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 UALA2010071902564Apu · faultyAFTER PACKS WERE TURNED ON ACFT HAD A FOUL SMELL. DURING PACK BURNOUT FOUND APU TO BE THE SOURCE OF OIL SMELL IN ACFT CABIN. AFTER APU SHUTDOWN, THEN RE-START SMELL CAME BACK. RECOMMEND REPLACING CABIN RECIRC FILTERS DUE TO POSSIBLE CONTAMINATION.-DURING PACSDR UALA2010071902570Skin · damagedCREW REPORTED DAMAGE TO NOSE AREA FWD OF NOSE GEAR. APPROX 8 INCHES FWD OF NOSE EE DOOR, ACROSS EE DOOR AND 1' AFT. BLENDED DAMAGE FWD OF E&E DOOR WITHIN LIMITS AND PRIMED. CUT OUT DAMAGE AFT OF DOOR PERFORMED NDT INSP OF DAMAGE REMOVAL FRAMES AND STRINGER NOSDR UALA2010071902581Stringer · corrodedSTRINGER JUST BELOW THE CABIN OUTFLOW VALVE IS CORRODED. REPAIR IAW SRM 51-42-11,ON WU P7018X,AND SRM 51-75-12.SDR UALA2010071902590Antenna · corrodedRT SIDE AIRPHONE ANTENNA FOUND DAMAGED. ANTENNA IS CRACKED ALONG THE ENTIRE LENGTH OF THE BASE. REPLACED ANTENNA. ANTENNA WAS CORRODED.SDR UALA2010071402520Oxygen System · dischargedUPON ARRIVAL TO GATE O2 DROP TO 0 PSI SERVICED O2 TO FULL 1900 PSI AT 24 DEGREES C. ACCOMPLISHED TSM TASK 35-10-00-810-813 LEAK CHECK OF LOW AND HIGH PRESS CIRCUITS HAD NO LEAKS. CHECKED ALL CONNECTIONS ARE THE CORRECT CONDITION. PRESSURE REMAINING AT 1900 PSSDR UALA2010071402522Slide · no testFAILS PTP TEST. FWD LT LOAD. CHANGED RT SLIDE. REPLACED RT FWD DOOR ESCAPE SLIDE. OPS ARE NORMAL.SDR UALA2010071402527Panel · damagedVIBRATION NOISE ENCOUNTERED IN FLIGHT. ACP VIBRATION CK AND FOUND PANEL 191DT HAS EROSION DAMAGE ON L/E OF PANEL. ACP QUICK DISPATCH SPEED TAPE REPAIR. A PERMANENT REPAIR MUST BE ACCOMPLISHED WITHIN 300 FLT HOURS. FLT 225-25 CREW REPORTS NO VIB-NOISE FELT ISDR UALA2010071302513Terminal Block · burnedFOUND BURNED AND LOOSE CONNECTION ON CTR CONDUCTOR AT 1999VT IN AFT LT CEILING OF FWD PIT. REPLACED 1999VT TERM BLOCK AND SECURED NR1 & NR3 LUGS. MADE ENOUGH SLACK TO CLIMP ON NR2 LUG 56 1-YV200, AND THE AFT SIDE 2EA 6GA LUGS NEEDS REPLACED AND WIRE SPLICED ISDR UALA2010071202473Slide · unwanted deployDOOR 2R SLIDE DEPLOYED DURING AIRCRAFT SERVICING. DOOR EMERGENCY BOTTLE DID NOT BLOW. DOOR SLIDE HANDLE WAS CONFIRMED 'DISARMED' PRIOR TO DOOR OPENING. INITIAL INVESTIGATION SHOWED A STEEL CABLE FROM THE SLIDE FELL OFF AND GOT HUNG WITH THE GIRT BAR BRACKETSDR UALA2010070902446Slide · defectiveDOOR 2L PRESSURE GAUGE VERY DIFFICULT TO READ. REPLACED SLIDE PER AMM.SDR UALA2010070902449Power Supply · faultyDURING EMERGENCY LIGHT SYSTEM TEST, FAULTED INT LOADS EMER LEFT. REPLACED LEFT EPSU AND BATTERY, ALSO AFT BATTERY, OPS NORMAL.SDR UALA2010070902451Floorbeam · corrodedCORROSION FOUND ON FLOORBEAMS FRAME 24 DURING FLOORBOARD REPLACEMENT. THREE (3) EA FLOORBEAMS EXTENSIVE CORROSION. EXFOLIATION CORROSION FOUND BETWEEN FRAME 21 AND FRAME 24 ON RT SIDE FLOOR RAIL Y-765 APPROX 4 INCHES LONG BY 1 INCH WIDE. CORROSION FOUND ON SDR UALA2010071202456Lanyard · brokenLEFT