JASC 7230
Service difficulty reports · 5,066
Reports filed under 7230 · Turbine Engine Compressor 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 = '7230' 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 = '7230' 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 2007UALA02002Compressor · stalledABORTED TAKEOFF DUE TO NR 2 ENGINE COMPRESSOR STALL. [08-08-07] ACFT NR 3 ENG FERRIED TO SFO FOR ENGINE CHANGE. ENGINE REPLACED AT SFO ON 06/15/07. SHOP TEARDOWN FOUND ONE 6TH STAGE VSV VANE ARM BROKEN OFF AT THE "CLAW" TO THE ARM RADIUS AT THE 6:00 POSSDR NOCA10907Compressor · stalledLEFT ENGINE HAD TWO COMPRESSOR STALLS PASSING THROUGH 1500 FEET ON DEPT WHILE ADDING POWER ON THE LT ENGINE. MAINTENANCE WILL ACCOMPLISH A BITE ON THE BPCU AND TPU AND GET FAULT CODES, WILL FOLLOW FIM REF 71-06-00 FIG 105A FOR ENGINE SURGE (STALL) IN FLIGHT DSDR DL76L070604Compressor · damagedSET UP TO PERFORM BORO INSP OF THE LEFT ENG HPC 5TH-15TH STAGES PER AMM 7200-00-206-344-NOO. THIS DUE TO ENG TREND ALERT AND PREV SURGE REPORT. FOUND DAMAGE TO THE 7TH STAGE HPC AND AFT. REPLACED LT ENG.SDR TSAA0772028Compressor Wheel · failedNON-ETOPS CARGO FLIGHT 956 HNL-ITO - DURING CLIMB AT 24500 FEET, CREW HEARD WHAT SOUNDED LIKE A COMPRESSOR STALL FROM THE NR 1 ENGINE. CREW REDUCED POWER SETTINGS AND ALL ENGINE PARAMETERS WERE NORMAL. CREW LANDED IN ITO WITHOUT FURTHER INCIDENT. MAINTENANCSDR AALA20070937Blade · failedORD INFLIGHT T366/24MAY - RETURNED ORD DUE TO CREW REPORTING LOUD BANG DURING CLIMB AND RIGHT ENGINE GAS TEMPERATURE OVER 800C. LANDED ORD WITHOUT INCIDENT. SINGLE ENGINE TIME 13 MINUTES. REPLACED NUMBER TWO ENGINE ON 24 MAY AT ORD DUE TO COMPRESSOR BLADE SDR AALA20070873Compressor · stalledDFW INFLIGHT T688/17MAY - RIGHT ENGINE VIBRATION AND COMPRESSOR STALL DURING CLIMB. ENGINE GAS TEMPERATURE PEAK 1018. ENGINE SHUT DOWN BY CREW IN FLIGHT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. REPLACED RISDR 2007UALA01436Blades · failedRTFL WITH NR 1 ENGINE SHUT DOWN. LOUD BAND HEARD ON CLIMBOUT. REPLACED NR 1 ENGINE. [06-26-07] ENGINE INGESTED COWLING ACOUSTIC PANELS DURING CLIMBOUT CAUSING DAMAGE TO A STAGE 3 COMPRESSOR BLADE.SDR ARWA20070501Blades · damagedJUST PRIOR TO ROTATION, DURING TAKEOFF ROLL, A/C SUDDENDLY BEGAN TO VIBRATE, AND DURING INITIAL CLIMB VIBRATION WAS DETERMINED TO BE COMING FROM NR 1 ENGINE. ENGINE WAS SHUTDOWN. [SUP 06-01-07] PERFORMED FULL BOROSCOPE INSPECTION AND FOUND COMPRESSOR SECTIOSDR DL777070473Blades · damagedON TAKE OFF OUT OF NRT THE RIGHT EXPERIENCED 4 TO 6 STALLS WITH FLAMES FROM TAILPIPE. A/C RTB TO NRT. ENGINE WAS NOT SHUTDOWN. FURTHER INSPECTION REVEALED METAL ON THE MCD AND IN THE TAILPIPE. MAX TGT OF 946 AND 940 FOR 8 