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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA991230031Limit Switch · failed(CAN) ECAM WARNING RUDDER TRAVEL LIMIT NR 1 & 2 ILLUMINATED ON CLIMB. AIRCRAFT LANDED, RUDDER TRAVEL LIMITER REPLACED.SDR 99ZZZX4706Bearing · spalledENGINE REMOVED DUE TO M50 MATERIAL ON THE MAG CHIP DETECTORS. DISASSEMBLY OF THE ENGINE REVEALED THE NR 4 BEARING EXHIBITED SPALLING DAMAGE ON THE OUTER RACE. THE BEARING WAS SUBMITTED TO THE LAB FOR ANALYSIS. THE INVESTIGATION IS STILL IN PROGRESS AT THIS ASDR CA991230030Bolt · cracked(CAN) AFTER ENGINE REMOVAL BOLT SENT FOR NDI AS PER AIRBUS NTM PART 8-51-80-00 AND FOUND CRACK.THIS FAIL SAFE BOLT CAME FROM A QUICK CHANGE KIT RECEIVED FR OM BF GOODRICH WITH LOANER ENG. UPON ENG REMOVAL 333 CYCLES LATER,THE BOLT ARE REQUIRED TO PASS NDI INSPSDR 99UAL900615Blower · failedA LOUD NOISE WAS HEARD UNDER FLIGHT DECK AND F/A SMELLED ELECTRICAL ODOR. PROBLEM WAS POSIBLE AVIONICS COOLING SYSTEM. AFTER OVERRIDING SYSTEM, SMELL DISSIPATED AND NOISE STOPPED. ALL SYSTEMS REPORTING NORMAL. FLIGHT CONTINUED TO DESTINATION. *S/D* THE ASDR 99UAL900616Power Supply · failedEMERGENCY LIGHT TEST FAILS EPSU COM L. *S/D* EMERGENCY POWER SUPPLY UNIT (11WL) WAS FOUND FAULTED DURING TEST WITH MESSAGE EPSU COM L SHOWN. THE UNIT WAS REPLACED AND CHECKED NORMAL.SDR 99UAL900611Rod · out of adjDURING APPROACH THE T/E FLAPS DID NOT FULLY DEPLOY. L/E SLATS OPERATED NORMALLY. *S/D* AN INSPECTION FOUND THE ACTUATING (ADJUSTMENT) ROD INSIDE THE INTERCONNECTING STRUT BETWEEN THE LT I/B AND O/B FLPS HAD ORIGINALLY BEEN ADJUSTED ALMOST OUT OF LIMIT, CAUSDR 99UAL900590Bolt · looseCREW REPORTED, UNABLE TO RETRACT GEAR AFTER TAKEOFF. RECEIVED LANDING GEAR NOT UPLOCKED AND SHOCK ABSORBER ECAM FAULTS. *S/D* TIGHTENED NLG BARREL FITTING BOLT FOR PROX SENSORS REF IPC 32-21-11-13 ITEM 60. SECURED WITH LOCK WASHER, OPERATED LANDING GEAR, ASDR 20000424AP014Pitot Line · obstructedSAL - AFTER TAKEOFF, PILOTS NOTED A 50 KNOT DISCREPANCY BETWEEN THE CAPTAIN AND FIRST OFFICER AIRSPEED INDICATIONS, THEN AT FLIGHT LEVEL 3,000 FEET THE CAPTAIN SIDE SHOWED 240 KTS AND F/O''S 165 KTS, DUE THIS SITUATION THE FLIGHT RETURNED TO SAL AIRPORT. AFTESDR 99UAL900568O-Ring · failedFLIGHT CREW ADVISED OVERHEAD MEMPHIS LOST YELLOW SYSTEM HYDRAULIC. ELECTED TO DIVERT TO DFW FOR REPAIRS. LANDED 6.8 OVERWEIGHT AT 149,000 LBS. *S/D* FOUND O-RING AT BOTTOM OF YELLOW PUMP PRESSURE LINE TORN. REPLACED O-RING AND SERVICED YELLOW SYSTEM TO 2SSDR 99UAL900569Engine · stalledFLT CREW REPORTS SUSPECTED ENGINE STALL WHEN PULLING THROTTLE