JASC 7250
Service difficulty reports · 3,624
Reports filed under 7250 · Turbine Section, newest first.
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 jasc_code = '7250' 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 jasc_code = '7250' 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 ASMF200910001Valve · leakingACFT RETURNED TO PLATFORM DUE TO A RT ENGINE FUEL LEAK. MX DETECTED A FUEL LEAK OUT OF LIMITS IAW MM 71-71-00 PAGE 606, PROCEEDING FROM THE HPTACC VALVE. ACFT WAS SENT TO THE HANGAR AND HPTACC VALVE WAS REPLACED AND TESTED IAW MM 75-21-01 AND TASK 71-00-00-7SDR CA091007001Lock Pin · missing(CAN) DURING DISASSEMBLY OF THE ENG AFTER SPLITTING THE HP2 TURBINE DISC FROM THE HPT1 TURBINE DISC IT WAS FOUND THAT LOCKING PLUGS WERE MISSING. THE LOCKING PLUG IS PREVENTING THE LOCKING RING HOLDING THE HP1 TURBINE BLADES TO BE RELEASE. THE LOCKING RING WASSDR ERAA200900009Turbine Blades · damagedLOUD NOISE FROM RIGHT ENGINE DURING TAKEOFF. ABORTED TAKEOFF. REMOVED NR 2 POWER SECTION AND FOUND DAMAGE ON 2ND STAGE POWER TURBINE BLADES. REMOVED AND REPLACED ENGINE.SDR DL777091517Shroud · damagedTHE 1ST STG LPT OUTER SHROUD WAS BORESCOPED PER OPN 52140. DAMAGE WAS FOUND IN THE OUTER SHROUD. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.SDR GLBA20090910ATurbine Wheel · damagedPILOTS REPORTED THAT UPON TAKEOFF WITH TORQUE ONLY AT 3200 FOOT LBS. RT ITT EXCEEDED 800 C. AND THE TAKEOFF WAS THEN ABORTED. MX PERFORMED MANY CHECKS INCLUDING AN INSP OF THE BLEED AIR VALVE IAW 75-30-00. MX PERFORMED A HOT SECTION BORESCOPE AND FOUND SOME RSDR 2010FA0000216Turbine Blades · fracturedTHE REPORT SUGGEST THAT THE LPT3 BLADE HAD FRACTURED IN HIGH CYCLE FATIGUE THAT HAD PROPAGATED FROM AN INTERGRANULAR CRACK ON THE AIRFOIL T/E.SDR CA090903005Blades · fracturedON TAKEOFF ROLL LOW ENGINEOIL PRESSURE AND ENGINE FIRE WARNINGS ACTIVATED. TAKE OFF WAS ABORTED. INITIAL INSP REVEALED FRACTURED POWER TURBINE BLADES AND AN EXTERNAL OIL LEAK. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUSE.SDR SWAA095583Engine · overheatedABORTED TAKEOFF / DECLARED EMERGENCY. ON TAKEOFF NR 1 ENG OFF EGT WAS CLIMBING THRU, 800 REDUCED POWER TO MAINTAIN LIMITS AND RETURNED TO AIRPORT. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR FDKA2009082400177Engine · damagedASH FLT 6106 GRR TO CVG. RTF DUE TO NR 1 ENGINE SHUT DOWN, OIL PRESSURE DROPPED TO ZERO. EMERGENCY DECLARED. CONTRACT MX FOUND ENGINE DIFFICULT TO TURN AND METAL IN THE EXHAUST. MX R2 NR 1 ENGINE OPS LEAKS GOOD.SDR DL76L091322Turbine Blades · damagedFAIL SCHEDULE BOROSCOPE INSPECTION. TURBINE BLADE DAMAGED ON SECOND STAGE OF LPT. REPLACED NR 1 ENGINE.SDR 2009FA0000926Blade · separatedON AUG 6, 2009 AT 6:45 AM, DURING TAKEOFF, THE NR 2 ENGINE FAILED WITH A REPORTED "LOUD SHARP BANG" RESULTING IN THE ACFT`S "YAWING". THERE WERE NO INDICATIONS OF FIRE/SMOKE, HOWEVER, AN EMERGENCY WAS DECLARED AND ACFT RETURNED TO DEPARTURE AIRPORT AND LANDEDSDR 2009FA0000739Turbine Nozzle · wornENG WAS RECEIVED FOR REPAIR DUE TO NOISE. UPON DISASSEMBLY OF THE TURBINE IT WAS DISCOVERED THE NR 2 NOZZLE DIAPHRAGM HAD BEEN DISLODGED FROM THE CASTING AND WAS MAKING CONTACT WITH THE 2ND STAGE WHEEL. MORE THAN HALF OF THE