SECONDS. PER AMM ENGINE CHANGE RESDR ZZDA070427154Compressor · stalledCOMPRESSOR STALL NR 2 AFTER T/O. HAD ROLLBACK TO IDLE. FOR VIBRATION FOR 3 TO 5 MIN RAN CHECK LIST- ENGINE CAME BACK WE RETURNED FOR LANDING. NO TGT EXCEEDED. REPLACED NR 2 ENG A/C OK FOR SERVICESDR CA070710004Guide Vane · failed(CAN) DURING FLIGHT, THE TURBINE TEMPERATURE ROSE SUDDENLY FROM 738 TO 785 DEGREES CELSIUS. A BORESCOPE INSPECTION REVEALED DAMAGE TO THE CT GUIDE VANE. THE ENGINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THE HOT SECTION WAS REMOVED FROM THE ENGINE ASDR 2007FA0000400Bearing · failedDURING FLIGHT THE UPPER CHIP PULL ILLUMINATED, IT WAS CLEANED IAW MM AND RETURNED TO SERVICE. A COUPLE OF HOURS LATER, A SECOND LIGHT ILLUMINATED. FOUND LOTS OF FINE CHIPS. REPLACED ENGINE. FOUND NR 1 BEARING BAD. (K)SDR CA070424005Compressor Wheel · making metal(CAN) OPERATOR REPORTED THAT WHEN THE ENGINE WAS STARTED, THE PROPELLER DID NOT ROTATE. AFTER SHUTDOWN, THE ENGINE AND PROP COULD BE ROTATED BY HAND. HOWEVER, SEVERAL SMALL PIECES OF METALLIC DEBRIS WAS REMOVED FROM THE EXHAUST AREA. DISASSEMBLY OF THE ENGINESDR CA070424007Blade · failed(CAN) DURING TAKEOFF ROLL AT 80KTS, THE TOWER ADVISED THE CREW THAT FLAMES WERE VISIBLE OUT OF ONE OF THE ENGINES. THE CREW REJECTED THE TAKEOFF AND ENGINES WERE SHUTDOWN. THE AIRCRAFT WAS TOWED BACK TO THE RAMP. MAINTENANCE INSPECTED THE ENGINES AND FOUND NSDR AALA20070725Blade · damagedEWR INFLIGHT T1179/21APR DURING CLIMB LEFT ENGINE COMPRESSOR STALLED AT 600 FEET ABOVE GROUND LEVEL. POSSIBLE BIRD STRIKE. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. ENGINE SHUT DOWN FOR TAXI. REPLACED NUMBER ONE ENGINE ON 20 APR 2007 AT EWR DUE TO BLADESDR 2007UALA01246Compressor · stalledCREW RECEIVED NR 1 ENG STALL ECAM AT FL380 IN LIGHT CHOP & LIGHT MTN WAVE ACTIVITY. LOUD BANG HEARD BY F/A. [06-14-07] REPLACED NR 1 ENGINE DUE TO STALL HISTORY.SDR AALA20070712Compressor · stalledORD INFLIGHT T1877/18APR AFTER TAKE OFF LEFT HAND ENGINE COMPRESSOR STALLED. THROTTLE RETARDED AND INDICATIONS NORMAL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. METAL DEBRIS FOUND IN LEFT HAND ENGINE EXHAUST. REPLACED LEFT HAND ENGINE ON 19 APR 2007 ASDR DHLA200700022Compressor · stalledREJECTED TAKEOFF AT APPROX 20 KNOTS DUE TO AN AUTOPACK TRIP AND AN APPARENT COMPRESSOR STALL.SDR 2007UALA01237Blades · damagedBIRD STRIKE TO NR 1 ENGINE. ACCOMPLISHED BOROSCOPE INSP OF NR 1 ENG HPC 5TH, 6TH, 10TH AND 11TH STG BLADES PER MM 72-00-00. FOUND 1 EA 6TH STG BLADE WITH LARGE TEAR IN AREA C OF L/E BEYOND FLYBACK LIMITS, 18 EA 10TH STG BLADES WITH DAMAGE BEYOND LIMITS IN ARSDR DL76G070324Fan Blade · bentBIRD STRIKE ON TAKEOFF 700 FT RT ENG VIBS. INSPECT RT ENGINE PER FIM 71-05-00 FIG 124. 