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 97UAL900220Circuit Board · failedCREW ABORTED TAKEOFF AT 80 KNOTS DUE TO AVIONICS FAILURE ON THE AIRCRAFT. *S/D* OVERHEAD LIGHT FAILED TO ILLUMINATE WITH EXTRACT FAN SWITCH SET TO OVERRIDE MODE. REPLACED ANNUNCIATOR DIM TEST CARD 6LP. AIRCRAFT OPERATED NORMALLY WITH NO OTHER DEFECTS FOUNDSDR 97UAL900172Door Handle · not stowedFORWARD CARGO DOOR OPEN MESSAGE APPEARED AT ABOUT 13,000 FEET DURING CLIMB. *S/D* FOUND FORWARD CARGO DOOR HANDLE NOT STOWED COMPLETELY. ADJUSTED HANDLE FLAP, CHECKED PROXIMITY SWITCH ALIGNMENT AND LUBED DOOR LOCKING MECHANISM. DOOR OPERATED NORMALLY WITH SDR 97UAL900171Skin · lightning strikeDIVERTED TO IAD AND LANDED UNDER AMBER ALERT DUE TO LIGHTNING STRIKE AND SMOKE IN CABIN. *S/D* LIGHTNING STRIKE CAUSED DAMAGE TO 6 RIVETS ALONG THE LEFT SIDE OF THE AIRCRAFT LOWER FUSELAGE. RIVETS WERE REPLACED WITH NO OTHER DAMAGE BEING DETECTED.SDR 97UAL900152Low Level Warn · activatedLOSS OF BLUE SYSTEM HYDRAULIC FLUID EN ROUTE TO ORD. LOW LEVEL DISPLAYED ON UPPER ECAM. SUPPLEMENTAL DATA UPDATE AFTER LANDING RAN ELECTRICAL PUMP AND CYCLED FLIGHT CONTROLS. NO FAULTS WERE FOUND AND NO REOCCURRING DISCREPANCIES ENCOUNTERED.SDR 97UAL900095Mechanism · lack of lubeFLIGHT RETURNED TO PDX DUE TO AFT CARGO DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT WAS DISPATCHED WITH THE CARGO DOOR HANDLE FLUSH AND THE DOOR INDICATION LIGHTS NORMAL, HOWEVER, THE DOOR FLAPPER PANEL MOST LIKELY DID NOT SPRING BACK TO THE FLUSH SDR 97UAL900052Gen Contl Unit · shortedAT 16,000 FEET DURING CLIMB OUT OF ORD, LOST ELECTRICAL POWER. NR 1 AC BUS, NR 1 TR AND AC ESSENTIAL BUS WERE NOT POWERED. APU WOULD NOT START. SELECTED ALTERNATE POSITION OF AC ESSENTIAL FEED SWITCH. AFTER AC ESSENTIAL BUS WAS POWERED APU STARTED AND WASDR 96UAL900975Power Supply · looseEMERGENCY LIGHTS FAILED TEST ON PTP PANEL. *S/D* RESEATED POWER SUPPLY BATTERY AND OPERATIONALLY CHECKED NORMAL.SDR 96UAL900977Battery · dischargedEMERGENCY LIGHTS FAIL TEST. *S/D* REPLACED BATTERY IN POWER SUPPLY 10WL.SDR 96UAL900952Lever Arm · failedON CLIMBOUT PASSING APPROXIMATELY 6,000 FEET A LOUD BANG WAS HEARD AND THE NR 2 ENGINE ROLLED BACK. ALL INDICATIONS LOOKED GOOD FOR A RELIGHT. WHEN RELIGHT WAS ATTEMPTED VIBRATION WAS HIGH AND THE RESTART WAS ABORTED. *S/D* 3 HIGH PRESSURE COMPRESSOR VARIASDR 96UAL900948Light · malfunctionedRIGHT REAR OVER WING EMERGENCY EXIT LIGHT CAME ON IN LIGHT TURBULENCE. PROBLEM COULD NOT BE DUPLICATED AND CAUSE COULD NOT BE DETERMINED. UPON SUBSEQUENT REINSPECTIONS, NO PROBLEM COULD BE FOUND.SDR 96UAL900839Control Unit · malfunctionedRIGHT LANDING GEAR DID NOT DISPLAY GREEN ON GEAR EXTENSION. CYCLED GEAR AND RIGHT GEAR DOOR ECAM DISPLAYED MOMENTARLY FOLLOWED WITH NORMAL 3 