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 UALA2012020200627Oxygen Mask · deployedO2 MASKS DEPLOYED AT 25ABC, GENERATOR NOT ACTIVATED. STOWED MASKS. PER MT 35-003 MASKS MUST BE DROP CHECKED WITHIN 3 DAYS. -SEC- :ACP'D DROP CHK OF O2 MASKS, PER MT 35-003. OPS CHECK NORMAL.Jan 31, 2012 · N433UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2012020200656Lanyard · unsecureDOOR 1L ARMING LEVER CANNOT BE MOVED TO THE ARMED POSITION. RE-SECURED LANYARD ON GIRT BAR AT 1L. ACP OPS CHECK NORMAL.Jan 31, 2012 · N461UA · Airbus A320232 · Escape SlideSDR UALA2012020200612Director · malfunctionedCIDS MAINT TEXT: CREW REPORTED EVAC WARNING SOUNDING AND COULD NOT RESET. REPLACED CIDS DIRECTORS NR 1 AND NR 2. BOTH CIDS DIRECTORS PASSED. CONFERRED WITH TOMC.Jan 30, 2012 · N414UA · Airbus A320232 · Audio/Video MonitoringSDR UALA2012020200614Oxygen Mask · brokenF/O O2 MASK INFLATABLE HARNESS UPPER BRACKET IS BROKEN. REPLACED F/O O2 MASK ASSY PER AMM.Jan 30, 2012 · N456UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012020200613Sill · corrodedMAJOR REPAIR. CORROSION ON L2 DOOR SILL AT FR 68 AT 2 EA FASTENER HOLES. REPAIRED PER SRM 53-41-14 FIG 201 SHEET 3. MUST BE REINSPECTED PER SRI 53-41-41 PG 203-204 AT 92731 FC OR 208644FH FROM REPAIR EMBODIMENT. CURRTG PTC 14814 AND PTT 35900. SHOULD READ 53Jan 30, 2012 · N473UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012013000588Light · defectiveBOTH AFT LAV VANITY LIGHT COVERS DISCOLORED TO THE POINT THAT ITS DARK IN LAVS. STILL ALLOWS SATISFACTORY LIGHT TO PASS, COVERS NEED REPLACEMENT WITHIN 20 DAYS. REPLACED LENS BOTH LAVS.Jan 28, 2012 · N437UA · Airbus A320232 · Passenger Compartment LightingSDR UALA2012013000598Smoke Detector · faultySMOKE - LAVATORY DET FAULT ON UPPER ECAM. REPLACED LAV 'A' DETECTOR. CIDS AND SDCU GROUND TESTS OKAY.Jan 27, 2012 · N436UA · Airbus A320232 · Smoke DetectionSDR UALA2012012700570Valve · faultyVENT SKIN VLV FAULT, RTFL.Jan 27, 2012 · N409UA · Airbus A320232 · Cabin Cooling SystemSDR UALA2012012700557Stringer · corrodedSTR 31R AT FRAMES 65 AND 66 IS CORRODED BELOW OUTFLOW VALVE. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER IAW SRM 51-42-11. PANEL 162CW INSTALLED PER SRM 51-42-11. RIVETS HEAT TREATED PER UAL GNMM 1-0-7-003 REF NR E4327I.Jan 26, 2012 · N427UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2012012700568Oxygen Mask · leakingF/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). CREW COMMENTS: F/O O2 MASK FAILS SELF TEST. REPLACED WITH SERVICEABLE UNIT. OPS AND LEAK CHECK GOOD.Jan 26, 2012 · N462UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012012600535Rudder · faultyDURING VACUUM LOSS INSPECTION (DONE BY AIRBUS) IT WAS NOT POSSIBLE TO APPLY VACUUM TO ONE OF THE