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 UALA2010101303812Cone · crackedNR 1 ENGINE EXHAUST CONE HAS A CRACK A T 9 O'CLOCK. CRACK LOCATED IN ZONE 1 AND IS 7.5 INCHES IN LENGTH. ACP EVA 80212 STOP DRILLED HOLE. CRACK CAN BE WELD REPAIRED IAW SM USING AMS5837 FILLER.Oct 11, 2010 · N460UA · Airbus A320232 · Engine Collector/Tailpipe/NozzleSDR UALA2010101103779Window · damagedLT FWD EMER EXIT WINDOW SHOWS SIGNS OF HEAT DISTORTION FROM LIGHTNING STRIKE. REPLACED LT FWD EMER EXIT HATCH WINDOW.Oct 10, 2010 · N473UA · Airbus A320232 · Door WindowsSDR UALA2010100803737Door · obstructedL2 DOOR DISARMED MESSAGE, RTFL. DISARMED DOOR, FOUND F/A SEAT BELT STRAP UNDER DOOR, ACROSS GIRT BAR AREA. DOOR ARM AND DISARM NORMAL.Oct 8, 2010 · N468UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2010100803756Rod End · wornVIBRATION-NOISE ENCOUNTERED IN FLIGHT. DATA VIBRATION REPORT CHECK LIST OBTAINED FROM FLIGHT CREW, TSM DECISION TABLE COMPLETED, ELEV & RUDDER HAD THE TWO HIGHEST SCORES. TROUBLESHOT VIBRATION WITH INFO GIVEN. FOUND RT AND LT OTBD ELEVATOR ACTUATOR ROD ENDS WOOct 8, 2010 · N470UA · Airbus A320232 · Stabilizer Control SystemSDR UALA2010100803758Computer · faultyACFT TRIM ISSUES. REPLACED ELEVATOR & AILERON COMPUTER 1 AND OP CK GOOD. REPLACED FLIGHT AUGMENTATION COMPUTER, OPS CHECKED GOOD.Oct 7, 2010 · N436UA · Airbus A320232 · Flight Control SystemSDR UALA2010100603699Skin · corrodedREPAIR DOUBLER IS INSTALLED DUE TO CORROSION AT CUTOUT FOR AFT LAV SERVICE PANEL ON LOWER AFT FUSELAGE. REPLACED INNER DOUBLER REF SRM ON NR C4392K.Oct 5, 2010 · N408UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2010100603700Stringer · corrodedMAJOR REPAIR. AFT PIT CORROSION BETWEEN FR65 AND 66 STR 33R UNDER OUTFLOW VALVE MOTOR. REPLACED STRINGER SECTION REF SRM 51-42-11 ON NR C4784K.Oct 5, 2010 · N408UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2010100503686Skin · corrodedCORROSION ON SKIN UNDER DOME NUTS BETWEEN FR 58 & 59 AT ANTENNA MOUNT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR PER RE0-L01272 & EVA-80171 AND SRM.Oct 4, 2010 · N408UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2010100503687Skin · corrodedCORROSION ON SKIN UNDER DOME NUTS BETWEEN FR 57 & 58 AT ANTENNA MOUNT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR IAW REO-01272, EVA-80171 AND SRM.Oct 4, 2010 · N408UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2010100503688Skin · corrodedCORROSION ON SKIN UNDER DOME NUTS BETWEEN FR 55 & 56 AT ANTENNA MOUNT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR IAW REO-L01272, EVA-80171 AND SRM.Oct 4, 2010 · N408UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR UALA2010100403685Power Supply · failedGROUND SCAN ON CIDS BITE CHECK AND CABIN EMERGENCY LIGHTING CHECK FAILED. REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY AT LT OVERWING EXIT (11WL). GROUND SCAN ON CIDS AND CABIN EMERGENCY LIGHTING CHECK BOTH PASS WITH NO FAILURES.Oct 4, 2010 · N473UA · Airbus A320232 · Emergency LightingSDR UALA2010100403675Release Cable · out of adjustR1 DOOR GIRT BAR DOES NOT FULLY LOCK INTO FITTING. ADJUSTED ESCAPE SLIDE RELEASE CABLE IAW MM ON NR C7145K BY NR308039 AND INSPECTED BY LC81.Oct 3, 2010 · N408UA · Airbus A320232 · Emergency EquipmentSDR UALA2010100403677Battery · failedLEFT MID EMERGENCY LIGHT BATTERY FAILS SELF TEST. REPLACED BATTERY, ALL SYS CHECKED OK.Oct 3, 2010 · N428UA · Airbus A320232 · Emergency LightingSDR UALA2010100103641Stringer · corrodedAFT PIT HAS CORROSION ON STR 40R BETWEEN FR 58 & 59. MAJOR REPAIR. REMOVED CORRODED SECTION OF STRINGER AND REPLACED WITH SPLICED SECTION.Oct 1, 2010 · N408UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2010100403664Bolt · shearedAT FLOORBEAMS EXPANSION JOINTS AFT OF F46, MOST LT BOLT FOUND SHEARED. REPLACED ALL 6 BOLTS, NDT JOINTS-NO CRACKS.Oct 1, 2010 · N457UA · Airbus A320232 · Fuselage Main, Floor BeamSDR UALA2010100103631Slide · reads lowDOOR 1R SLIDE PRESSURE LOW. REPLACED NR 1R DOOR SLIDE ASSY.Sep 30, 2010 · N446UA · Airbus A320232 · Escape SlideSDR GTIA1000047Windshear Sys · faultedLOW SPEED, ABORT TAKEOFF DUE TO WINDSHEAR DET FAULT.Sep 29, 2010 · N601NK · Airbus A320232 · Wind Shear Detection SystemSDR UALA2010093003613Stringer · corrodedAFT PIT STRINGER 43L BETWEEN FR 54 AND 59 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REPLACED STRINGER SECTION.Sep 29, 2010 · N408UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2010092903592Oxygen Mask · unwanted deployO2 MASK SEAT 14A DEPLOYED. 02 DOOR WILL NOT SECURE CLOSED. TAPED DOOR CLOSED. SEATS 14ABC NOT TO BE OCCUPIED. REPLACED CONTAINER.Sep 28, 2010 · N461UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2010092903594Controller · malfunctionedFLAPS SLOW, SLAT SYS 2 FAULT ON RECALL. RESET NO HELP. REPLACED NR2 SFCC. RAN FLAPS & SLATS THRU NUMEROUS CYCLES. SYS OPS APPEARS NORMAL. HAD VALVE BLOCK SYS STATUS MESSAGE PRIOR TO REPLACEMENT OF SFCC NR 2. MESSAGE CLEARED AFTER SFCC REPLACED.Sep 28, 2010 · N415UA · Airbus A320232 · Leading Edge Slat Control SystemSDR UALA2010092903595Fitting · out of adjustR2 DOOR GIRT BAR DOES NOT LOCK IN FITTINGS IN ARMED POSITION. ADJUSTED AFT GIRT BAR FITTING ON NR D4528Y.Sep 28, 2010 · N426UA · Airbus A320232 · Emergency EquipmentSDR UALA2010092803586Life Vest · missingLIFE VESTS MISSING UNDER SEATS. REPLACED ALL MISSING LIFE VESTS.Sep 28, 2010 · N496UA · Airbus A320232 · Life JacketSDR UALA2010092703557Slide · faultyPOWER SUPPLY FOR EMERGENCY LIGHTS AT AFT LT DOOR FAULTS EXTERIOR LIGHTS. FAULTS FROM CIDS AND FROM POWER PACK. REPLACED DOOR 2L SLIDE.Sep 27, 2010 · N433UA · Airbus A320232 · Escape SlideSDR UALA2010092903611Bracket · damagedO2 MASK FAILED TO DEPLOY AT AFT JUMPSEAT WHEN ACCOMPLISHING 6185 O2 SAFETY PIN CHECK. NEEDS NEW O2 BOX CONTAINER DUE TO SOLENOID BRACKET WAS CRACKED. REPLACED OXYGEN CONTAINER AND GENERATOR IAW MM.Sep 27, 2010 · N443UA · Airbus A320232 · Passenger Oxygen SystemSDR UALA2010092803578Door · unsecureLAVATORY WASTE DOOR BENT OR WON'T OPEN-CLOSE FWD CAB LT LAV. FORWARD LAV DOOR WHICH HOLDS THE FIRE EXTINGUISHER FELL OFF. DOOR FALLS OFF BECAUSE THE HOLDER AT THE BOTTOM IS DAMAGED AND DOOR WILL NOT STAY IN PLACE SECURELY. NO TIME ORD. SECURED WITH SAFETY WIRESep 27, 2010 · N463UA · Airbus A320232 · Fluid Service DoorsSDR UALA2010092803580Line · faultyEGT OVERLIMIT DISPLAYED ON UPPER ECAM SCREEN. REPLACED NR1 ENG. COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENGINE PARAMETERS ABNORMAL. REPLACED NR 1 ENG. NR 1 ENG BLEED PRESSURE FLUCTUATES FROM 8-26 PSI AT IDLE POWER NO ECAM WARNING. REPLACED PRV PER AMSep 27, 2010 · N447UA · Airbus A320232 · Turbine Engine Oil SystemSDR USAA2010092792105Light · malfunctionedEMERGENCY LIGHT - DOORS 1L AND 1R EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. MX CYCLED EMERGENCY LIGHT SWITCH ON/ OFF. OPS NORMAL.Sep 26, 2010 · N661AW · Airbus A320232 · Emergency LightingSDR UALA2010092703551Controller · faultyCABIN PRESS SYS FAULT, FLIGHT DIVERTED. ACFT ALSO EXPERIENCED CPC1 FAULT. CREW STATED THAT MANUAL MODE WOULD NOT HOLD PRESSURIZATION, SO THEY DECENDED TO 10,000 FT. TROUBLESHOOT REF MT21-013, PARA 2 "ACFT UNABLE TO MAINTAIN CABIN PRESSURE". REPLACED OUTFLOW VASep 26, 2010 · N407UA · Airbus A320232 · Cabin Pressure ControllerSDR UALA2010092803576Wire · disconnectedPAX O2 GEN BOX, 10 DEF, DOES NOT OPEN WHEN TESTED. CONNECTED O2 CONTAINER WIRES. OPERATIONAL TEST OKAY.Sep 26, 2010 · N418UA · Airbus A320232 · Oxygen System WiringSDR USAA2010092792102Lens · missingEMERGENCY LIGHT - EMERGENCY EXIT LIGHT ON SIDEWALL NEAR FLOOR ADJACENT TO DOOR 2R IS MISSING LENS COVER. MX REPLACED EXIT LIGHT LENS AT 2R DOOR.Sep 25, 2010 · N652AW · Airbus A320232 · Emergency LightingSDR UALA2010092803577Actuator · failedWHILE ACCOMPLISHING LM6185, O2 SAFETY PIN CK, O2 COMPARTMENT DOOR AT SEATS 8DEF FAILED TO OPEN, MASKS NOT DEPLOYED. REPLACED DOOR ACTUATOR, OPS CKS GOOD.Sep 25, 2010 · N449UA · Airbus A320232 · Passenger Oxygen SystemSDR USAA2010092792104Tire · blownEMERGENCY LANDING - ACFT LOST TREAD FROM 1 OF THE LT MAIN TIRES ON TAKEOFF. FLIGHT CONTINUED AND WHILE ENROUTE, CREW REPORTED LOSS OF YELLOW HYD SYS. AN EMERGENCY WAS DECLARED, ACFT LANDED WITHOUT INCIDENT AND TAXIIED TO GATE. MAINTENANCE DETERMINED TREAD LSep 24, 2010 · N662AW · Airbus A320232 · TireSDR UALA2010092403546Power Supply · faultyEPSU TEST GIVES "EPSU INTERNAL LOAD L" MESSAGE. REPLACED EPSU AND BATTERY PER MT. TESTS OKAY.Sep 24, 2010 · N472UA · Airbus A320232 · Emergency LightingSDR UALA2010092403547Sleeve · delaminatedDURING WALK AROUND FOUND NR1 ENG LT REVERSER C-DUCT AREA, AT ABOUT 7 O'CLOCK POSITION, SHOWING DELAMINATION. DAMAGE IS 9 INCHES BY 4.5 INCHES. LOCATED AFT OF ENGINE. REF MT 78-010. SPEED TAPED AREA IAW MT 78-010. SPOKE WITH OPBLM AND THEY CONCURRED. WILL NEESep 24, 2010 · N444UA · Airbus A320232 · Engine Thrust ReverserSDR UALA2010092403543Power Supply · inoperativeEPSU FAULT LEFT DISPLAYED WHILE DOING INTERIOR EMERGENCY LIGHT TEST. UNIT FAULTING WHILE DOING EPSU SELF TEST. REPLACED POWER SUPPLY UNIT AND BATTERY. OPS CHK GOOD.Sep 23, 2010 · N434UA · Airbus A320232 · Emergency LightingSDR UALA2010092203520Placard · out of positionDOOR 2R HAS LEFT SIDE PACK COVER ON RIGHT SIDE THUS COVERING VISUAL INDICATOR. SUPPLEMENTAL DATA UPDATE REMOVED WRONG PLACARD, INSTALLED INTERIM PLACARD PER GN. DOOR 2R HAS LEFT SIDE PACK COVER ON RIGHT SIDE THUS COVERING VISUAL INDICATOR. PLACARD FOR SLIDE COSep 22, 2010 · N420UA · Airbus A320232 · Placards and MarkingsSDR UALA2010092303536Attach Fitting · crackedNR 2 PYLON OTBD RIB 5 ATTACHING PLATE CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED ATTACH ANGLE ON NR D4149Y AND INSPECTED BY LC38.Sep 22, 2010 · N424UA · Airbus A320232 · Nacelle/Pylon, Attach FittingsSDR UALA2010092003483Stringer · corrodedAFT FUSELAGE STRINGER JUST BELOW CABIN OUTFLOW VALVE IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED CORRODED STRINGER. INSTALLED NEW REPLACEMENT STRINGER & REPAIR SPLICE ANGLES. WORK ACP BY STAM.Sep 19, 2010 · N409UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2010092003493Panel · misinstalledAFT LAV PANEL IS INADEQUATE. FBO MECHANIC STATED THAT PANEL APPEARS TO BE INSTALLED UPSIDE DOWN, WHICH WOULD CAUSE BUTTON TO BE IN WRONG POSITION. PANEL WAS REPLACED WITH THE CORRECT PANEL. NOW THE FLUSH TOUCH BUTTON IS VISIBLE AT THE UPPER LT CORNER.Sep 17, 2010 · N419UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR UALA2010091603439Bolt · sheared1 BOLT FOUND SHEARED AT FLOORBEAMS EXPANSION JOINT AFT OF F46. REPLACED ALL 6 BOLTS AND NDT STRUCTURE, NO CRACKS. FOUND. C-W ON SMB W-U G8897H.Sep 14, 2010 · N425UA · Airbus A320232 · Fuselage Main, Floor BeamSDR UALA2010091303394Rod End · wornVIBRATION-NOISE ENCOUNTERED IN FLIGHT. LIGHT AIRFRAME VIBRATION ON TAKEOFF. BELIEVE IT IS ASSOCIATED WITH FLAPS OR SLATS. REPORTING CHECKLIST REF TSM 05-50 -00-810-801 COMPLETED AND INDICATES NLG DOOR GAPS TO BE CHECKED. ALL ELEV AND RUDDER ROD ENDS ARE OUT Sep 13, 2010 · N492UA · Airbus A320232 · Rudder StructureSDR UALA2010091403418Stringer · corrodedAFT CARGO COMPARTMENT BILGE AT STRINGER 42L BETWEEN FRAMES 56 & 57 CORRODED. MAJOR REPAIR ACCOMPLISHED: CUT OUT CORRODED SECTION OF STRINGER. FABRICATED & INSTALLED STRINGER SPLICE REPAIR COMPRISED OF NEW STRINGER SECTION & 2 