IAE V2500-A1

Service difficulty reports · 306

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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 = 'V2500A1'
  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 20000509SH042Seal · crackedPART RECEIVED FROM WESTFIELD GAGE FOR FPI IAW V2500 MANUAL REVISION 42, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501. PART REJECTED AT FPI DUE TO A CRACK (ONE PLACE ON TOP SURFACE, 0.200 INCH LONG). NOTE: SUBMITTER STATED SECOND TIME THIS SApr 19, 2000 · Turbine Engine Compressor SectionSDR 20000509SH007Bearing · scoredENGINE WAS REMOVED FOR ''NR 4 BEARING INSPECTION/REPAIR''. THE NR 4 BEARING EXHIBITED AXIAL SCORING OF THE ROLLERS AND OUTER RACE. . (X)Apr 18, 2000 · Turbine Engine Compressor SectionSDR 20000512SH023Seal · crackedPART RECEIVED FROM WESTFIELD GAGE CO., FOR FLUORESCENT PENETRANT INSPECTION IAW IAE V2500 PROPULSION SYS ENG MANUAL, REV 42, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501. PART REJECTED AT F.P.I. DUE TO A CRACK ONE PLACE ON TOP SURFACE, 0.200 IApr 13, 2000 · Turbine Engine Compressor SectionSDR 20000509SH006Seal · crackedFLUORESCENT PENETRANT INSPECTION IAW I.A.E. V2500 PSEM, REV 42, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501). PART REJECTED AT F.P.I. DUE TO A CRACK ON THE TOP SURFACE, 0.180 INCH LONG (AS MARKED). (X)Apr 11, 2000 · Turbine Engine Compressor SectionSDR AWXA0000209Sensor · failedNR 1 ENG SENSOR FAULT AVOID RAPID THROTTLE CHANGE. REMOVED AND REPLACED NR 1 ENG EEC TT 00409972 M+E 26-7320-9-0016 CURRENT HISTORY NOT AVAILABLE COMPUTER DOWN. REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT.Apr 1, 2000 · N635AW · Airbus A320231 · Fuel Control/Turbine EnginesSDR 20000331SH008Bearing · failedENGINE WAS REMOVED DUE TO ''''METAL ON MCD''''S, METAL IN FILTER, VIBRATION AND STALLS''''. DISASSEMBLY OF THE ENGINE REVEALED NR 4 BEARING CAGE HAD FRACTURED. FAILURE INVESTIGATION IS IN PROGRESS AT GE ENGINE SERVICES - DALLAS. (X)Mar 11, 2000 · Turbine SectionSDR 20000518SH011Bearing · failedGEARBOX REMOVED FOR METAL IN CHIP COLLECTOR AND STRAINER. DISASSEMBLY, INSPECTION DISCLOSED BEARING (CAGE) FAILURE. MATERIAL FORWARDED TO IAE ENGINEERING FOR REVIEW. (X)Mar 8, 2000 · Doug MD9030 · Turbine Engine Accessory DriveSDR AWXA0000105Actuator · failedLP 7624668, ENGINE 2 COMPRESSOR STALL OCCURRED TWICE DURING TRANSITION FROM FLEX TO CLIMB. REPLACED E2 VSV ACTUATOR IAW AWA TASK CARD R5M75303. OPS CHECK OK.Feb 29, 2000 · N635AW · Airbus A320231 · Compressor Bleed ControlSDR AWXA0000041Alternator · failedGATE RETURN, ENGINE AUTO SHUT-DOWN, AFTER ENG START, PUSHBACK, AND