DIAPHRAGM AND BEEN WORN AWAY; THE SDR SWIA200922266Case · crackedLEFT ENGINE LOW PRESSURE TURBINE CASE CRACKED BEYOND LIMITS. (C-CHECK) REPLACED ENGINE.SDR UALA2009072302190Blade · brokenNR 1 ENG OIL PRESS & QTY ZERO, ENG SHUTDOWN. ENGINE SUFFERED A T-2 BLADE FAILURE. RESULTING UNBALANCE BROKE THE OIL TUBES LEADING TO THE OIL LOSS. ENGINE REPLACED. ACCOMPLISHED TWO CROSS COUNTRY FLIGHTS WITH NO DISCREPANCIES REPORTED.SDR CA090720002Turbine Blades · broken(CAN) DURING A ROUTINE 30 HR INSP, N2 TURBINE BLADE IS INSP IAW ALERT LETTER 2726/09/ARID/82 AND TIP AREA OF BLADE WAS FOUND MISSING. ENG WAS SENT TO FOR INSP AND REPORT TO FOLLOW.SDR CA090717001Turbine Blades · failed(CAN) ON T/O AT 4000 FT, LOUD BANG ON ENG NR 1, VIBRATION UP TO 9.5. ENGINE FAILED. FIRE HANDLE PULLED BUT BOTTLES NOT FIRED BY FLIGHT CREW. THIS IS AN OLD PN HPT BLADE FAILURE - 13,000 CYCLES ON THE OLD PN BLADES. THIS IS THE FOURTH -5A ENGINE SUFFERING THSDR 2010FA0000044Turbine Wheel · crackedDURING O/H OF THE STAGE 1 HPT DISK AFTER 18642 HRS AND 3330 CYCLES SINCE NEW. INSP OF THE DISK IAW ATA 72-53-02 INSP 001 REVEALED 5 OFF CRACKS DURING A CLASS G FPI. 4 OFF CRACKS WERE NOTED TO THE EDGE OF THE LOWER PRESSURE FACE AND 1 OFF CRACK NOTED TO THE ESDR 2009FA0000623Shaft · fracturedDURING START ATTEMPT, THE POWER SECTION DID NOT ROTATE WHEN THE NG REACHED 13 PERCENT. START WAS ABORTED AND PROPELLER TURNED BY HAND. A NOISE WAS HEARD FROM THE EXHAUST STACK AND DRAGGING/BINDING WAS FELT. POWER SECTION WAS REMOVED AND SENT FOR TROUBLESHOSDR AXSA197WA7/1/09Turbine Wheel · failedPILOT APPLIED TAKEOFF POWER FOR DEPARTURE. AT THE TIME BOTH ENGINES STABILIZED AT 1300 FT/LBS OF TORQUE THE PILOTED HEARD A LOUD BANG FOLLOWED BY A GRINDING NOISE FROM THE RT ENGINE. THE PILOT ABORTED THE TAKEOFF AND SHUTDOWN THE ENGINE AND RETURNED TO THE GATSDR CA090629003Blades · improper partUPON VISUAL INSP AFTER CLEANING, THE WORD "SCRAP" WAS SEEN TO BE VIBROPEENED INTO ALL THE POWER TURBINE BLADES.SDR 2009FA0000691Turbine Blades · crackedDURING HOT SECTION INSP, FOUND 2 HIGH TURBINE BLADES CRACKED ON THE T/E AT MID SPAN OF THE BLADE. WORST CRACK BEING APPROX .360 AND .200. (K)SDR 2009FA0000564Shaft · crackedTHE ENGINE WAS DISASSEMBLED BECAUSE OF A REPORTED VIBRATION. A CRACK WAS DISCOVERED THAT ORGINATED FROM THE CURVIC COUPLING END OF THE SHAFT, MEASURING APPROX 5.5 INCHES AND EXTENDING APPROX 300 DEGREES AROUND THE SHAFT. REPAIR STATIONW/O A105779. ENGINE TOTSDR 2009FA0000563Shaft · crackedTHE ENGINE WAS DISASSEMBLED TO FACILATE INSP BECAUSE OF METAL IN THE OIL. UPON VISUAL INSP, A CRACK WAS DISCOVERED ORGINATING AT THE CURVIC COUPLING END OF THE SHAFT. THE CRACK MEASURED APPROX 4.5 INCHES AND EXTENDED APPROX 270 DEGREES AROUND THE SHAFT.SDR CA091002002Turbine · damaged(CAN) TURBINE RUB NOISE REPORTED ON SHUTDOWN. RECOMENDED REMOVING THE TURBINE AND SENDING OUT FOR INSP. TURBINE WAS REPAIRED FOR N1 RUB.SDR GUUA93672060409AGas Generator · fodDURING CLIMBOUT, SPARKS COMING OUT OF THE NR 1 ENGINE. ALL INSTRUMENT INDICATIONS READING NORMAL AND NO ANNUNCIATOR ILLUMINATED. FOUND NR ONE ENGINE GAS GENERATOR FIRST STAGE COMPRESSOR BLADE DAMAGE DUE TO FOREIGN OBJECT DEBRIS, REPLACED GAS GENERATOR.SDR 2009FA0000509Turbine · seizedDURING EXTERNAL LOAD OPERATIONS AT A HOVER, THE ENGINE STOPPED SUDDENLY CAUSING THE PILOT TO AUTO ROTATE FROM APPROX 80 FEET AGL. THE PROBABLE CAUSE OF THE ENGINE STOPPAGE IS A MALFUNCTION IN THE TURBINE MODULE. RECENT OCCURRENCE, NO PRELIMINARY REPORT PUBLISDR C2XA09CL076Turbine Wheel · crackedDURING COMPLIANCE WITH SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND DURING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL075Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL074Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND DURING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR DL738090915Blades · missingNBR 2 ENG AUTO SHUTDOWN IN FLT. FOUND METAL IN TAILPIPE. REQUIRES ENG CHG REMOVED AND REPLACED ENG IAW TRANSMITTIAL 12T102 MALF-1T0 POS-02 CTL-610344001 SKILL-02 OFF SN ON SN DPN 1 876610, 875403, 715001628.SDR CA090527003Stator · damaged(CAN) NR 1 ENGINE AUTO SHUTDOWN 125NM EST OF YYZ. AN EMERGENCY WAS DECLARED WITH ATC THE FLIGHT LANDED. STATUS MESSAGE: L ENG EEC C1 MAINT MSG ON ARRIVAL: L ENG EEC C1 L PIMU L NECEL VENT VLV, LT ENG STARTER REMOVED FOR ACCESS. N2 TRANSDUCER STATOR REMOVSDR C2XA09CL072Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL071Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND DURING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR C2XA09CL068Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL061Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR CA090608001Turbine · stalled(CAN) EIR ENGINE STALLING.SDR C2XA09CL060Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR 2009FA0000366Turbine · failedON LANDING THE PILOT SAID HE HEARD A POP AND THE ENGINE STARTED TO SPOOL DOWN. HE PULLED OFF THE RUNWAY AND STOPPED BUT THEN SAW SMOKE COMING FROM THE EXHAUST AND THOUGHT IT WAS RESIDUAL FUEL. HE THEN MOTORED THE ENGINE AND THE SMOKE TURNED BLACK. HE CALLED SDR C2XA09CL057Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR CA090429002Turbine Blades · failed(CAN) EIR PT6A 2009-027 POWER TURBINE BLADE FAILURE.SDR FSEA 09 0002Turbine · damagedAPPROX 45 MINUTES INTO FLIGHT AT FLT LEVEL 170 WHILE IN CRUISE FLIGHT CONDITIONS. RT ENGINE MADE AN UNUSUAL NOISE, FLAMES WERE SEEN FROM THE EXHAUST DUCTS. CREW INITIATED ENGINE SHUT DOWN PROCEDURES. CREW CONTACTED APPROACH CONTROL DECLARED AN EMERGENCY ANDSDR C2XA09CL055Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR C2XA09CL054Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09CL051Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR C2XA09CL050Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.SDR CA090512006Case · bulged(CAN) NR 1 ENGINE IFSD AND ATB OUT OH HI LO. METAL IN TAIL PIPE AND BULGED HP T CASE, INDICATIVE OF A 1ST STAGE HPT BLADE FAILURE. THE ENGINE HAD 3480 CYCLES SINCE REPAIR. ENGINE INDUCTED AT MFG FOR REPAIR. FURTHER DETAIL WILL BE SUBMITTED UPON DISSASSEMBLY OFSDR C2XA09CL049Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR CA090423010Turbine Blades · failed(CAN) EIR PT6A 2009-08 CT BLADE FAILURE.SDR CA090421001Bearing · seized(CAN) ETR PW100-490 HP ROTOR LOCK UP.SDR C2XA09CL047Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.
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