INSP HOLES. CHECKS ACP ON PTT SEQUENCE 7962015. REF CF9015 REMOVED RUDDER. NEED TO INSTALL NEW RUDDER. INSTALLED HINGE BOLTS ONLY. BOLTS NOT TORQUED. ACP'D Jan 26, 2012 · N483UA · Airbus A320232 · Rudder Control SystemSDR UALA2012013000591Engine · contaminatedLARGE OIL LEAK ON ENG 2 SAMC TEXT: IDENTIFY FLUID TYPE & LEAK SOURCE. ACP CHECK OF THE ENGINE. FOUND NO LEAK SOURCE. CHECKED OIL AT TANK, TANK IS FULL. COCKPIT INDICATION INDICATES 21 QTS. REVIEW OF PLN OIL SHOWS OIL USE AT 0.07 QTS PER HR (WELL WITHIN LIJan 26, 2012 · N431UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR UALA2012012300460Pump · faultyREMOVED RAT REF AMM 29-22-51, DUE TO EQ CALLOUT. REMOVED RAT. REPLACED RAT & PUMP.Jan 23, 2012 · N443UA · Airbus A320232 · Hydraulic Pump, AuxiliarySDR UALA2012012400502Valve · out of sequenceSKIN AIR OUTLET VLV FAULT, RTFL DISPLAYED ON UPPER ECAM. OVERWEIGHT LANDING SPEED 142 KNOTS, 300 FPM DESCENT. LANDING WEIGHT 152000 LBS. BASED ON THE INFORMATION AND PER MM, NO INSPECTION IS REQUIRED. SKIN AIR OUTLET VALVE WAS OUT OF SEQUENCE WITH INLET VJan 23, 2012 · N409UA · Airbus A320232 · Pressure Regulator/Outflow ValveSDR UALA2012012400504Container · defectiveTHE 23DEF O2 MASKS FELL DOWN. LATCH FOR O2 DOOR WON'T HOLD. KEEPS POPPING BACK OPEN WITH BUMP OF BIN. APPLIED MEL3521A. REPLACED CONTAINER ASSY AT 23DEF & OPS CHK PER MM. PERFORM DROP TEST.Jan 23, 2012 · N426UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2012012300481Oxygen Mask · unsecureO2 MASKS DROPPED AT MID CABIN, CONTACT CREW FOR LOCATION. ACCOMPLISHED MT35-003 AND FOUND NO DISCREPANCIES WITH DOOR, LATCH OR O2 MASKS. REPACKED MASKS AND ACCOMPLISHED DROP CK AS REQUIRED. WILL NEED MANUAL DROP CHECK WITHIN A MAX OF 3 DAYS. O2 MASKS ARE LJan 22, 2012 · N407UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2012012000430Ram Air Turb · damagedREF EQ3075, FOUND BOTH RAM AIR TURBINE BLADES WITH WEAR MARKS IN LEADING EDGES, 3IN FROM HUB. WEAR IS 1-8\ DIA X .002' DEEP, NO RELIEF. WEAR HAS BEEN CAUSED BY CROSS MEMBER IN RAM AIR TURBINE STORAGE WELL, WEAR DAMAGE ON CROSS MEMBER IS APPROX 3-16\W X 1-8\DJan 20, 2012 · N423UA · Airbus A320232 · Hydraulic System, AuxiliarySDR UALA2012012300472Battery · faultySOME EMERGENCY EXIT LIGHTS ON WITH SWITCH IN OFF POSITION EPSU BATT AFT L MESSAGE ON PTP. REPLACED EPSU BATTERY PER MM. OPS CHECK GOOD.Jan 20, 2012 · N467UA · Airbus A320232 · Emergency LightingSDR UALA2012012300443Control Unit · faultyLEFT FUEL IS 1100 LBS LESS THAN RIGHT TANK DURING CRUISE AND DESCENT. FUEL ERROR READING LEFTW-49 RIGHT W-2400. BURN EQUAL AND LOAD EQULAT TAXI. TROUBLESHOOT REF TSM. SWAPPED FLSCU 1&2 SYS TEST NO FAULTS. TESTED FUEL TRANS VLVS PER TSM. NO LEAKS NOTED NEJan 19, 2012 · N406UA · Airbus