COMPLETING AFTER START FLOW, ENG 2 ECAM FAILURE MESSAGE CAME UP AND NR 2 SPOOLED-DOWN. REMOVED AND REPLACED NR 2 STATOR, ENG DEDICATED ALTENATOR (EDA). OPS CK NML. ENG SHUT DOWN ON TAXI OUTJan 27, 2000 · N621AW · Airbus A320231 · AC Generator-AlternatorSDR 20000621SH015Bearing · crackedPART RECEIVED FOR FLUORESCENT PENETRANT INSPECTION PER SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501, OF THE IAE V2500 PROPULSION SYSTEM ENGINE MANUAL, REV 41. PART REJECTED AT FPI DUE TO CRACKS 2 PLACES ON TOP SURFACE 0.10 INCH AND 0.125 INCH.Dec 17, 1999 · Turbine SectionSDR 99ZZZX4707Bearing · spalledENGINE WAS 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 TDec 7, 1999 · Airbus A320232 · Turbine Engine Compressor SectionSDR 20000621SH016Seal · crackedPART RECEIVED FOR FLUORESCENT PENETRANT INSPECTION PER IAE V2500 PROPULSION SYSTEM ENGINE MANUAL, REV 38, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501. PART REJECTED AT FPI DUE TO A CRACK 0.200 INCH LONG ON TOP SURFACE. (X)Dec 7, 1999 · Turbine SectionSDR 99ZZZX4135Seal · crackedPART RECEIVED FROM WESTFIELD GAGE FOR FLUORESCENT PENETRANT INSPECTION IAW INTERNATIONAL AERO ENGINE V2500 PROPULSION SYSTEM ENGINE MANUAL, REVISION 38, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501. PART REJECTED AT FPI DUE TO A CRACK ON TOP FOct 8, 1999 · Turbine SectionSDR 99ZZZX4099Bearing · spalledENGINE WAS 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.Oct 6, 1999 · Turbine Engine Compressor SectionSDR AWXA9900343Actuator · failedEMERGENCY DECLARED (NOT BY PILOT) ENG NR 1 COMPRESSOR VANE FAULT ON DESCENT, NO OTHER ABNORMAL ENG INDICATIONS OR FAILURES. FIRST TIME FAULT FADEC CONFIRMS 2.5 BLEED ACTUATOR FAIL CURRENT HISTORY.Oct 6, 1999 · N646AW · Airbus A320231 · Compressor Bleed ControlSDR 99ZZZX4100Bearing · spalledENGINE WAS 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.Sep 24, 1999 · Turbine Engine Compressor SectionSDR AWXA9900325Fuel Pump · failedDURING CLIMB THROUGH FL180, NR 2 ENG COMPRESSOR STALLED 3X. DURING DESCENT BACK INTO CMH ENG RPM AND F/F WAS LOWER THAN NR 1. DURING TAXI BACK, NR 2 ENG FAILED. REMOVED AND REPLACED NR 2 ENG MAIN FUEL PUMP IAW TASK CARD R5M73304. OPS CK NML. AFTER DIRECTISep 23, 1999 · N643AW · Airbus A320231 · Engine Fuel PumpSDR 99ZZZX3712Seal · crackedPART RECEIVED PER SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501 FOR THE INTERNATIONAL AERO ENGINES V2500 PROPULSION SYSTEM ENGINE MANUAL, REV 38. PART REJECTED AT F.P.I. DUE TO 4 CRACKS ADJACENT TO MACHINED FLANGE; 0.020 INCH, 0.025 INCH, 0.050Sep 17, 1999 · Turbine SectionSDR 99ZZZX3648Bearing · crackedPART RECEIVED FROM WESTFIELD GAGE CO FOR FLUORESCENT PENETRANT INSPECTION PER SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501 OF THE INTERNATIONAL AERO ENGINE V2500 PROPULSION SYSTEM ENGINE MANUAL (REVISION 38). PART REJECTED AT FPI DUE TO CRACK Sep 9, 1999 · Engine (Turbine/Turboprop)SDR 99ZZZX3663Bearing · spalledENGINE WAS REMOVED DUE TO M50 MATERIAL ON THE MAG CHIP DETECTORS. DISASSEMBLY OF THE ENGINE REVEALED THE NR 4 BEARING EXHIBITED SPALLING DAMAGE TO THE OUTER RACE. THE BEARING WAS SUBMITTED TO THE LAB FOR ANALYSIS. THE INVESTIGATION IS STILL IN PROGRESS AT TSep 8, 1999 · Turbine Engine Compressor SectionSDR 20000712SH021Seal · crackedPART RECEIVED FOR FLUORESCENT PENETRANT INSPECTION PER SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501, IAW INTERNATIONAL AERO ENGINE V2500 PROPULSION SYSTEM ENGINE MANUAL, REV. 38. PART REJECTED AT F.P.I. DUE TO CRACK 0.3580 INCH LONG ON TOP SURJul 21, 1999 · Turbine SectionSDR 99ZZZX2517Seal · crackedPART RECEIVED FROM WESTFIELD GAGE CO., INC., FOR FLUORESCENT PENETRANT INSPECTION PER SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501, IAW INTERNATIONAL AERO ENGINE V2500 PROPULSION SYSTEM ENGINE MANUAL. PART REJECTED AT FPI DUE TO CRACK 9.0360 IJun 15, 1999 · Turbine Engine Compressor SectionSDR AWXA9900222Compressor · stalledAIR TURNBACK, NR 2 ENGINE COMPRESSOR STALL AND HIGH EGT. NONE RECEIVED. WILL UPDATE WHEN INFORMATION IS AVAILABLE.Jun 14, 1999 · N636AW · Airbus A320231 · Turbine Engine Compressor SectionSDR 99ZZZX2232Seal · crackedPART REJECTED AT FLUORESCENT PENETRANT INSPECTION DUE TO CRACK ON OUTSIDE TOP FLAT, APPROXIMATELY 0.375 INCH IN LENGTH, AS MARKED ON PART.May 19, 1999 · Turbine Engine Compressor SectionSDR 20000712SH040Bearing · crackedPART REJECTED FOR CRACKS IN 2 PLACES. 2 CRACKS ON OUTSIDE DIAMETER WALL IN CLOSE LINEAR ALIGNMENT - 0.060 INCH THICK. CRATER TYPE CRACK IN INSIDE DIAMETER FLANGE, 0.125 INCH DIAMETER. (X)May 10, 1999 · Turbine SectionSDR 99ZZZX2173Seal · crackedSUBMITTER STATED THIS IS AN ON-GOING PROBLEM WITH THIS PART. FAIL F.P.I. FOR CRACKS ALMOST ALWAYS IN THE SAME GENERAL AREA.May 1, 1999 · Turbine Engine Compressor SectionSDR 99ZZZX2429Turbine Disc · crackedDURING INSPECTION OF PARTS FOR THIS ENGINE, FOUND THE HPI T/DISC HAD CRACKING FROM ITS AIR METERING HOLES AND BELLING OF THE FRONT SECTION. THESE FEATURES HAVE BEEN CAUSED BY A FIRE WHICH WAS PRESENT IN THE NR 6 BEARING COMPARTMENT.May 1, 1999 · Airbus A320212 · Turbine SectionSDR 99ZZZX1914Spacer · failedVISUAL AND BINOCULAR INSPECTION OF THE SPACER REVEALED SOME ENTRAPPED COPPER-COLORED METALLIC