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 UALA2012040202039Seal · damagedON TOP OF LEFT WING TRAILING EDGE FLAPS APPEAR TO HAVE RUBBER SEAL PROTRUDING UP OUT OF WING. MADE INTERIM REPAIR REF MT 57-03.Apr 2, 2012 · N464UA · Airbus A320232 · Trailing Edge FlapsSDR UALA2012040202029Connector · damagedPAX REPORTED SPARKING AND A ODOR OF SMOKE. FOUND CONNECTOR ON SEU AT ROW 29ABC BURNED. REPLACED SEU AT 29ABC, CHECK GOOD.Apr 2, 2012 · N433UA · Airbus A320233 · Communications System WiringSDR UALA2012040202048Oil System · leakingAPU WET WITH OIL IN AREA AROUND BURNER SECTION. SUSPECT INTERNAL OIL LEAK IN THE EXHAUST SECTION. APU DOES NOT LEAK OIL WHEN SHUTDOWN. REPLACED APU, OPS CHECKED GOOD. NO LEAKS.Apr 1, 2012 · N468UA · Airbus A320232 · APU Oil SystemSDR UALA2012040202058Converter · faultyCAPTAIN'S WINDSHIELD WIPER WILL NOT TURNOFF. REPLACED CAPT WINDSHIELD WIPER MOTOR CONVERTER. MOTOR NOW SHUTS OFF AND PARKS WILL ONLY RUN IN HIGH, GOES TO PARK WHEN IN LOW.Apr 1, 2012 · N432UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR GTIA20120331392Power Supply · faultyEPSU (11WL) EMER L/ DEU B (300RHG) FAULT. TROUBLESHOT IAW TSM 33-51-00-810-858-A. R & R EPSU IAW AMM 33-51-38-000-001-A & 33-51-38-400-001-A AND EPSU BATTERY IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. PERFORMED TEST IAW AMMMar 31, 2012 · N608NK · Airbus A320232 · Emergency LightingSDR UALA2012040202049Window · damaged1ST OFFICER'S SLIDING WINDOW'S VISIBILITY IS IMPAIRED. CLEANED WINDOW FOR BETTER FLIGHT VISIBILITY, WINDOW WITHIN LIMITS. BUBBLES DO NOT IMPAIR FLIGHT VISIBILITY.Mar 31, 2012 · N463UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2012040202059Computer · failedAILERON SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED NR 2 ELAC PER AMM. ACCOMPLISHED TEST PER MM TASK. LAND III CAPABILITY TEST PER AMM. ALL TESTED OK. EFCS-1 & EFCS-2 GROUND SCANS RECORDED NO FAULTS. ORD TST NOTED DURING CONFERENCE CALL THAT UNIMar 31, 2012 · N442UA · Airbus A320232 · Flight Control SystemSDR UALA2012033001991Windshield · faultyLEFT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. - ANTI ICE. CAPTS WINDSHIELD HEAT INOP. VERY CHRONIC, ALREADY USING SPARE SENSOR. REMOVED AND REPLACED LEFT WINDSHIELD PER MM.Mar 30, 2012 · N485UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2012033001992Battery · failedEMERGENCY TEST FAILS. REPLACED EEL BATT 11WL. SYS OPS CHECK NORMAL.Mar 30, 2012 · N485UA · Airbus A320232 · Emergency LightingSDR UALA2012040202042Windshield · faultyLT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN - ANTI ICE. REMOVED AND REPLACED LT WINDSHIELD PER MM.Mar 30, 2012 · N485UA · Airbus A320232 · Flight Compartment