SLIDE HAS GIRT BAR LACING BROKEN. REPLACED SLIDE ASSY IAW MM. OPS TEST IAW MM.SDR UALA2010070902438Outflow Valve · faultyPRESSURIZATION ISSUE, RTFL. NEEDS NEW AIR OUTLET VALVE 22HQ , NO PARTS IN MSP. SECURED OUTLET VALVE IN FULL CLOSED POSITION PER MEL. SECURED SKIN EXCHANGER ISOL VALVE PER MEL 21090 PROCEDURES. REPLACED SKIN AIR VALVE PER MM AND TESTED PER MM, OPS CHECK OKASDR UALA2010070802435Unknown · odorON DESCENT THROUGH 13K HAD STRONG ELEC BURNING ODOR. NO VISIBLE SMOKE. INSPECTED WINDOW HEAT CONNECTION, CONDUIT, INSP'D CB PANELS IN COCKPIT, INSPECTED PEDESTAL AREA, LT EE, NOSE EE, BOTH RT EE'S RAN BOTH ENG'S FOR TEN MIN WITH BOTH PACKS ON WARM, TURNED ONSDR UALA2010070902454Circuit Board · failedEMERGENCY EXIT LIGHT BULB ON UPPER CONSOLE BURNED OUT. "OFF" LIGHTS WORK DURING LAMP TEST, BUT DO NOT ILLUMINATE WHEN SWITCH IS PLACED "OFF". CHECKED FUSE "F" FOR OPEN CIRCUIT. FOUND BOARD 7LP CAUSING ISSUE. LIGHT WORKS OFF PIN 44 REF ASM. FOUND THAT BOARSDR UALA2010070702420Battery Pack · failedEMERGENCY LIGHT TEST FAILS FOR RIGHT OVERWING LIGHT BATTERY. REPLACED RT OVERWING EMERGENCY LIGHT BATTERY. EMERGENCY LIGHT TEST PASSED.SDR UALA2010070702421Power Supply · malfunctionedCABIN EMERGENCY EXIT LIGHT TEST GIVES 'EPSU INTERNAL LOAD FWD LEFT' FAULT. REPLACED BATTERY AND POWER SUPPLY. SYSTEM TESTS OKAY.SDR UALA2010070802427Stowage Box · malfunctionedCAPT O2 MASK DOES NOT TEST WITH PRESS TO TEST-BUTTON. REPLACED CAPTS O2 MASK BOX, CHECKS NORMAL.SDR UALA2010070202363Oxygen System · malfunctionedCAPT O2 MASK TEST BUTTON ON DOOR DOES NOT RESET AFTER BEING PUSHED. REPLACED O2 BOX, LEAK CHECKS AND OPS CHECK OKAY.SDR UALA2010070602365Gcu · failedNR 2 ENG GEN FAILURE, RTFL. CHECKED CDFS, FOUND LOW OIL PRESSURE. CHECKING OIL LEAKAGE. SVCD ONE QT OF OIL. RAN APU TEST OK. APU HOURS METER READ 02530. TROUBLESHOOTING GEN 2 INOP. PFR FAULTING GCU-2 1XU2. REPLACED GCU 2, TESTS OK IAW CFDS AND RAN ENGINE. GSDR UALA2010070102345Rib · delaminatedCLOSURE RIB 1 ON LT OUTBOARD FLAP IS DAMAGED. THE DAMAGE IS AN AREA OF DELAMINATION OF APPROXIMATELY 1.5 INCH IN DIAMETER. MAJOR REPAIR ACP'D. DAMAGED AREA WAS CUTOUT AND REPAIRED PER SRM AND UA-EVA-73902 REV B. REPAIR AND RII INSP WAS ACP'D ON SMB N-R K50SDR UALA2010070102348Structure · dentedDENT ON LEADING EDGE NR 2 SLAT APPROX 1 FT OUT FROM INBOARD EDGE MEASURES 6-32 DEEP. TEMPORARY REPAIR INSTALLED. MUST INSTALL STRUCTURAL INSERT REPAIR WITHIN 4500 FC, OR 6000 FH OR 20 MONTHS OR CHECK WHICHEVER OCCURS FIRST. REPLACED SLAT ON WUP K4341F.SDR UALA2010070202355Microphone · inoperativeCAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. CREW COMMENTS: CAPTS O2 MASK MICROPHONE INTERMITTENTLY INOP DURING TEST AND IN USE, O2 IS OK. REPLACED MASK, MASK BOX AND AMU. O2 AND AUDIO CHECKS OK, LEAK CHECK OKAY.SDR UALA2010063002334Slide · faultyMESSAGE EXT LOADS LT AFT DISPLAYED ON PTP FOR EMERGENCY LIGHT TEST. REPLACED LT AFT DOOR ESCAPE SLIDE. INSP'D SLIDE AT DOOR 2L, SLIDE SECURED ON DOOR, PIN REMOVED AND STOWED, ASSIST BOTTLE RE-ARMED AND SAFETIED, EMERGENCY LIGHTS TEST OKAY. ACFT RETURNED TO SDR UALA2010063002337Slide · faultyEMERGENCY LIGHT TEST FAILED. 