GREENS. *S/D* REPLACED LGCIU AND OPERATIONALLY CHECKED NORMAL.SDR 96UAL900816Battery Pack · dischargedEMERGENCY LIGHTS FAIL CABIN INTERCOMMUNICATION DATA SYSTEM TEST ON NR 2 SERVICE. *S/D* REPLACED 11WL POWER SUPPLY AND BATTERY PACK. ALSO, REPLACED BATTERY PACK OVER DOOR 2L, OPERATIONALLY CHECKED NORMAL.SDR 96UAL900817Smoke Alarm · malfunctionedCREW REPORTED, ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE CARGO SMOKE DISCHARGE AGENT 2. *S/D* RECYCLED AIRCRAFT POWER AND THE MESSAGE CLEARED. NO FURTHER MESSAGES ENCOUNTERED.SDR 96UAL900773Idg Bolts · looseRETURNED TO ORD UNDER AMBER ALERT WITH NR 1 ENGINE GENERATOR FAILURE. *S/D* IDG DID NOT DISCONNECT. ROOT CAUSE WAS DUE TO IDG SCAVENGE PUMP/GOVERNOR HOUSING BOLTS COMING LOOSE. THIS ALLOWED VIBRATION WHICH BROKE THE WIRE STRANDS TO THE DISCONNECT SOLENOID.SDR 96UAL900713Battery Pack · dischargedEMERGENCY LIGHT TEST GAVE A FAILED INDICATION DURING TESTING. *S/D* REPLACED FORWARD EMERGENCY BATTERY PACK AT FORWARD OVERHEAD DOOR 1 LEFT.SDR 96UAL900714Battery Pack · dischargedSEAT EEL LIGHTS ARE INOPERATIVE AT SEAT ROWS 13 THROUGH 15 AND 19 THROUGH 21. *S/D* REPLACED RIGHT HAND AFT ESCAPE PATH BATTERY PACK.SDR 96UAL900716Assist Bottle · dischargedWHILE PERFORMING OPERATIONAL CHECK OF NR 2 AFT RIGHT DOOR AFTER SLIDE REPLACEMENT, THE DOOR ASSIST BOTTLE DISCHARGED AND DOOR WAS UNABLE TO OPEN.SDR 96UAL900656Power Supply · inoperativeCABIN EMERGENCY LIGHTING CHECK FAILS TEST. POWER SUPPLY INOPERATIVE. REPLACED POWER SUPPLY AT DOOR 1L.SDR 96UAL900657Smoke Detector · malfunctionedAFT CARGO SMOKE WARNING IN FLIGHT. WARNING CANCELED ON ITS OWN, RETURNED TO FIELD. *S/D* RESET CIRCUIT BREAKERS AND PERFORMED BITE TEST OF SYSTEM, OPERATIONALLY CHECKS NORMAL. REPLACED SMOKE DETECTION CONTROL UNIT AS A PREVENTATIVE MEASURE.SDR 96UAL900643Switch · failedGREEN HYDRAULIC SYSTEM RESERVOIR INDICATED LOW FOLLOWED BY ECAM ALERT, SYSTEM GREEN PRESSURE LOW. CREW FOLLOWED ECAM PROCEDURES FOR LANDING WITH MANUAL GEAR EXTENSION ACCOMPLISHED. *S/D* FAILED LOW LEVEL SWITCH GENERATED ECAM MESSAGE. CREW PROCEDURE IS TO SDR 96UAL900594Lamps · failedEMERGENCY LIGHT SYSTEM FAILED TEST AT FORWARD FLIGHT ATTENDANT PANEL. *S/D* FOUND LAMPS FAILED. REPLACED AND OPERATIONALLY CHECKED NORMAL.SDR 96UAL900595Light · failedEMERGENCY LIGHT SYSTEM FAILED TEST PER NR 2 SERVICE. *S/D* CHANGED P0WER SUPPLY AND BATTERY. ALSO, REPLACED SLIDE AND OPERATIONALLY CHECKED NORMAL.SDR 96UAL900565Servo Control · leakingLANDED UNDER AMBER ALERT AT IAD DUE TO LOSS OF HYDRAULIC PRESSURE. *S/D* FOUND LEFT OUTBOARD AILERON SERVO CONTROL LEAKING. REPLACED SERVO CONTROL AND OPERATIONALLY CHECKED NORMAL.SDR 96UAL900547Lamp · failedAFT DOOR EXIT SIGN REMAINED ON AFTER TEST. *S/D* REPLACED LAMPS IN EXIT SIGNS. SYSTEM OPERATIONALLY