WindowsSDR UALA2012033001983Support Bracket · crackedRIGHT AIR COND BAY, HEAT EXCH AFT UPPER SUPPORT BRACKET, ATTACHED TO CTR WING LWR SKIN IS CRACKED AT FWD INBD CORNER OF THE BRACKET. VERIFIED WITH HFEC. INSTALLED NEW FITTING. STATIC LEAK CHECKED OK.Mar 29, 2012 · N406UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012033002003Oil Cooler · failedNR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. FOUND FUEL ON OIL SIDE OF FCOC, REPLACED FUEL CONTROL OIL COOLER PER MM.Mar 29, 2012 · N423UA · Airbus A320232 · Engine Oil CoolerSDR UALA2012032801952Bolt · backed outENG 2 - TAIL CONE HAS 7 (OF 13) ATTACH BOLTS BACKED OUT AS FOLLOWS (CLOCK POSITION, DISTANCE BACKED OUT): 2:45, 3-16": 3:30, 1-8": 4:30, 1-8": 5:30, 3-16": 6:30, 1-8": 7:30, 7-32": 9:15, 5-32". FROM BASE WRITE-UP U5015K. CHECK TURBINE EXH CASE SHANK NUTS ANDMar 28, 2012 · N405UA · Airbus A320232 · Engine Collector/Tailpipe/NozzleSDR UALA2012032901971Girt Bar · out of adjustDOOR 2L WILL NOT INDICATE ARMED. ADJUSTED GIRT BAR, OPS CHECK OKAY.Mar 28, 2012 · N402UA · Airbus A320232 · Emergency EquipmentSDR UALA2012032901973Connector · not seatedUNABLE TO UPLOAD WATER. :WHEN OPENING AFT PANEL FILL VALVE THE FWD DUMP VALVE THE FWD SVC PANEL DRIVES TO OPEN AND DUMPS THE WATER RENDERED POTABLE WATER SYS INOP PER MEL 38050. RESET CB'S AND RESEAT CONNECTOR OF 16MA MOTOR GRD CHK NORM. RETURNED SYS BACK TMar 28, 2012 · N469UA · Airbus A320232 · Water/Waste System WiringSDR UALA2012032701933Battery · faultyEMERGENCY BATTERY R FAULT. REPLACED BATTERY AT 12WL PER AMM.Mar 27, 2012 · N435UA · Airbus A320232 · Emergency LightingSDR UALA2012032801957Wire Harness · damagedCAPTAIN'S WINDSHIELD HEAT IS INOPERATIVE. SYSTEM CHECKEDS NORMAL WHILE AT THE GATE. INSTALLED WINDSHIELD HEAT WIRING HARNESS PER AMM. TEST PER TASK. TESTS OKAY.Mar 27, 2012 · N485UA · Airbus A320232 · Ice/Rain Protection System WiringSDR UALA2012032701940Clamp · looseANTI-ICE VALVE LEAKING HOT AIR ONTO NOSE COWL CAUSING DELAMINATION OF NOSE COWL. NR 1 ENGINE ANTI-ICE VALVE FOUND ONE CLAMP NOT SECURED. THIS CAUSED THE AFT BULKHEAD HEAT SHIELD TO COME APART BEHIND THE ANTI-ICE VALVE.Mar 26, 2012 · N403UA · Airbus A320232 · Ice/Rain Protection SystemSDR UALA2012032701944Sensor · out of adjustACFT WANTS TO PULL HARD TO THE RIGHT DURING TAXI, ACFT REQUIRES 8.7 UNITS OF LEFT RUDDER TRIM TO TAXI STRAIGHT. REPLACED LT SENSOR AND ADJUSTED PER MM. TAXIED ACFT STEERS STRAIGHT.Mar 26, 2012 · N434UA · Airbus A320232 · Rudder Control SystemSDR UALA2012032601923Computer · faultyLEFT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. REPLACED WINDOW HEAT COMPUTER PER MM.Mar 25, 2012 · N485UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR UALA2012032601889Slide · faultyEMERGENCY LIGHTS TEST WILL NOT PASS, GIVES EXT LOADS AFT LEFT MESSAGE. USED SLIDE CONNECTOR TEST PLUG, FOUND DOOR 2R SLIDE BAD. REPLACED DOOR 2R EMERGENCY SLIDE PACK PER AMM, OPS NORMAL TEST GOOD.Mar 24, 2012 · N433UA · Airbus A320232 · Escape SlideSDR UALA2012032601895Strap · exposed2L DOOR YELLOW RELEASE STRAP HAS EXCESS STRAP STICKING OUT OF GIRT ASSEMBLY. REF AMM. ACCOMPLISHED ROUTING OF YELLOW RELEASE STRAP REF AMM, OPS CHECKED GOOD.Mar 24, 2012 · N409UA · Airbus A320232 · Escape SlideSDR UALA2012032601888Hose · brokenFWD GALLEY CHILLER HAS A BROKEN HOSE IN DRAIN LINE. INSTALLED FWD GALLEY CHILLER AS PER MM, OPS CHECKED GOOD.Mar 24, 2012 · N432UA · Airbus A320232 · Buffet/GalleysSDR UALA2012032601924Valve · leakingFUEL SLOWLY DRIPPING FROM UNDERSIDE OF LEFT WING. APPROX HALFWAY DOWN FROM THE FUSELAGE FOUND LEFT WING OTBD WATER SUMP VALVE LEAKING. RESET SUMP POPPET VALVE. LEAK CORRECTED.Mar 24, 2012 · N430UA · Airbus A320232 · Aircraft Fuel SystemSDR UALA2012032601916Engine · stalledNR 1 ENG STALL ECAM. ACCOMPLISHED FUNCTIONAL CHECKS OF THE HPC 7TH STAGE A, B & C SOLENOID VALVES PER AMM, HPC 7TH STAGE BLEED VALVES PER AMM. HPC 10TH STAGE SOLENOID VALVE PER AMM AND 10TH STAGE BLEED VALVE PER AMM. ACCOMPLISHED ALL TASKS IN TSM 71-00-00-81Mar 24, 2012 · N404UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR UALA2012032601908Oxygen Mask · unwanted deployCREW REPORTED O2 MASK DEPLOYED AT ROW 36 DEF. STOWED MASK LATCH AND CLOSED NORMAL. ACCOMPLISHED 02 MASK DROP CHECK. IAW AMM.Mar 23, 2012 · N428UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2012032301860Doubler · faultyEXISTING SKIN DOUBLER AT FR 73- 74, STR 31R-33R.33R. REMOVED EXISTING RPR AND INSTALLED NEW DOUBLER RPR PER SRM.Mar 22, 2012 · N423UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2012032301861Skin · damagedJIC 49795401C DURING HMV 3 VISIT REQUIRES LT AIRPHONE ANTENNA REMOVED AND SKIN DOUBLER INSTALLED. MAJOR REPAIR ACCOMPLISHED: INSTALLED SKIN DOUBLER PER SRM. SRI REQUIREMENTS REF SRI 53-00-11-TABLE 219. INSTALLED SKIN DOUBLER.Mar 22, 2012 · N423UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2012032301862Skin · damagedPER JIC 49795401C REQUIRES REMOVAL OF RT AIRPHONE ANTENNA AND SKIN DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: REMOVED AIRPHONE ANTENNA & INSTALLED SKIN DOUBLER. THIS ITEM ACCOMP COA 40795C.Mar 22, 2012 · N423UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2012032301864O-Ring · damagedHIGH PITCH SOUND IN CEILING AT ROW 20. REMOVED UPPER BEACON ASSY 7LY. FOUND O-RING DAMAGED. REPLACED PACKING ITEM 90 ON IPC PER MM33-48-11. PRESSURIZED A-C NO LEAK AND HIGH PITCH