DEBRIS IN THE SLOTTED RECESS ON THE SIDE FACE FLAT. FINE GRIT-LIKE PARTICLES WERE ALSO OBSERVED IN THE BORE ANNUAL RECESS. THE ANODIZED SURFACES EXHIBITED A MOTTLEApr 27, 1999 · Turbine Engine Accessory DriveSDR 20000712SH030Seal · crackedPART REJECTED AT F.P.I. DUE TO A CRACK 0.180 INCH ON TOP SURFACE. (X)Mar 30, 1999 · Turbine SectionSDR 20000712SH032Bearing · crackedPART REJECTED AT F.P.I. DUE TO A CRACK ON TOP SURFACE, .0175 INCH. (X)Mar 30, 1999 · Turbine SectionSDR 99ZZZX920Seal · crackedTURBINE SEAL CRACKED.Feb 11, 1999 · Turbine SectionSDR 20000712SH041Bearing · crackedPART REJECTED FOR CRACKS 2 PLACES ON TOP SURFACE: CRACK NR 1, THROUGH CRACK .400 INCH LONG. CRACK NR 2, CRACK 0.500 INCH LONG. (X)Feb 8, 1999 · Turbine SectionSDR 99ZZZM212Engine · failedFLT 8251 IN DEN, NR 1 ENGINE FIRE INDICATION FOLLOWED BY ENGINE FAILURE. RETURNED TO DEN, OVERWEIGHT LANDING. NR 1 ENGINE CHANGE IS SCHEDULED IN DEN. (M)Jan 26, 1999 · Airbus A320231 · Engine (Turbine/Turboprop)SDR 99ZZZX2629Turbine Disc · crackedDURING INSPECTION OF PARTS FROM THIS ENGINE, FOUND THE HPI TURBINE DISC HAD CRACKING FROM ITS AIR METERING HOLES AND BELLING OF THE FRONT SECTION. THESE FEATURES HAVE BEEN CAUSED BY A FIRE WHICH WAS PRESENT IN THE NR 6 BEARING COMPARTMENT.Jan 26, 1999 · Airbus A320231 · Turbine SectionSDR 99ZZZX615Seal · crackedPART REJECTED DUE TO CRACK .190 INCH LONG AND LINEAR INDICATION .375 INCH LONG. JOB FOR: WESTFIELD GAGE P.O NR 98832.Dec 15, 1998 · Turbine SectionSDR 99ZZZX613Seal · crackedPART REJECTED AT FPI DUE TO CRACKS IN 2 PLACES ON TOP SURFACE: CRACK 'A' = 2 INDICATIONS 0.015 INCH AND 0.020 INCH. CRACK 'B' = 1 INDICATION 0.250 INCH. JOB FOR: WESTFIELD GAGE (P.O. NR 97553).Nov 2, 1998 · Turbine SectionSDR 99ZZZX620Seal · crackedPART REJECTED AT FPI DUE TO CRACK 0.500 INCH LONG ON SMALL OUTSIDE DIAMETER BEND RADIUS. JOB FOR: WESTFIELD GAGE P.O. 97541.Nov 2, 1998 · Turbine SectionSDR 99ZZZX618Seal · crackedPART REJECTED DUE TO CRACKS - 2 PLACES ON TOP FACE 0.750 INCH AND 1.500 INCH LONG (CRACKS VERIFIED BY MICROSCOPE).Sep 4, 1998 · Turbine SectionSDR 99ZZZX616Seat · crackedPART WAS REJECTED DUE TO 0.125 INCH CRACK ON TOP SURFACE. JOB FOR: WESTFIELD GAGE.Aug 12, 1998 · Turbine SectionSDR 99ZZZX617Seal · crackedCRACKS - 2 PLACES ON TOP SURFACE, AS MARKED 0.250 INCH AND 0.450 INCH.Jul 8, 1998 · Turbine SectionSDR 99ZZZX621Seal · crackedPART WAS REJECTED DUE TO NUMEROUS CRACKS ON INNER DIAMETER SURFACE.Apr 8, 1998 · Turbine SectionSDR 99ZZZX619Housing · failedTHIS IS A TITANIUM HOUSING WHICH HAS FAILED FPI INSPECTION. PART IS CRACKED IN TWO LOCATIONS. PART IS SCRAP.Jan 1, 1998 · Turbine SectionSDR AWXA9700655Engine · overtempSHUTDOWN ENGINE NR 1 DUE TO OVERTEMP/BLEED VALVE HI AND LO OPEN. ACCOMPLISHED BORESCOPE INSPECTION PER MM 72-00-00, PAGE 258. NO ABNORMALITIES NOTED. ENGINE NR 2 FUEL FAULT ON SHUTDOWN NOTED BY MX. BITE TEST OK. REMOVED AND REPLACED NR 1 ENGINE.Oct 23, 1997 · N622AW · Airbus A320231 · Engine (Turbine/Turboprop)SDR AWXA9700590Vsv Actuator · faultedAIR TURNBACK 15 TO 20 SECONDS AFTER TAKEOFF NR 1 ENGINE ECAM MESSAGE ENGINE NR 1 COMPRESSOR VANE. AT TOGA NR 1 ENGINE 635 TO 638. REDUCED TO CLIMB POWER AND TEMPERATURE REDUCED TO 600 TO 618. ECAM CLEARED. WARNING RETURNED AT LANDING. REMOVED AND REPLACED Sep 27, 1997 · N633AW · Airbus A320231 · Compressor Bleed ControlSDR AWXA9700070Vsv Actuator · failedNR 2 ENGINE COMPRESSOR FAULT. ENGINE SHUT DOWN ON DESCENT. REMOVED AND REPLACED NR 2 ENGINE VSV ACTUATOR, IAW CARD R5M75303. OPS AND LEAK CHECK GOOD.Feb 2, 1997 · N620AW · Airbus A320231 · Compressor Bleed ControlSDR CA970107006Fuel Pump · sheared shaft(CAN) ENGINE DID NOT PRODUCE TAKEOFF POWER AND WAS DIFFICULT TO START. INVESTIGATION FOUND THE TWO STAGE FUEL PUMP WAS NOT DELIVERING THE VOLUME OF FUEL REQUIRED, DUE TO A SHEARED DRIVE.Dec 26, 1996 · Airbus A320231 · Engine Fuel PumpSDR 97ZZZX197Engine · malfunctionON TAXI OUTBOUND AT SFO, PILOT REPORTED ENG NR 1 HAD N1, N2 DROP AND THE EGT ROSE TO OVER 636 FOR A FEW SEC. A/C RETURNED TO RAMP WHERE RIGGING OF VSV OF 7TH AND 10TH STAGE BLEED VALVES WERE CHECKED. ENG WAS ALSO CHECKED FOR HIGH TEMP. MASTER VSVA ACTUATOR Dec 7, 1996 · N941LF · Engine (Turbine/Turboprop)SDR 97ZZZX212Engine · failedON TAXI OUT OF SFO, PILOT REPORTED ENG NR 2 FAILED. A/C RETURNED TO GATE AND AFTER INSPECTION (DELAY OF 2 HRS, 23 MIN) A/C CONTINUED TO MEX. AND TO SFO W/O PROBLEM. PFR GAVE ECAM MSE 'ENG 1 VANE COMPRESSOR' WITH CFDS MESSAGE 'VSV MECH/HYD VALVE, ENG INSP'. Dec 2, 1996 · N941LF · Airbus A320232 · Engine (Turbine/Turboprop)SDR AWXA960423Oil Scav Pump · failedRNO - FLT 2012 - ON ARRIVAL IN RNO AND SHUTDOWN, GROUND CREW REPORTED A TAIL PIPE FIRE IN THE NR 2 ENGINE. AFTER SUBSEQUENT DRY MOTORINGS, GROUND FIRE EXTINGU ISHER WAS USED, THE FIRE WAS PUT OUT. FOUND OIL PUDDLED IN ENGINE CORE TAIL PI PE. REMOVED AND REPAug 25, 1996 · N625AW · Airbus A320231 · Turbine Engine Oil SystemSDR AWXA960289Eec · failedPHX/ORD - FLT 0004 - ABORTED TAKEOFF. NR 1 ENGINE DID NOT MAKE TAKEOFF POWER. REPLACED NR 1 ENGINE EEC PER R9373301. OPERATIONS CHECK GOOD. PART TOTAL CYCLES, 5,817. (X)Jun 24, 1996 · N635AW · Airbus A320231 · Fuel Control/Turbine Engines
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