CHECKED NORMAL.SDR 96UAL900503Clamp · brokenUNPLANNED STOP AT PDX DUE TO LOSS OF CABIN PRESSURIZATION. *S/D* FOUND CLAMP ON THE OUTLET OF THE NR 1 PACK CONDENSER BROKEN CAUSING AIRCRAFT TO SLOWLY REPRESSURIZE. REPLACED CLAMP AND SYSTEM OPERATED NORMALLY.SDR 96UAL900470Fuel Pump · failedAT CRUISE FL330, RECEIVED AN ECAM MESSAGE 'COMPRESSOR VANE'. SHORTLY AFTER ENGINE 2 BEGAN FLUCTUATING AND THEN SHUT ITSELF DOWN. *S/D* FOUND ALUMINUM CHIPS IN FUEL FILTER, IMPELLER STAGE AND HOUSING OF FUEL PUMP HAD EXTENSIVE DAMAGE CAUSED BY A BOLT IN FUESDR 96UAL900471Light · failed testEMERGENCY ESCAPE LIGHTS FAIL OPERATIONAL TEST.SDR 96UAL900452Disconnect Box · mis installedFOUND LOCALIZED HEAT DAMAGE AT THE WALL DISCONNECT BOX OF THE PASSENGER ENTERTAINMENT SYSTEM. *S/D* THE DAMAGE WAS CAUSED BY IMPROPER INSTALLATION OF ONE CONNECTOR AND MOISTURE FROM CONDENSATION. THE WALL DISCONNECT BOX WAS REPLACED AND OPERATED NORMALLY.SDR 96UAL900419Lamp · failedCABIN EMERGENCY LIGHT TEST FAILED. RELAMPED EMERGENCY LIGHTS, RESEATED CONNECTOR ON EPSU 11WL, SYSTEM OPERATED NORMALLY.SDR 96UAL900409Window Track · crackedFIRST OFFICER'S SLIDING WINDOW LOWER RAIL TRACK FOUND CRACKED. SUPPLEMENTAL DATA UPDATE: REPAIRED TRACK PER STRUCTURAL REPAIR MANUAL SRM-55-11-12.SDR 96UAL900398Switch · looseLOST GREEN SYSTEM HYDRAULIC QUANTITY IN CRUISE. BLUE AND YELLOW SYSTEM WERE NORMAL. *S/D* FOUND THE ENGINE PRESSURE SWITCH CAME LOOSE IN FLIGHT. REPLACED SWITCH AND OPERATIONALLY CHECKED NORMAL.SDR 96UAL900323Electronic Box · failedHAD A RAPID DECOMPRESSION OF THE AIRCRAFT AT FL370. AUTO PRESSURE SYSTEMS 1 AND 2 FAILED SIMULTANEOUSLY. REGAINED CONTROL IN MANUAL. *S/D* ELECTRONIC BOX FAILED ON OUTFLOW VALVE. ELECTRONIC BOX WAS REPLACED AND SYSTEM OPERATED NORMALLY.SDR 96UAL900324Slide · leakingLEFT HAND OFF WING ESCAPE SLIDE REMOVED FOR FIRST OVERHAUL WAS FOUND TO HAVE NUMEROUS AREAS OF POROSITY AND A SEAM LEAK ON THE CROSS TUBE WHICH CAUSED THE UNIT TO FAIL AN AIR RETENTION TEST. PATCHED AND REPAIRED DAMAGED AREAS PER VENDORS MANUAL.SDR 96UAL900276Outflow Valve · malfunctionedLOST CABIN PRESSURE AT FL350. EXECUTED EMERGENCY DESCENT AND REGAINED CONTROL OF CABIN IN MANUAL MODE. *S/D* ELECTRONIC BOX NR 1 FAILED ON OUTFLOW VALVE DRIVING THE VALVE OPEN. REPLACED OUTFLOW VALVE AND OPERATIONALLY CHECKED NORMAL.SDR 96UAL900265Circuit Breaker · trippedEMERGENCY LIGHTS FAILED SYSTEM TEST. RESET CIRCUIT BREAKERS AND SYSTEM OPERATED NORMALLY.SDR 96UAL900266Power Supply · inoperativeEMERGENCY LIGHTS FAILED TEST. REPLACED POWER SUPPLY AND SYSTEM OPERATED NORMALLY.SDR 96UAL900247Girt Tube · wornSLIDE REMOVED FOR OVERHAUL. SLIDE HAD 3 HOLES ON THE LOWER SIDE OF THE GIRT INFLATION TUBE. REPAIRED SLIDE PER VENDORS MANUAL.SDR 96UAL900237Door Sensor · malfunctionedCREW