SOUND NOTED.Mar 22, 2012 · N412UA · Airbus A320232 · Exterior LightingSDR UALA2012032201823Battery Pack · failedEPSU BATTERY FAILED DOOR 1L. REPLACED EPSU BATTERY PACK PER MM, OPS TEST GOOD.Mar 21, 2012 · N447UA · Airbus A320232 · Emergency LightingSDR UALA2012032201826Power Supply · faultyEMERGENCY LIGHTS IN CABIN ARE VERY DIM AND EPSU WILL NOT SELF TEST. RMVD & RPLD EPSU, OP CHECKS GOOD IAW A320 MM ON N-R V9255I.Mar 21, 2012 · N423UA · Airbus A320232 · Emergency LightingSDR UALA2012032201839Stringer · corrodedSTR 43L AT FRAME 63 HAS CORROSION. MAJOR REPAIR. INSTALLED STRINGER REPAIR PER SRM.Mar 21, 2012 · N423UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2012032301849Transceiver · faultyNR 1 RADIO TRANSMIT BROKEN-UNINTELLIGIBLE MULTIPLE FREQS AND MICS. NEEDS VHF TRANSCEIVER. SWAPPED POSITION 2 WITH POSITION 3, NOW VHF-1 NORMAL. VHF-2 S-N 3393, VHF-3 S-N 3623, VHF-1 S-N 4612. VHF FAULT SEEMS TO BE VOICE TRANSMISSION PROBLEM ONLY, ACARS DATMar 21, 2012 · N401UA · Airbus A320232 · VHF Communications SystemSDR UALA2012032001794Computer · faultyVIBRATION NOISE ENCOUNTERED IN FLIGHT. REF FLT MANUAL 12.20.1 NEED TO COMPLETE VIBRATION REPORTING CHECKLIST AND DEBRIEF MAINTENANCE (SAMC) ON ARRIVAL TO DESTINATION STATION CREW COMMENTS: CONT...FL320-285KTS.78-148.4GW. PUT IN SLIGHT RUDDER BOTH L+R AND SMMar 20, 2012 · N434UA · Airbus A320232 · Elevator Control SystemSDR UALA2012032001803Connector · unsecureFUELER REPORTS NO PWR TO REFUEL PANEL. DOOR SWITCH 565-1239 20QU CIRCUIT BREAKER 2QU 565-0531 28VDC 4023VC PIN Y. FOUND BAD CONNECTION, SECURED, REF WDM 28-25-01 PG2 AND ASM 24-67-00 SCH1. OPS CK'S GOOD. NO FAULTS NOTED, HAVE POWER TO REFUEL PANEL.Mar 20, 2012 · N471UA · Airbus A320232 · Fuel System WiringSDR UALA2012032001808O-Ring · leakingACP MT 72-022 AND MT 72-033. FOUND BAD O-RING AT RT SIDE OIL LINE AT LAST CHANCE STRAINER. RPL O-RING. ACCOMPLISHED NON-RII BORESCOPE PER MT 72-022. NO COKING FOUND.Mar 19, 2012 · N438UA · Airbus A320232 · Turbine Engine Oil SystemSDR UALA2012032001809Scavenge Pump · damagedAFTER SHUTDOWN RAMP NOTIFIED CREW OF FIRE IN TAIL CONE OF ENG 2. FIRE LASTED FOR 5 MINS. PER OPBLM REPLACE OIL SCAV PUMP NR 2 ENG. REMOVED PUMP. REPLACED SCAVENGE PUMP PER MM AND SCAVENGE VALVE PER MM, RAN ENGINE OPS CHECK OK.Mar 19, 2012 · N438UA · Airbus A320232 · Turbine Engine Oil SystemSDR UALA2012031901755Fitting · gougedFWD CARGO DOOR FUSELAGE FITTING AT NR 4 LATCHING ROLLER, AFT LUG GOUGED. BLENDED GOUGE PER SRM AND MAT'L REMAINING IS WITHIN LIMITS.Mar 18, 2012 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012031901757Fitting · gougedFWD CARGO DOOR FUSELAGE FITTING AT NR 2 LATCHING ROLLER, FWD LUG