BACK TO NEAR IDLE IN ORDER TO SLOW ACFT. ALTITUDE WAS FL 350. IGNITION MSG DISPLAYED FOR APPROX 7 SECS. UNABLE TO DETERMINE WHICH ENG STALLED. *S/D* CHRONIC TOP-OF-DESCENT STALLS HAVE BEEN UNDSDR 99UAL900563Connector · disconnectedCABIN EMERGENCY LIGHTING SYSTEM TEST GIVES STATUS OF 'EXT LOADS EMER R' ON PTP DISPLAY. *S/D* 'EXT LOADS EMER R' WAS SHOWN DURING TEST ON PTP. CANNON PLUG WAS FOUND DISCONNECTED FROM RT WING AFT LIGHT ASSEMBLY (62WL). CANNON PLUG WAS RECONNECTED AND CHECKESDR 99UAL900555Windshield · crackedFLT EXPERIENCED A CRACKED OUTER WINDSHIELD ON THE CAPT SIDE AT FL390. FLT DESCENDED TO FL220 PER THE FLIGHT MANUAL. *S/D* WATER INGRESS THROUGH THE WEATHER SEAL REACHED THE WINDSHIELD''S BUSBAR, RESULTING IN ELECTRICAL ARCING AND SUBSEQUENT CRACKING OF THE SDR 99UAL900551Valve · intermittentON ARRIVAL TO MEX, CAPTAIN SET PARKING BRAKE AND IT FAILED. AIRCRAFT ROLLED ABOUT 20 FEET BEFORE CAPTAIN WAS ABLE TO APPLY BRAKES. AIRCRAFT CONTACTED JETWAY AT THE LEFT ENGINE COWL. *S/D* PERFORMED AN OPERATIONAL TEST OF THE PARKING BRAKE SYSTEM PER AMM TASDR 99UAL900525Bulb · failedUNIT EMER L AND COMM EMER L ATA 33-51-38 DISPLAYED AFTER TEST. *S/D* UNIT EMER L AND COM EMER L WERE SHOWN IN TEST DURING NR 3 SERVICE. LT OVERWING EPSU INDICATED 3 RED LIGHTS. NEW EPSU AND BATTERY DID NOT HELP. OVERWING EXTERIOR LIGHTS WERE RELAMPED AND SDR 99UAL900491O Ring · failedECAM GREEN HYDRAULIC LOW QUANTITY FL 370 CRUISE. *S/D* FOUND STRONG LEAK ON GREEN HP MANIFOLD PRESSURE LINE. REPLACED O-RING, CKD FOR LEAKS THROUGHOUT AREA AND NO LEAKS FOUND.SDR 99UAL900488Battery Pack · dischargedESCAPE PATH LIGHTS INOP AT ROW 16, 17, 18 AND ROW 22, 23, 24. REPLACED EPSU EMERGENCY POWER SUPPLY UNIT BATTERY PACK AND POWER SUPPLY. P/N 563-1188 AND 565-2005. SYSTEM CHECKS NORMAL.SDR 99UAL900468Transducer · failedIN CRUISE WITH AUTOPILOT 2 ENGAGED, AIRCRAFT EXPERIENCED AN UNCOMMANDED PITCH UP AND A SUBSEQUENT ELEVATOR AND AILERON COMPUTER 2 PITCH FAULT DISPLAY ON UPPER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING UNIT. AUTOPILOT 1 OPERATES NORMALLY. FLIGHT DIVERTED TO SDR 99UAL900464Fwc · malfunctionedF/O PITOT, TAT PROBES AND AUTO THROTTLE APPEAR ON STATUS PAGE ACCOMPANIED BY STALL WARNING AND AUDIBLE OVERSPEED WARNING SPURIOUSLY AT FL 370, MACH .79 TO .80. FOR LAST 40 TO 50 MINS OF FLIGHT STALL WARNING AND OVERSPEED CONTINUOUSLY. *S/D* FAULT COULD NOT BSDR 99UAL900463Engine · failedJUST PRIOR TO GEAR EXT, STRONG ODOR (LIKE HOT A-C DUCT) PERMEATED CABIN CAUSING BURNING EYES AND NOSE. AFTER EXTENSIVE TROUBLESHOOTING AND REPLACEMENT OF TWO ENGINES, AN OIL