012 · N601NK · Airbus A320232 · Passenger/Crew DoorsSDR UALA2012093005536Battery Pack · faultyEMERGENCY LIGHTS TEST PER 3 SVC WILL NOT PASS, GIVES MESSAGE EPSU BATTERY EMER R. REPLACED BATTERY PACK.Sep 29, 2012 · N466UA · Airbus A320232 · Emergency LightingSDR UALA2012093005540Skin · dentedFOUND ON ARRIVAL, DENTS 52 INCHES FWD OF DOOR 1L APPROX 1 INCH ABOVE THRESHOLD, DAMAGE AREA 5 BY 5 INCHES. MAJOR REPAIR ACCOMPLISHED: RE-EVALUATED DENTS REF SRM & FOUND OUT OF LIMITS. CUT OUT DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR REF SRMSep 29, 2012 · N460UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2012093005541Threshold · corrodedL-2 DOOR THRESHOLD AFT INBOARD CORNER CORRODED NEAR FRB68. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE AND FABRICATED & INSTALLED REPAIR ANGLE REF SRM53-41-14 FIG 201.Sep 29, 2012 · N460UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012093005542Threshold · corrodedR-2 DOOR THRESHOLD AFT INBOARD CORNER CORRODED NEAR FRB68. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE AND FABRICATED & INSTALLED REPAIR ANGLE REF SRM 53-41-14 FIG 201.Sep 29, 2012 · N460UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012100105548Hydraulic Line · leakingLOSS OF GREEN HYD SYSTEM ACCOMPLISH CHECK OF GREEN ENGINE DRIVEN PUMP FOR A POSSIBLE CAVITATION CONDITION. SEE TSM TASK 29-11-00-810-803-A FOR FURTHER TROUBLESHOOTING INFO. ACP CHECK OF EDP AND ALL SYSTEM DP'S ON FILTERS ALL GOOD. CREW COMMENTED WHEN THEY SSep 29, 2012 · N429UA · Airbus A320232 · Hydraulic System, MainSDR UALA2012100105561Sealant · deterioratedFUEL DRIPPING FROM RIGHT WING OUTBOAR FLAP CANOE. FOUND DETERIORATED SEALANT O/B SIDE OF CASTING THAT HOLDS FLAP TRACK FAIRING. CLEANED AFFECTED AREA AND RESEALED. ALSO RESEALED ENTIRE CASTING AREA AND CAP SEALED FASTENERS AS PRECAUTIONARY.Sep 29, 2012 · N409UA · Airbus A320232 · Wing Miscellaneous StructureSDR UALA2012093005537Scuff Plate · leakingPRESSURIZED AIRCRAFT TO 4 INCHES FOUND EVIDENCE OF PRESSURIZATION LEAKAGE AT LOWER DOOR SILL 2L MARKED AREA IN RED. RESEALED FWD AND AFT DOOR SCUFF PLATES.Sep 29, 2012 · N449UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2012100105553Idg · faultyAFTER GEAR EXTENSION ON APPROACH ALL CABIN LIGHTS FLICKERED UNTIL LANDING. REPLACED NR 2 IDG. LEAK CHECKED OPS CHECKED, DISCONNECTED, RECONNECTED & RAN NR 2 ENGINE SECOND TIME. ALL CABIN LIGHTS ARE GOOD.Sep 28, 2012 · N422UA · Airbus A320232 · AC Generator-Alternator
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