GOUGED. BLENDED GOUGE PER SRM AND MAT'L REMAINING IS WITHIN LIMITS.Mar 18, 2012 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012031901759Fitting · chafedFWD CARGO DOOR FUSELAGE FITTING AT NR 3 LATCHING ROLLER, FWD LUG CHAFED. BLENDED CHAFED AREA PER SRM AND MAT'L REMAINING IS WITHIN LIMITS. DAMAGE REWORKED PER SRM ON NON ROUTINE.Mar 18, 2012 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012031901761Fitting · chafedFWD CARGO DOOR FUSELAGE FITTING AT NR 5 LATCHING ROLLER, AFT LUG CHAFED. BLENDED CHAFED AREA PER SRM AND MAT'L REMAINING IS WITHIN LIMITS. DAMAGE REWORKED PER SRM 53-26-00, FIG 101 ON NON ROUTINE.Mar 18, 2012 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012031901763Fitting · chafedFWD CARGO DOOR FUSELAGE FITTING AT NR 6 LATCHING ROLLER, AFT LUG CHAFED. BLENDED CHAFED AREA PER SRM, FIG. 101 AND MAT'L REMAINING WITHIN LIMITS. DAMAGE REWORKED PER SRM ON NON ROUTINE.Mar 18, 2012 · N418UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012031901786Fan · failedAFTER TOW OVER TO GATE UNABLE TO SILENCE AEVC HORN. ACP TEST IN CFDS FOUND EXTRACT FAN 18HQ FAILED, WITH AEVC HORN SOUNDING. ACP MEL 2126S CREW MUST RESET HORN CB P9 AFTER ENG START. REPLACED FAN 18HQ, OPS CHECK GOOD.Mar 18, 2012 · N415UA · Airbus A320232 · Air Distribution FanSDR UALA2012031901762Actuator · faultyNEED TO REPLACE L/G ELEV SERVO ACT. REMOVED L/G ELEV SERVO ACT PER MM. INSTALLED L/G ELEV SERVO ACT. NEED TO INSTALL COTTER PIN 25, 20, AND LOCKING CAP 19 PER 27 34-51 PG 428. THEN CONT 27-34-51 PG 431 STEP D TIL END. MR27350 DASH OFF 421 DASH ON 69. ACCMar 18, 2012 · N409UA · Airbus A320232 · Elevator Control SystemSDR UALA2012031901764Computer · faultyINSTALLED NEW ELAC 2 STILL HAVE A HARD FAULT. MR27935-280 INSTALLED. OLD ELAC IS MR27935-232. ACCMP'D AFS LAND TEST. GROUND OPS CHECK GOOD.Mar 18, 2012 · N409UA · Airbus A320232 · Elevator Control SystemSDR UALA2012031901752Slat · damagedDAMAGE FOUND ON LT NR 2 SLAT. REPLACED NR 2 SLAT.Mar 18, 2012 · N427UA · Airbus A320232 · Leading Edge DevicesSDR UALA2012031901785Cone · crackedCAPTAIN REPORTS NR 1 ENG HAS SEVERAL CRACKS ON EXHAUST CONE. REPLACED NR 1 ENG EXHAUST CONE PER MM.Mar 17, 2012 · N433UA · Airbus A320232 · Engine Collector/Tailpipe/NozzleSDR GTIA20120316385Bottle · low pressureR1 DOOR ASSIST BOTTLE HAS LOW PRESSURE. R1 DOOR ASSIST BOTTLE SERVICED IAW AMM 52-10-00-614-001.Mar 16, 2012 · N606NK · Airbus A320232 · Passenger/Crew DoorsSDR UALA2012031901743Switch · stuckEMERGENCY EXIT LIGHT SWITCH STUCK IN OFF POSITION. REPLACED EMERGENCY EXIT LIGHT SWITCH 4WL, CHECKS GOOD.Mar 16, 2012 · N427UA · Airbus A320232 · Emergency Lighting
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