'EXT LOADS AFT L' MSG DISPLAYED. REPLACED 13WL EPSU AND BATTERY, NO HELP. NEED MORE TIME TO T-SHOOT PER MT 33-001 REV-B MAINTENANCE ACTION AND TSM. REPLACED SLIDE AND EPSU 13 WL BATTERY PER AMM.SDR UALA2010062902318Unknown · unknownRAPID DEPRESSURIZATION AT 3000FT IN DESCENT FOR LANDING. PERFORMED AFS TEST PER AMM, TEST OKAY. TESTED CPC1, CPC2 AND MANUAL PRESSURIZATION PER AMM. TEST OK. ALL FAC'S AND FMGC'S CK'D NORMAL. OK EGT TEMPERATURE WITHIN LIMITS JRH INLET-EXH. CK OK AIDS EXCSDR UALA2010063002322Bracket · out of adjustR FWD EMERGENCY EXIT DISPLAYED ON UPPER ECAM SCREEN - DOOR. CREW COMMENTS: FWD RT OVERWING EMERG EXIT DOOR OPEN ECAM DURING EARLY TAKEOFF ROLL. ABORTED. REPEAT GRIPE. ADJUSTED BRACKET PANEL ATTACHES TOO, FOR A SECURE FIT. TAKEOFF ROLL AT 20 KNOTS, BRAKE TSDR UALA2010063002326Seal · brokenAFT WATER FIRE EXT HAS BROKEN SEAL. REPLACED BOTTLE WITH BOTTLE ROBBED FROM 4042 FWD CABIN.SDR UALA2010062802304Control Unit · faultySDCU MAINTENANCE STATUS CLASS II MESSAGE DISPLAYED ON LOWER ECAM. SUPPLEMENTAL DATA UPDATE SDCU PREVIOUS FLT LEGS SHOWED INTERMITTANT FAULT MSG "SDCU CHANNEL 1 (10WQ)". REPLACED SCDU UNIT. OP TESTS OKAY.SDR UALA2010062802276Apu · smokeAPU PRODUCED ODOR IN CABIN, GROUND PERSONNEL REPORTED APU PUTTING OUT SMOKE, SOME OILY SMOKE IN VENT WITH APU BLEED ON ACCOMPLISHED MT 72-016 AND FOUND APU OUT OF OIL, FOUND OIL IN PNEUMATIC DUCT AFT OF LOAD CONTROL VLV. CK MAG PLUG AND EXHAUST AREA NO EXTERSDR UALA2010062802284Unknown · smokeSMOKE REPORTED IN AFT GALLEY 10 MIN PRIOR TO LANDING. NO SMOKE FOUND BY CREW. OPERATED AFT GALLEY OVENS, HOT PLATES AND COFFEE MAKERS AND CHECKED AFT ELECTRICAL PANELS WITH NO EVIDENCE OF SMOKE. OK FOR SERVICE.SDR UALA2010062802280Smoke Detector · false activationAFT CARGO SMOKE DISPLAYED ON UPPER ECAM SCREEN. AGENT 1 DISCHARGED, AFT CARGO 'SMOKE' LIGHT ON OVERHEAD PANEL ALSO ILLUMINATED. PFR, LLR, AND PLR ALL SHOWED NO FAILURES. CFDS SDCU TEST-SMOKE LOOPS AFT LDCC-TESTED OK. LOOP A AND B OK. BOTTLE REPLACED.SDR UALA2010062802286Computer · faultyECAM VENT BLOWER FAULT. FLIGHT DIVERTED. REPLCED AEVC 10HQ PER MM. REPLACED SKIN AIR INLET VALVE 15HQ PER MM. REPLACED SKIN AIR OUTLET VALVE 22HQ PER MM (P/N VFT300A1AMDTA - SERIAL 2041). ACP SUCCESSFUL OP TEST OF AVIONICS EQUIPMENT VENTILATION SYSTEM.SDR UALA2010062502269Thermostat · faultedENG NR 2 BLEED FAULT, RTFL. THERMOSTAT FAILURE. REPLACED NR 2 ENGINE FAV CONTROL THERMOSTAT. TESTS OKAY DURING HIGH POWER RUN.SDR UALA2010062102179Lamp · failedEMERGENCY LIGHTS TEST FAILS WITH 'EXTERNAL LOADS EMER R' MESSAGE. RELAMPED AFT OVERWING LIGHT ASSY.SDR UALA2010062102169Sliding Window · delaminatedCAPTAIN'S SLIDING WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS. NEED