5 FAN BLADES. DAMAGED BEYOND LIMITS. BORESCOPE HPC OK. REPLACED FAN BLADES SET PER AMM 72-31-02-404-084-H00. REQUIRES VIBRATION SURVEY VIBRATION SURVEY WITH IN LIMITS PSDR CA070419002Blades · departed(CAN) LT ENGINE EXPERIENCED A SUDDEN POWER LOSS ON CLIMB OUT. THE ENGINE WAS SHUTDOWN AND THE A/C RETURNED TO BASE WITHOUT ANY FURTHER INCIDENT. THE POWER SECTION WAS REMOVED FOR INVESTIGATION. THE INVESTIGATION REVEALED THAT PIECES WERE MISSING FROM SEVERALSDR CA070514046Rotor · seized(CAN) DURING CLIMB THE ENGINE EXHIBITED VIBRATION AND SHUTDOWN, UNCOMMANDED. SUBSEQUENT INSPECTION REVEALED HIGH PRESSURE ROTOR SEIZURE AND METAL CONTAMINATION IN THE TURBO MACHINE OIL SYSTEM. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTASDR HALA0700168Fan Blade · damagedNR 1 ENG 1ST STAGE FAN BLADE NR 8 HAS A NICK IN THE LEADING EDGE 17" FROM BLADE TIP 1/16" DP BY 1/8" WD. REPAIRED NR 8 FIRST STAGE FAN BLADE BY BLENDING PERAMM 72-31-02.SDR 2007UALA01066Compressor · surgesENGINE NR 1 AUDIBLE COMPRESSOR SURGE. [SUP 05-18-07] DETERMINED THAT VARIABLE STATOR VANE ACTUATOR WAS MALFUNCTIONING AND WAS REPLACED. FURTHER TEARDOWN FOUND EXTENSIVE FUEL LACQUERING THROUGHOUT ACTUATOR, WHICH INTERFERED WITH PROPER OPERATION.SDR DHLA200700023Compressor · stalledDEPARTING RNWY 22R AT ILN, NR 2 ENG COMPRESSOR STALL OCCURRED AT AN EPR OF 2.05. WIND WERE 290DEG AT 14 GUSTING TO 26 (70DEG X-WIND) IAS -0, OAT - 13DEG, PA - 1077 A/C GW 178.8. FOR INFORMATION ONLY. INSPECTED INLET AND EXHAUST OF NR 2 ENG PER AOM CHPT 1.8 PSDR UE5R1Blade · crackedCOMPRESSOR TURBINE DISC BLADE FAILURE. SINGLE BLADE IN COMPRESSOR TURBINE DISC CRACKED IN FUR TREE AREA OF BLADE. CAUSED MISALIGNMENT OF CT BLADE AND SUBSEQUENT RUB ON SHROUD SEGMENTS. THE CRACK IN FIR TREE WAS NOT VISIBLE WITH ENGINE SPLIT IF PERFORMING A ROUSDR DLM90070287Engine · fodAT FL310, LEFT ENGINE SHUT DOWN IN FLT HEARD BANG AND FELT SHUTTER N1 RAPIDLY DECREASED, EGT INCREASED TO 730 OIL PRESS WENT TO -0-. C/W BORESCOPE INSP FOUND FOD BEYOND M/M LIMITS. DAMAGE STA AT 3RD STG HPC. STG 2.5 LPC BLADES ARE CLEAN ENG CHANGE REQUIRED. SDR 4531504022007Blade · bentRT ENGINE INGESTED A BIRD ON TAKEOFF. FAN BLADE BENT. TAKE-OFF ABORTED. AIRCRAFT DID NOT ROTATE. CREW SAYS BIRD APPEARED TO BE A SEAGULL.SDR CA070514040Fan Blade · fractured(CAN) DURING CRUISE, THE ENGINE EMITTED A LOUD NOISE AND HIGH VIBRATIONS AND SHUTDOWN. SUBSEQUENT INSPECTION REVEALED A FRACTURED LOW PRESSURE COMPRESSOR FAN BLADE, DAMAGE TO THE ENGINE NACELLE INLET, MISSING ENGINES COWLS AND ASSOCIATED AIRFRAME IMPACT DAMAGSDR 6017803312007Blade · separatedLOUD BANG ON LT ENGINE AT FL 410 FOLLOWED BY MAJOR VIBRATION, SHUT ENGINE DOWN IN FLIGHT. PRELIMINARY INVESTIGATION: 