RESIDUE AND FINE WHITE METALLIC POWDER RESIDUE WAS FOUND IN THE NR 2 IAE V2500, ENGINSDR 99UAL900427Battery · dischargedEMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. *S/D* AFT CHARGER AND BATTERY WERE REPLACED. (P/N 11-0049) CHARGER, BATTERY (P/N 3214-30). AIRCRAFT HAS BEEN GOOD SINCE REPLACEMENTS.SDR 99UAL900421Actuator · failedDIVERTED TO ATL DUE TO LOSS OF HYDRAULIC PRESSURE. *S/D* LT YAW DAMPER ACTUATOR DEVELOPED A PIN HOLE LEAK WHICH CAUSED THE HYD SYSTEM (GREEN) TO BLEED DOWN. ACTUATOR (P/N SC4700-3), (S/N 5030), MR27258-1035. ACTUATOR WAS REPLACED AND AIRCRAFT RETURNED TO SSDR 99UAL900420Window · not latchedABORTED TAKEOFF AFTER PILOTS WINDOW OPENED AT 80-90 KTS. PILOTS REPORTED WINDOW WAS NOT FULLY LOCKED. *S/D* CAPTAIN'S SLIDING WINDOW WAS NOT FULLY LOCKED. RED-COLORED RELEASE BUTTON ON WINDOW HANDLE POPS UP WHEN THE WINDOW IS LOCKED. THIS SERVES AS A VISUSDR 99UAL900401Bearing · failedNR 1 ENG IN-FLIGHT SHUTDOWN. CREW REPORTS COMPRESSOR STALL, FOLLOWED BY VIBRATION. RETARDED THROTTLE AND EXPERIENCED ANOTHER COMPRESSOR STALL. *S/D* NR 3 BEARING FAILED, CAUSING SECONDARY DAMAGE TO THE INLET GEARBOX AND HIGH PRESSURE COMPRESSOR MODULE. INSDR 20000424AP015Sensor · damagedMIA - FLT 391 - DURING TAKEOFF, THE LGCIU NR 1 FAULT AND AFT CARGO DOOR MSG CAME ON THE UPPER ECAM DISPLAY, DUE TO THIS SITUATION THE AIRCRAFT RETURNED TO MIAMI AIRPORT. AFTER UNEVENTFUL LANDING AT MIAMI AIRPORT, THE CREW REPORTED OVERWEIGHT LANDING. MAINTENSDR 99UAL900367Light · failed testAFT CABIN EMERGENCY LIGHTS FAIL TEST. MESSAGE IS INTERNAL LOADS EMER LT. TEST OF AFT CABIN EMERGENCY LIGHTS FAILED BUT TEST PASTED AT THE NEXT STATION.SDR 99UAL900352O Ring · failedAT APPROX 1 HOUR OUT OF LAX, CREW REPORTED LOSING ALL HYDRAULIC FLUID ON YELLOW SYSTEM. SAMC WAS CONTACTED AND SYSTEM WAS SHUT DOWN PER ECAM MESSAGE. CAPTAIN ELECTED TO CONTINUE TO DESTINATION. *S/D* O-RING BETWEEN YELLLOW ACCUM & PRESS. LINE REPLACED - RSDR 99UAL900338Battery · dischargedSYSTEM FAILED EMERGENCY LIGHTING TEST. MESSAGE WAS: BATT L. PSU BATTERY WAS REPLACED (PSU P/N IS 565-0038).SDR 99UAL900328Bulb · failedOVERWING ESCAPE ROUTE LIGHTING INOP. RELAMPED AND OP'S CHECK OK.SDR 99UAL900327Tube · chafedFUEL FLOW ON LEFT ENGINE 80 LB/HR MORE THAN RIGHT. FUEL WENT OUT OF BALANCE ON 3 SEPARATE OCCASIONS, WITH THE WORST BEING 900 LBS, IE LEFT SIDE LOW. FUEL BURN WAS 1500 LBS, MORE THAN PLANNED. *S/D* FUEL LEAK FROM LINE TO ACOC AIR MODULATING VALVE. CLAMPS SDR 99UAL900309Windshield · crackedCREW REPORTS, F/O WINDSHIELD CRACKED. *S/D* CRACK WAS DUE TO BUSBAR ACRHING FROM MOISTURE INGRESS AND