A320232 · Fuel Transfer ValveSDR UALA2012011900395Skin · damagedTWO EXTERNAL SKIN DOUBLERS INSTALLED AT FR63 - 64 AT FORMER L-BAND ANTENNA LOCATIONS PER COA40795C AND SRM 53-00-11 FIG 238. MAJOR REPAIR ACCOMPLISHED. DOUBLERS INSTALLED PER JC 97954010 BY 396114 AND LC-09. PER SRI 53-00-11 TABLE 219 DOUBLERS REQUIRE FIRSTJan 18, 2012 · N421UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2012011900416Computer · faultyELEVATOR-AILERON COMPUTER (ELAC) 2 FAULT LIGHT INOP - F-CTL REPLACED ELAC 2. INTERMITTANT FLT-CTL ELAC 2 PITCH FAULT. SAMC TEXT: POST FLIGHT SHOWS "L POS PEDAL XDUCER UNIT". ITEM NUMBER 25CE1. PLEASE REPLACE IAW AMM. REPLACED L POS PEDAL XDUCER UNIT. NO FAJan 18, 2012 · N443UA · Airbus A320232 · Elevator Control SystemSDR UALA2012011800377Valve · faultyUNWANTED FUEL USE FROM RT WING. *SUPPLEMENTAL DATA UPDATE* OPBLM PROG TEXT: - ITEM ROLLED FORWARD. SAMC TEXT: APPROX 900 LBS IMBALANCE DURING A 3 HOUR FLT IAD- SJU. WORK WITH LM2750. OPBLM. REPLACED LEFT WING REFUEL VALVE SEE SEQ 9582001.Jan 18, 2012 · N406UA · Airbus A320232 · Aircraft Fuel Distribution SystemSDR UALA2012011700357Transmitter · faultyCREW COMMENTS: GOT BRAKES AUTO BREAK FAULT ECAM AFTER TAKEOFF. AUTO BRAKE FUNCTION INOP - BRAKES. EXTENSIVE HISTORY OF BRAKE SYSTEM 1 FAULTS. COMPLIED WITH MEL AFTER ACCOMP PFR. SUSPECT BRAKE PETAL XMITR 565-9200 NIL DEN. TROUBLESHOT PER TSM. AC TROUBLESJan 17, 2012 · N412UA · Airbus A320232 · Landing Gear Brake SystemSDR UALA2012011700358Structure · out of limitsFUSELAGE DENT FR 57-58 STR 25R-26R. FOUND TO BE OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR IAW SRM. WORKED ON W-U V0931J.Jan 16, 2012 · N421UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2012011600325Fastener · wrong partCOMPARTMENT 107 IN FWD GALLEY HAS WRONG SIZE QUARTER TURN. FOUND CORRECT QTR TURN INSTALLED.Jan 15, 2012 · N435UA · Airbus A320232 · Buffet/GalleysSDR UALA2012011600314Battery · faultyEMERGENCY LIGHT TEST FAILS TEST WITH MESSAGE 'EPSU BATTERY EMER R' AND 'EPSU BATTERY EMER L'. PERFORMED SELF TEST OF LEFT AND RIGHT OVERWING EPSU'S. EACH EPSU FAULTED BATTERY. REPLACED LEFT AND RIGHT OVERWING EPSU BATTERIES REF MM. ACCOMPLISHED SELF TEST OJan 14, 2012 · N424UA · Airbus A320232 · Emergency LightingSDR UALA2012011600315Battery · failedEMERGENCY LIGHT TEST FAILED 33-51-38 EPSU BATTERY EMER R. TS TO BAD AD-3214-30 BATTERY. REPLACED WITH PCN 565-0033 BATTERY PER MM. RETEST OF EMER LIGHTS TEST OK.Jan 14, 2012 · N473UA · Airbus A320232 · Emergency LightingSDR UALA2012011600331Transmitter · leakingHYDRAULIC LEAK COMING FROM MAIN GEAR WHEEL WELL. LEAK COMING FROM BASE OF HIGH PRESSURE TRANSMITTER, ON YELLOW SYS MODULE. ADJACENT TO YELLOW SYS RES. REPLACED TRANSMITTER PER AMM. NO LEAKS