REPORTED, AT THE OUTER MARKER THE GEAR WAS SELECTED DOWN AND THE INDICATIONS REMAINED RED. THE GEAR WAS RECYCLED AND OPERATED NORMALLY. *S/D* ACCOMPLISHED CHECK OF DOOR SENSORS AND WIRING. SWUNG GEAR SEVERAL TIMES AND COULD NOT DUPLICATE PROBLEM. SYSSDR 96UAL900226Proximity Sensor · out of adjustDURING GEAR EXTENSION ON ARRIVAL AT SFO, LANDING GEAR UNLOCK LIGHTS ILLUMINATED WITH NO GREEN DOWN AND LOCKED INDICATION. RECYCLED GEAR HANDLE AND GEAR EXTENDED NORMALLY. SUPPLEMENTAL DATA: UPDATE FOUND RIGHT HAND LANDING GEAR DOOR PROXIMITY SENSOR OUT OF ASDR 96UAL900219Battery Pack · dischargedMID CABIN EMERGENCY ESCAPE PATH LIGHTING GOES OUT AFTER ONE MINUTE OF OPERATION. REPLACED MID CABIN EMERGENCY LIGHTING BATTERY PACKS AND OPERATED NORMAL.SDR 96UAL900200Downlock Ind · malfunctionedON SHORT FINAL, GEAR SELECTED DOWN, DID NOT RECEIVE GEAR LOCKED INDICATION LIGHT. RECYCLED GEAR LEVER AND GEAR LOCKED. HEARD GURGLING SOUND FROM CENTER CONSOLE. FIRST OFFICER'S PFD AND ND WENT BLANK AND THEN CAME BACK UP WITH NO PILOT ACTION. *S/D* COULD SDR 96UAL900199Proximity Sensor · out of adjustAT FL 310, RECEIVED ECAM MESSAGE THAT FORWARD CARGO DOOR OPEN. NO PRESSURIZATION PROBLEM. SUPPLEMENTAL DATA: UPDATE PROXIMITY SENSORS WERE FOUND OUT OF ADJUSTMENT. ADJUSTED SENSORS AND OPERATIONALLY CHECKED NORMAL.SDR 96UAL900162Power Supply · inoperativeEMERGENCY LIGHT TEST FAILED. REPLACED FWD EMERGENCY POWER SUPPLY UNIT.SDR 95UAL900301Eel Power Supply · inoperativeAFT EMERGENCY LIGHTS OVER AFT DOORS ARE INOPERATIVE. REPLACED POWER SUPPLY AND OPERATIONALLY CHECKED NORMAL.SDR 95UAL900287Battery Pack · dischargedRIGHT HAND OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATED NORMAL.SDR 95UAL900162Retract Mech · malfunctionedAT FL 330 MACH .80, EXPERIENCED A LOUD BANG WITH RED NOSE GEAR WARNING AND UNCOMMANDED NOSE GEAR EXTENSION. SLOWED AIRCRAFT AND GEAR RETRACTED.SDR 95UAL900082Engine · flame-outNUMBER ONE ENGINE FLAMED-OUT IN FLIGHT.SDR 95UAL900075Eel Battery · dischargedEMERG EXIT LIGHTS BEGAN FLASHING AT DOORS 1L AND 1R AND WERE ON STEADY AT 2L AND 2R. RESET CIDS AND 1L AND 1R WORKED NORMAL, BUT COULD NOT CORRECT 2L AND 2R. REPLACED EMERGENCY POWER UNIT AND BATTERY. TEST OF EPSU REVEALED UNIT OK.SDR 95UAL900070Actuator · leakingGREEN HYD SYSTEM QTY INDICATION APPROACHED YELLOW BAND, FLIGHT DIVERTED TO DEN. GEAR EXTENDED MANUALLY, LANDED WITHOUT INCIDENT. REPORTED LT INBOARD AILERON ACTUATOR HAD PIN HOLE HYD LEAK ON TOP OF ACTUATOR. REPLACED ACTUATOR.SDR 95UAL900039Elevators · out of tolCREW REPORTS HIGH SPEED BUFFET, WHEN SPEED IS BETWEEN 305 AND 320 KNOTS AT FLIGHT LEVEL 28.0, APPEARS TO GO AWAY WHEN SPEED DROPS BELOW 300 KNOTS. REPLACED BOTH ELEVATORS AND THS ACTUATOR.
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