CONTACT WITH THE WINDOW HEAT ELEMENT. F/O WINDSHIELD WAS REPLACED PER AMM 56-11-11 ON 6-7-99.SDR 99UAL900298Oil Tubes · leakingON ACFT WALK AROUND, FOUND ACTIVE FIRE IN NR 1 ENGINE LOCATED NEAR LAST TURBINE DISK. FIRE SEEMS TO BE FED BY A SMALL OIL LEAK OF ABOUT 20 TO 25 DROPS. AT LOW POWER SETTINGS OIL SCAVENGE PUMP SOMETIMES DOES NOT SCAVENGE ADEQUATELY FROM THE NUMBER 5 BEARING CSDR 99UAL900257Rmp · smokingFIRST OFFICER'S RADIO MANAGEMENT PANEL SMOKING. RADIO MANAGEMENT PANEL (RMP) WAS REMOVED FOR THIS PROBLEM. LATER THE PANEL WAS FOUND TO BE OK AND REINSTALLED IN THE AIRCRAFT. MR23131-0135.SDR 99UAL900259Mcdu · failedCAPT MCDU FAILED, THEN F/O MCDU FAILED-WENT BLANK. *S/D* THIS WAS CODED IN CHAPTER 45 NOT 34. BOTH THE CAPT'S AND FO'S MCDU CBS WERE RESET AND SYSTEM OP'S CHECK NORMAL. NO FURTHER MAINTENANCE HAS BEEN PERFORMED AND NO FURTHER PROBLEMS WITH THE MCDU HAVE HASDR 99UAL900254Brake · failedBRAKE EXTREMELY SENSITIVE, MOST NOTICABLE ON THE LEFT BRAKE. ON LANDING AIRCRAFT JERKED ABRUPTLY TO THE LEFT. *S/D* FOUND NR 1 BRAKE SEIZED WITH YELLOW PISTONS STUCK IN ACTUATED POSTION. REPLACED NR 1 BRAKE. TAXI TESTED, ALL FUNCTIONS NORMAL.SDR 99UAL900255Ram Air Turb · failedRAT FAILED AUX HYD SYS OPS TEST. *S/D* DURING FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT, RAM AIR TURBINE FAILED CHECK. REPLACED RAT PER AMM AND OPS CHECKED NORMAL.SDR 99UAL900245Battery · dischargedCABIN EMERGENCY SYSTEM TEST FAIL. *S/D* BAD BATTERY WAS FOUND ON LEFT OVERWING POWER SUPPLY UNIT. BATTERY WAS REPLACED.SDR 99UAL900235Lanyard · detachedAFT RIGHT DOOR LIFE RAFT LANYARD NEEDS TO BE RESTOWED. IT IS INHIBITING ARMING THE DOOR. LANYARD WAS PULLED FROM ITS ATTACHMENT POINT ON THE GIRT BAR TRIGGER BY A F/A. MAINTENANCE SUBSEQUENTLY REATTACHED THE LANYARD TO ITS PROPER LOCATION ON THE GIRT BAR TRSDR 99UAL900228Light · inoperativeEMERGENCY EXIT LIGHTS, FLOOR LIGHT DAMAGED. ALL EXIT LIGHTS REMAIN ON AT ALL TIMES EVEN WITH FLT DECK SWITCH OFF. *S/D* THE EXIT SIGNS AND ALL RELATED LIGHTS ARE SWITCHED ON WHEN THE NO SMOKING SWITCH IS IN THE AUTO POSITION AND THE LANDING GEAR IS EXTENDEDSDR 20000424AP012Pump · inoperativeCUN - FLT TA581 - DURING CRUISE OF THE FLIGHT, THE LEFT AND RIGHT NR 1 WING FUEL BOOST PUMPS FAULT LIGHTS CAME ON. THE FLIGHT WAS DIVERTED TO CANCUN FOR MAINTENANCE. AT CANCUN, MAINTENANCE TECHS REMOVED AND REPLACED THE LEFT AND RIGHT NR 1 WING FUEL BOOSTS PSDR 20000424AP013Pump · inoperativeCUN - FLT TA581 - DURING CRUISE OF THE FLIGHT, THE LEFT AND RIGHT NR 1 WING FUEL BOOST PUMPS FAULT LIGHTS CAME ON. THE FLIGHT WAS DIVERTED TO CANCUN