NOTED.Jan 13, 2012 · N420UA · Airbus A320232 · Hydraulic Pressure SensorSDR UALA2012011300275Warning Light · illuminatedRAT FAULT DISPLAYED ON UPPER ECAM SCREEN. RAT AND EMERGENCY GENERATOR FAULT LIGHT ON PROGRAM TEXT: WORK WITH LM2730. SEE PTT 7922001 FOR BCL 1 REPLACEMENT.Jan 13, 2012 · N475UA · Airbus A320232 · Hydraulic System, AuxiliarySDR UALA2012011300276Seat · defectiveFIRST OFFICER SEAT, MANUAL HORIZONTAL ADJUSTMENT DEFECTIVE. REPLACED SEAT ASSY.Jan 13, 2012 · N428UA · Airbus A320232 · Flight Compartment EquipmentSDR UALA2012011200258Control Valve · malfunctionedGROUND RETURN AND CANCELLATION DUE TO INOPERATIVE PACK. PACK 1 FAULT LIGHT INOP - AIR AIR. PROG TEXT: - ITEM ROLLED FORWARD. NR 1 PACK FLOW CONTROL VALVE REPLACED AND REPLACED SOLENOIDS 7170HM1, 10HA1. SWAPPED BOTH SDACS, PERFORMED CATIII CHECK. ACFT PACJan 12, 2012 · N472UA · Airbus A320232 · Cabin Cooling SystemSDR UALA2012011100229Skin · wornEXTERNAL FUSELAGE FRAME 34 STR 43L - FUSELAGE SKIN HAS DEEP WEAR FROM SCREW. ACP'D ON DOCK WU E5765G BY AMTS 38425, 054888, 181147, 163495. RPR'D PER SRM.Jan 10, 2012 · N401UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2012011200261Control Valve · failedPACK 2 FAIL ON LANDING ROLL OUT. REPLACED NR 1 PACK FLOW CONTROL VALVE PER MM, OPS CHECKED GOOD.Jan 10, 2012 · N431UA · Airbus A320232 · Cabin Cooling SystemSDR UALA2012010900187Skin · dentedRIGHT FUSELAGE 27' AFT OF R2 DOOR THRESHOLD, DENTED. MEASURING APPROX 3.5 W X 3.0 L. DEPTH IS APPROX .093. DENT LOCATED FUSELAGE FRAME BETWEEN FR69 AND FR70 ABOVE STRINGER 23R. REPAIRED SKIN.Jan 9, 2012 · N443UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2013010900156Battery · failedCABIN EMERGENCY LIGHTS TEST FAILED. REPLACED EPSU BATTERY AT 10WL POSITION ACP'D OP TEST PER AMM, OKAY.Jan 8, 2012 · N484UA · Airbus A320232 · Emergency LightingSDR GTIA20120107328Cylinder · low pressureR-1 DOOR BOTTLE PRESSURE LOW. SERVICED R-1 DOOR EMERGENCY ACCUMULATOR AS REQ IAW AMM 52-10-00-614-001. NO FURTHER DEFECTS NOTED.Jan 7, 2012 · N606NK · Airbus A320232 · Passenger/Crew DoorsSDR GTIA20120107329Cylinder · low pressureL1 CREW/PAX DOOR CYL DAMPER PRESSURE LOW. SERVICED L-1 CREW PAX DOOR CYL DAMPER PRESS IAW AMM TASK 52-10-00-614-001-A.Jan 7, 2012 · N602NK · Airbus A320232 · Passenger/Crew DoorsSDR UALA2012010900188Skin · dentedDENT IN FUSELAGE SKIN BETWEEN FR9 AND FR10 AT STR 22L. DOUBLER REPAIR INSTALLED PER SRM. RPR REQ'S INSPECTION AT 60000 CYC AFTER REPAIR EMBODIMENT WITH SUBSEQUENT INSP'S TBD PER SRI 53-11-11 PAGE 213-214 TABLE 204. FIRST INSP REQ'D AT PTC 81944.Jan 7, 2012 · N413UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2012010900197Oxygen Mask · no testCAPTS O2 MASK FAILS TEST. REPLACED MASK TESTED, OPS NORMAL.Jan 7, 2012 · N437UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012010900199Pinion · failedCAPTAIN'S RUDDER PEDAL ADJUSTMENT INOPERATIVE. PEDALS DO NOT SPRING BACK FROM FULL FWD POS WITH HANDLE. REPLACED THE AIR PINTON, OPS CHECKED GOOD.Jan 7, 2012 · N428UA · Airbus A320232 · Rudder Control SystemSDR UALA2012010900198Windscreen · faultyR WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. RIGHT WINDSHIELD SENSOR WITHIN TOLERANCE PER TSM 30-42-00-810-804. REPLACED RIGHT WINDOW HEAT CONTROLLER PER MM. REPLACED FIRST OFFICER WINDSCREEN. ANTI-ICING AND DEFOGGING SYSTEM TEST CHECKS GOOD PER MM.Jan 5, 2012 · N489UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR UALA2013010900174Power Supply · no testEMERGENCY LIGHT TEST FAULT, "EXT LOAD EMER R" ON CIDS. RIGHT OVERWING EMERGENCY POWER SUPPLY WILL NOT TEST. REPLACED EPSU PER MM AND BATTERY PER MM. EPSU AND EMERGENCY LIGHT SYSTEM OPS TEST NORMAL.Jan 5, 2012 · N401UA · Airbus A320232 · Emergency LightingSDR UALA2012010600147Light · inoperativeEMERGENCY LIGHT FAILED EPSU EXT LOAD. FOUND RT OVERWING EXIT AFT LIGHT FWD BULB INOPERATIVE. RELAMPED, NO HELP. REPLACED RT AFT OVERWING EMERGENCY SLIDE LIGHT ASSEMBLY.Jan 4, 2012 · N424UA · Airbus A320232 · Emergency LightingSDR UALA2012010500110Lamp · inoperativeEMERGENCY LIGHT FAILED ON 3 SVS TEST. EPSU EXT LOAD EMER R. FOUND ONE EMERGENCY LIGHT INOPERATIVE AT THE FWD RT OVERWING DOOR. RELAMPED, OP CHECKED OKAY.Jan 4, 2012 · N442UA · Airbus A320232 · Emergency LightingSDR UALA2012010600148Oxygen Mask · failed1ST OBSERVER O2 MASK FREEFLOWS. REPLACED MASK, OPS OKAY.Jan 4, 2012 · N405UA · Airbus A320232 · Crew Oxygen SystemSDR UALA2012010400083Actuator · failedCAPTAIN'S RUDDER PEDAL ADJUST WILL NOT SPRINGBACK FOR POSITIONING. REPLACED RUDER PEDAL ACTUATOR PER AMM, ALL OKAY.Jan 3, 2012 · N470UA · Airbus A320232 · Rudder Control SystemSDR UALA2012010400084Actuator · failedFIRST OFFICER'S RUDDER PEDALS WILL NOT SPRING BACK FOR ADJUSTING UNLESS PEDALS ARE ALREADY HALF FORWARD. REPLACED RUDDER PEDAL ACTUATOR PER AMM, ALL OK.Jan 3, 2012 · N470UA · Airbus A320232 · Rudder Control SystemSDR UALA2012010500109Computer · faultedFMGC 2 FAULT. REPLACED NR 2 FMCG PER MM. AUTOLAND CAT III TEST.Jan 3, 2012 · N441UA · Airbus A320232 · Autopilot SystemSDR UALA2012010600133Pump · underservicedRAT HYD PUMP IS UNDERSERVICED. REPLACED RAT PUMP.Jan 3, 2012 · N457UA · Airbus A320232 · Hydraulic Filter, AuxiliarySDR UALA2012010300013Circuit Breaker · trippedCABIN EMERGENCY LIGHTING CIRCUIT BREAKER H5 TRIPPED. RESET EMERGENCY LIGHT CIRCUIT BREAKER H5. ACCOMPLISHED EMERGENCY LIGHT TEST. ALL LIGHTS CHECKED OKAY.Jan 1, 2012 · N488UA · Airbus A320232 · Light System Wiring
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