1ST STAGE COMPRESSOR BLADE LET LOOSE. BOUNCED AROUND INSIDE CONTAINMENT RING BUT MADE ITS WAY FORWARD WHERE IT PENETRATED THROUGH THE INLET. TSDR HALA0700133Blade · damagedETOPS SIGNIFICANT SYSTEM, NR 1 ENG BLADE 5 FOD. BLENDED NR 1 ENG NR 5 BLADE PER AMM 72-31-02. NO CRACKS NOTED. OK FOR SERVICE.SDR HALA0700132Fan Blade · dentedETOPS SIGNIFICANT SYSTEM, DURING L ENG INSPECTION FOUND DENT DAMAGE APPROX .030-.035 INCH NBR 4 FAN BLADE, 1 INCH FROM TIP AREA A. PERFORMED BLENDING PER AMM 72-31-02-308-003-N00 AND OK FOR SERVICE.SDR 2007UALA00856Compressor · stalledNR 2 ENGINE HAD A COMPRESSOR STALL WITH AN AUDIBLE BANG. [SUP 06-01-07] INSPECTED ENGINE PER AMM TASK FOR STALL CONDITION AND FOUND NO DEFECTS. LUBED VARIABLE STATOR VALVE MECHANISM AND PERFORMED IDLE RUN CHECK. NO FURTHER IRREGULARITIES NOTED.SDR AALA20070514Compressor · stalledDURING CLIMB, AIRCRAFT EXERIENCED LOUD BANK AND FIVE DEGREES OF YAW AT 2600 FEET. CREW RETURNED TO MSP AND LANDED WITHOUT INCIDENT. CREW REPORTED NUMBER TWO ENGINE GIVING LITTLE MORE THAN IDLE THRUST ON SHORT FINAL. REPLACED NUMBER TWO ENGINE ON 20 MARCH ATSDR CA070514017Stator · damaged(CAN) THE ENGINE EXPERIENCED COMPRESSOR STALLS ON TAKEOFF ROLL AND THE TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED A DAMAGED SECOND STAGE COMPRESSOR STATOR. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514017)SDR CA070319005Impeller · fractured(CAN) ENGINE WAS REMOVED DUE TO NOT MAKING TARGET TAKEOFF TORQUE. UPON DISASSEMBLY THE 2ND STAGE COMPRESSOR IMPELLER FAILED AND HAS EXPERIENCED A FATIGUE TYPE FAILURE. THE PRESENT TIME ON THE IMPELLER IS 20,650.2 HOURS AND 28,175 CYCLES. A LARGE PIECE OF THESDR MASA200700144Fan · damagedASH 7302 IAD - BURNING ODOR IN CABIN AFTER BIRD STRIKE. MX COMPLIED WITH REPAIR TO THE FAN CASE AND COWLING.SDR COMA0760241Compressor · contaminatedFLIGHT 5307 - DURING CLIMBOUT OF TUL EVIDENCE OF SMOKE IN CABIN AND COCKPIT, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. PERFORMED ENGINE RUNS TO REMOVE RESIDUAL COMPRESSOR WASH FLUID.SDR S9BA00207Compressor Wheel · damagedLT ENGINE VIBRATION OCCURRED WHEN MOTORED AFTER FUEL LINE REPLACEMENT. REMOVED AND HAD C/T DISK ASSEMBLY OVERHAULED INSTALLED SAME ASSEMBLY. (SULFIDATION)SDR CA070312002Blades · damaged(CAN) ON TAKEOFF AT 500 AGL, 3 TO 4 STALLS ON NR 2 ENGINE, LOUD POPPING NOISE, ATC SAW FLAMES COMING OUT. AIRCRAFT RETURNED TO DEPARTURE, ENGINE BOROSCOPE FOUND DAMAGED COMPRESSOR BLADES FROM STAGE 6 TO STAGE 9. ENGINE REMOVED FROM AIRCRAFT AND SENT TO SHOP FOSDR 2007UALA00678Compressor · stalledRTFL DUE TO NR 2 ENGINE COMPRESSOR STALLS. [SUP 05-18-07] BOROSCOPE NR 2 ENG SERIAL NR 727193, FOUND SEVERE DAMAGES ON COMPRESSOR STAGES 16 & 17 THROUGH