SPLICE FITTINGS AT MID FRAME 55 &Sep 13, 2010 · N407UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2010091403419Skin · damagedLT MED HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: FLUSH DOUBLE INSTALLED JUST FWD LT MED 1 APPROX FR 11 STR 20L.Sep 13, 2010 · N434UA · Airbus A320232 · Passenger/Crew DoorsSDR UALA2010091303363Transducer · illuminatedFLT CONTROL INDICATION, FLIGHT DIVERTED. AMBER BOX AROUND LEFT GREEN & RIGHT BLUE AILERONS, POSSIBLE ELAC 2 FAULT. CFDS SHOWS "27-93-34 ELAC 2 AIL ORDER DISAGREE". NOTE: ELAC 2 REPLACED TWICE. CHECK - REPLACE SIDE STICK TRANS. UNITS 4CE1 AND 4CE2. ECAM WSep 12, 2010 · N452UA · Airbus A320232 · Flight Control SystemSDR UALA2010091303362Connector · malfunctioned2 HOURS AFTER TAKEOFF GOT A -RAT OUT- MEMO ON ECAM WITH A RAT OPERATING ICON ON HYD STATUS. NO ADDITIONAL NOISE NOTED IN CRUISE, JUST ECAM INDICATIONS. TROUBLESHOT IAW TSM, FAULT ISOLATION STEP 4B (1). RAT DID NOT DEPLOY, BUT AMBER "RAT HYD FAULT" AND "RAT OSep 11, 2010 · N423UA · Airbus A320232 · Hydraulic Power System WiringSDR UALA2010091003351Controller · malfunctionedRT PACK OVERHEAT. RTFL DUE TO OVERHEAT FAULTS ON RIGHT PACK NEED TO REPLACE 10HA2. REPLACED 10HA2 BLEED PRESSURE REGULATOR VALVE SOLENOID. REPLACED EXHAUST OUTLET DOOR ASSY AND DOOR ACTUATOR (P/N 762A0000-04), OPS CHECKED GOOD, PACK TEMP CONTROL SYSTEM TESTSep 10, 2010 · N446UA · Airbus A320232 · Cabin Cooling SystemSDR UALA2010091003354Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ELAC NR 2 ECAM HAD SHARP SMOKE ODOR THAT IS GONE. TURNED OFF ELAC NR 2. DID NOT ATTEMPT A RESET DUE CONFIRMED SMOKE ODOR IN ELAC NR 2. REPLACED ELAC NR 2. ACCOMPLISHED ELAC OPERATIONAL TEST, AFS TEST AND LAND CAT Sep 9, 2010 · N466UA · Airbus A320232 · Flight Control SystemSDR UALA2010090903338Stringer · corrodedAFT PIT BILGE STR 43L CORRODED BETWEEN FR 57 AND 58. MAJOR REPAIR ACCOMPLISHED: STRINGER 43L CORRODED BETWEEN FR57 AND FR58. REMOVED CORROSION AND INSTALLED ANGLE REPAIR.Sep 8, 2010 · N409UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR UALA2010090803329Pitot Head · obstructedCAPT AIRSPEED SPLIT. NEED TO ACCOMPLISH TEST OF PHC 1,2,3 AND ADR 1,2,3 IN CFDS. ALSO ACCOMPLISH VISUAL CHECK OF CAPTS PITOT TUBE. ALSO CHECK FOR EVIDENCE OF WATER IN SYS. ACCOMPLISHED TEST OF ADR'S AND PH C'S THROUGH THE CFDS-NO FAULTS FOUND. ACCOMPLISHESep 8, 2010 · N454UA · Airbus A320232 · Pitot/Static SystemSDR UALA2010090803319Wire · broken'ENG FIRE EXTINGUISH-SQUIB' LIGHT OF 'AGENT 1' PUSHBUTTON SWITCH IS OFF DURING 'LOOP-SQUIB TEST'. FOUND BROKEN WIRE 6 INCHES FROM NR1 FIRE BOTTLE SQUIB 5WE1 IN NR1 PYLON. REPLACED BROKEN WIRE FROM CONNECTOR VC473 TO SQUIB CONNECTOR. TESTED OK. REPAIRED CONSep 6, 2010 · N470UA · Airbus A320232 · Fire Protection System Wiring
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