TO EVALUATE CONDITION. CREW COMMENTS: CAP SLIDING WINDOW, VERYHOT, MANY DELAMINATION BUBBLES OBSCURING VISIBILITY. REPLACED LT SLIDING WINDOW.SDR UALA2010062102191Eec · malfunctionedP2T2 FAULTS NR1 ENG, FLT DIVERTED. DUE TO EPR MODE FAULT NR 1 ENG REPLACED EEC NR 1 ENG. RCV'D 2ND ENG 1 FADEC B FAULT. REPLACED EEC. RAN NR 1 ENG NO FAULTS NOTED. ENG 1 SENSOR FAULT ON A LATER SEGMENT, REPLACED EEC. ACPD NR 1 ENG RUN. NO FAULTS NOTED.SDR UALA2010062102188Oxygen Mask · no testCAPTAIN'S O2 WILL NOT TEST. REPLACED CAPTAIN'S O2 MASK ASSY. OPS GOOD.SDR UALA2010061702135Control Unit · malfunctionedBRAKING ABNORMAL. CREW LOST BSCU 1 AND NOSE WHEEL STEERING ON LANDING. BSCU 2 ALREADY DEFERRED. POST FLIGHT REPORT POINTS TO BAD BSCU. REPLACED BSCU, CHANNEL 1 & 2 BITE TEST PASS.SDR UALA2010061702141Window · noisyL3 COCKPIT WINDOW IS NOISY. NOISE COMING FROM LOOSE SEAL. BECOMES NOISIER AS SPEED BUILDS. REPLACED COCKPIT WINDOW L3.SDR UALA2010061702142Smoke Detector · false activationLAV SMOKE DETECTOR MESSAGE. ACCOMPLISHED LAV SMOKE DETECTOR OPS TESTS, ALL PASSED, NO FAULTS.SDR UALA2010061802148Slide · faultyDURING CABIN CREW SERVICE CHECK AND 3SV MX CHECK OF THE EMERGENCY LIGHT CHECK, CIDS MESSAGE EXT. LOADS AFT L. 2L DOOR EMERGENCY LIGHTS INOP. ALL EMERGENCY LIGHTS ARE INOP AND ALSO THE AFT OUTER LT WING EMERGENCY LIGHT. CHECKED POWER PACK AND LIGHT FOUND TO CSDR UALA2010061602120Power Supply · inoperativeEMERGENCY LIGHT TEST FAULT, 'EPSU INT LOAD EMER R'. REPLACED POWER SUPPLY UNIT AND BATTERY. EMERGENCY LIGHT TEST OK.SDR UALA2010061702131Wire · frayedNR 1 ENGINE UPPER PYLON, ABOVE HIGH STAGE AND ANTI-ICE DUCT HAS SEVERAL WIRE BUNDLES WITH FRAID AND MELTED INSULATION AREAS. PTT'S 5296038 AND 5296 037, 3 EA HARNESSES REPLACED. ALL OPS CHECKS NORMAL.SDR UALA2010061502104Nacelle · damagedGROUND OPS REPORTING DAMAGE TO CNA FOR THE NR 1 ENG STRUCK BY TUG AND OR CART. DETERMINE DIMENSIONS, LENGTH- WIDTH - AND AMOUNT OF DEFLECTION. CNA DAMAGED BEYOND ANY LIMITS. REPLACED CNA.SDR UALA2010061502107Valve · failedSKIN VALVE FAULT, RTFL R & R SKIN AIR VALVE IAW AMM. PERFORMED OPS CHECK, OPS CHECKS OK. PERFORMED OPERATIONAL CHECK, OPS CHECKS OKAY. CFDS BITE CHECK OK.SDR UALA2010061502100Thermostat · failedENG 2 BLEED FAULT, RTFL. PRE-COOLER OUTLET TEMP AMBER 265C FAULTED 2 TIMES. REPLACED ENG 2 FAN AIR THERMOSTAT. LEAK TEST OK.SDR UALA2010061602126Adapter · failedRECEIVED SLIDE WITH PACKING ADAPTER STILL ATTACHED TO THE ASPIRATOR. VACUUM ADAPTER IS USED TO AID DURING PACKING OF THE SLIDE. IT IS TO BE REMOVED WHEN PACKING IS COMPLETED. REMOVED VACUUM ADAPTER FROM SLIDE. PROCEED TO O/H SLIDE.SDR UALA2010061502097Switch · failedRAM AIR TURBINE WILL NOT RETRACT AFTER ACCOMPLISHING PART NUMBER CHECK. *S/D* PERFORMED T/S PER AMM, FOUND BLUE PRESSURE SW 2074GJ FAILED. REPLACED SWITCH AND CONNECTOR. OPS NORMAL.
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