AP8. FOUND RT ENGINE BLADE 1 & 2 GOUGES IN LEFT EDGES. BLADES 1 AND 2 OK. REPLACEMENT OF NR 2 ENG NR 4SDR 2007UALA00701Compressor · stalledON DESCENT NR 1 ENG COMPRESSOR STALLED WITH AUDIBLE BANGS. TWO BANGS WHEN THROTTLE RETARDED AT FL370, ENG BANGED LIGHTLY DOWN TO FL 150 AND BETWEEN FL 150-100 VIBRATION AND NOISE INCREASED. [07-03-07] FOUND MINOR DAMAGE TO THE 3RD STAGE BLADES AND VANES, WISDR DL764070188Compressor · damagedON DESCENT, RECEIVED A BLEED HPSOV AND N2 VIBS INCREASED TO 5 UNITS. INLET AND EXHAUST OK CHECK CHIP DETECTORS OK RUN ENG AGAIN VIBS RETURNED. BOROSCOPE COMPRESSOR FOUND 6TH STAGE DAMAGE. BORO AND FOUND HPC 6TH AND 7TH STAGE DAMAGE BEYOND MM LIMITS. REMOVESDR CA070514058Compressor · damaged(CAN) DURING CRUISE THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY A REDUCTION IN ALL PARAMERTERS TO ZERO. SUBSEQUENT INSPECTION REVEALED COMPRESSOR AND POWER TURBINE DAMAGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20SDR 2007UALA00611Check Valve · malfunctionedLANDED UNDER AMBER ALERT DUE TO NR 1 ENGINE AT FLIGHT IDLE DUE TO COMPRESSOR STALL AND HIGH EXHAUST GAS TEMPERATURE. EMERGENCY EQUIPMENT CALLED AS PRECAUTION. TROUBLESHOOTING IDENTIFIED FAILED 8TH STAGE PNEUMATIC CHECK VALVE. AFTER EXTENSIVE TROUBLESHOOTINSDR DJFA2007024Fan Blade · damagedON A WALK AROUND MX FOUND 2 ENGINE FAN BLADES ON NR 2 ENGINE WITH THE TIPS CURLED. MX REMOVED 4 ENGINE FAN BLADES PN NR 23065323 AND INSTALLED 2 - KITS OF MATCHED PAIRS OF BLADES PN 23066437.SDR AALA20070364Blade · failedDFW INFLIGHT T1511/18FEB - DURING CLIMB, LEFT ENGINE SPOOLED TO IDLE POWER WITH EXCESSIVE VIBRATION AND ENGINE GAS TEMPERATURE AT 800 DEGREES. SHUT DOWN LEFT ENGINE AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT ENGINE DUE TO COMPRESSOR BLADE FAILURE. SYSTSDR CA070220006Actuator · leaking(CAN) AC PERFORMED NORMALLY FOR THE TAKEOFF AND INITIAL CLIMB TO 5000 FEET. APPROX (2) MINUTES INTO THE FLIGHT AFTER CLEARANCE TO 17000 FT WITH CLIMB PWR REAPPLIED TO COMMENCE THE CLIMB, THE RT ENG EXPERIENCED A COMPRESSOR STALL. AFTER (2) OR (3) SURGES THE ENSDR CA070314018Actuator · failed(CAN) ON APPLICATION OF POWER IN CLIMB, THE ENGINE EXPERIENCED A COMPRESSOR STALL ACCOMPANIED BY AN UNCOMMANDED POWER REDUCTION, PARAMETER FLUCTUATIONS AND A FADEC FAULT INDICATION. SUBSEQUENT INVESTIGATION LED TO REPLACEMENT OF THE ENGINE INLET GUIDE VANE ACSDR CA070219001Fan Blade · bent(CAN) FEB 16/07, AIR TURN BACK. THE CREW REPORTED THAT AFTER TAKEOFF A LOUD RUMBLING NOISE WAS HEARD. CREW BELIEVED THAT ICE MAY HAVE BEEN INGESTED INTO THE RT ENGINE DURING LANDING ON THE PREVIOUS LEG INBOUND TO DESTINATION. MAINTENANCE CONFIRMED SEVERAL FAN
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