FOR MAINTENANCE. AT CANCUN, MAINTENANCE TECHNICIANS REMOVED AND REPLACED THE LEFT AND RIGHT NR 1 WING FUEL BOSDR 99UAL900236Actuator · failedHYDRAULIC FLUID LEAKING LT EMPENNAGE SECTION, APPEARS TO BE COMING FROM RUDDER. *S/D* YAW DAMPER SERVO ACTUATOR LEAKING. ACTUATOR WAS REPLACED BY IMC ON 4/26/99 AND CORRECTED THE PROBLEM.SDR 99UAL900402Handle · out of adjustRAMP REPORTED AFT CARGO PIT DOOR HANDLE DIFFICULT TO STOW. FOUND HOUSING ASSY (ITEM 180 IPC 52 31 21 PG3B 0) CRACKED.SDR 99UAL900173Cowl · damageNUMBER 1 ENGINE FAN COWLS OPENED IN FLIGHT. RETURNED TO FIELD FOR A NORMAL LANDING. FAN COWL LATCHES WERE NOT SECURED FROM MAINTENANCE ACTION PREVIOUS NIGHT. LINE MAINTENANCE MANAGEMENT INSTITUTED A REQUIREMENT FOR A SECOND PAIR OF EYES TO VERIFY FAN COWL LSDR CA990330038Vsv Actuator · malfunctioned(CAN) THE AIRCRAFT WAS ON TAKEOFF ROLL WHEN AN ECAM MESSAGE NR 2 COMPRESSOR VANE ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE VARIABLE VANE ACTUATOR AND THE MASTER BLEED ACTUATOR WERE REPLACED, POWER ASSURANCE RUNS WERE CARSDR 99UAL900170Light · inopSEAT 22C EEL LIGHT INOP. REPLACED EEL LIGHT ASSEMBLY (P/N BR9644-21), OP-CHECKS OK.SDR 99UAL900147Pump · leakingINTERMITTENT GREEN HYD SYSTEM LOW ECAM WARNING. PRESSURE NORMAL AND NO FLUCTUATION. FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REPLACED PUMP PER MM29-11-51. LEAK AND OPS CHECKS GOOD.SDR 99UAL900142Battery Pack · dischargedEMERGENCY LIGHT TEST FAILED. SHOWS EPSU 28VDC EMER L. SUPPLEMENTAL DATA UPDATE 28 VDC FAULT WAS DETECTED AT THE EMERGENCY POWER SUPPLY UNIT (11WL) AND GAVE A FAULT MESSAGE 'EPSU 28 VDC EMER L'. THE BATTERY WAS REPLACED AND THE TEST WAS FOUND NORMAL.SDR 99UAL900132Regulator · leakingFLIGHT DIVERTED TO DEN WHEN SUPPLEMENTAL OXYGEN WAS LOST. WHILE SEARCHING FOR O2 LEAK FOUND CREW O2 REGULATOR TRANSMITTER ASSY LEAKING MASSIVLY. LEAK IS AT THE BACK OF THE TRANSMITTER HOUSING. REPLACED REGULATOR ASSY. LEAK CHECKED REGULATOR. NO LEAKS NOTESDR 99UAL900120Fan · overheatedFLIGHT CREW ADVISED DISPATCH OF FUMES IN THE COCKPIT (POSSIBLY DUE TO AN EXTRACT FAN OVERHEAT). CREW ON OXYGEN. DECLARED EMERGENCY FOR EXPEDITED LANDING AT ORD ON 14L. EXTRACT FAN OVERHEATED. NO REPORTED APU PROBLEMS. EXTRACT FAN REPLACED PER MM 21-26-51.SDR 99UAL900128B Nut · cross threadFLIGHT DIVERTED TO CUU DUE TO LOSS OF OIL PRESSURE AND OIL QUANTITY IN NR 2 ENGINE. ENGINE NR 2 OIL QUANTITY SHOWS 4.5 QT, FLASHING, ALL OTHER INDICATIONS NORMAL. OIL PRESSURE LINE FITTING WAS FOUND LOOSE AT T-FITTING ABOVE PRESSURE SWITCH, CAUSING OIL LEAKA
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