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.

SDR DHLA200800082Compressor · stalledENG FAIL LIGHT/AUTO PACK TRIP LIGHT FAILED AS THRUST APPLIED FOR T/O. RAN APPROPRIATE PROCEDURE IN AOM. CONTACTED MX AND DISPATCH. ALL INDICATIONS NORMAL AFTER PROCEDURE, APPARENT COMPRESSOR STALL AS THRUST APPLIED. NOTE, CREW REPORTED HEAVY CROSSWINDS DURJul 20, 2008 · N781DH · Boeing 727227SDR SWIA200819884Pad · wornNR 2 ENGINE SHUTDOWN DUE TO HIGH VIBRATION LEVELS ON CLIMBOUT. (FLIGHT NR 6083) REPLACED BLADE WEAR PADS ON THE NR 12 AND NR 24 BLADES. PERFORMED FAN BLADE LUBE AND FAN TRIM BALANCE IAW MANUAL 72-00-00. VIB CHECK GOOD. PN: 4114T15P02 S/N OFF: IHI2887R PN: 4Jul 20, 2008 · N718SK · Cndair CL6002C10SDR CA080724003Bearing · spalled(CAN) SN OF THE PART IS MS030633106124 WAS UNABLE TO PUT THIS INTO SN FIELD. A/C WAS DOWN FOR A ROUTINE OIL SAMPLE. AT THIS TIME THE OIL SAMPLE WAS NOTED TO HAVE A UNUSUAL AMOUNT OF METAL IN THE OIL SAMPLE. THE ENGINE SHOP WAS INFORMED TO HAVE A LOOK AT THE MJul 17, 2008 · Swrngn SA227ACSDR USA2008F00008Fan · out of balancePHL - FLT 722 EN ROUTE (PHL TO DUB). DURING CLIMBOUT FROM PHL THE RT ENGINE INDICATED VIBRATION OF 2.5 WITH SPIKES UP TO 2.8. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A FAN TRIM BALANCE. VIBRATION LEVELS WITHIJul 17, 2008 · N942UW · Boeing 7572B7SDR 2008UALA03852Compressor · damagedNR 2 COMPRESSOR STALL. RTFL. TWO LPT 4TH STAGE BLADES WERE FOUND TO HAVE FRACTURE ABOUT .5 INCHES FROM BLADE PLATFORM. CHANGED ENGINE. Jul 13, 2008 · N338UA · Boeing 737322SDR 2008FA0000491Blade · departedDURING ROUTINE INSP, FOUND DAMAGE TO THE 1ST STAGE STATOR ASSY, UPON FURTHER INSPECTION, FOUND 1 BLADE HAD FAILED AND DEPART THE LP ROTOR ASSY CAUSING DAMAGE TO THE REST OF THE ENGINE DOWN STREAM. (K)Jul 9, 2008 · N678RF · Cessna 525SDR CA080707009Diffuser · cracked(CAN) DURING MAINT FOR REPLACEMENT OF THE T2 BLADES AND WHEEL, AFTER REMOVING OUTER CASING OF THE M03 THE OUTSIDE SURFACE OF THE DIFFUSER WAS FOUND CRACKED FROM ONE SIDE TO THE OTHER. A SERVICEABLE M03 WAS INSTALLED AND THE HELICOPTER WAS RETURN TO SERVICE. DJul 3, 2008 · Aerosp AS355*SDR 2008UALA03670Blade · damagedENGINE EGT WENT UP RAPIDLY, ENGINE SHUT DOWN. RTFL. ENGINE WAS REPLACED AT LAX PRIOR TO FURTHER FLIGHT. SHOP TEARDOWN REVEALED THAT FIVE HP COMPRESSOR STAGE-6 BLADES HAD LEADING EDGE FOD. ONE ADDITIONAL STAGE-6 BLADE HAD A SMALL 'SHARK BITE' FROM ITS TRAILINJul 2, 2008 · N128UA · Boeing 747422SDR CA080711006Blades · damaged(CAN) DURING CRUISE AT FL200, THE PILOT NOTED THE ENGINE TEMPERATURE RAPIDLY RAISING TO 850°C WITH POWER TURBINE SPEED DECREASING. HE ELECTED TO SHUT THE ENGINE DOWN AND PERFORMED A SUCCESSFUL DEAD STICK LANDING. POST FLIGHT ENGINE EXAMINATION REVEALED HEAVY Jul 1, 2008 · Pilats PC12SDR 2008UALA03649Blades · damagedRIGHT ENGINE, BLADE 10 IS 'TORN' AT END. BADLY DAMAGED. *S/D* UNKNOWN FOD DAMAGE. REPLACED NR 2 ENG 1ST STAGE FAN BLADES 10 AND 28, ACCOMPLISHED ENG RUNS, SATISFACTORY.Jun 29, 2008 · N544UA · Boeing 757222SDR AWH2008F00000Blades · damagedAT ABOUT 2800 FT, THE PILOT REPORTED A LOUD BANG FROM ENGINE COMPARTMENT AND SUBSEQUENT ENGINE POWER LOSS. AN EMERGENCY WAS DECLARED, PILOT LANDED SAFELY. POST INCIDENT INSP REVEALED DAMAGE TO COMPRESSOR TURBINE BLADES, COMPRESSOR TURBINE VANE RING., POWER TURJun 25, 2008 · N984FE · Cessna 208BSDR CA080624001Compressor · failed(CAN) EIR PT6A 2008-040 OVER TEMPERATURE EVENT OCCURRED AS A RESULT OF COMPRESSOR FAILURE DUE TO LOSS OF STACK RIGIDITY, WHICH RESULTED FROM A LOSS OF STRETCH ON THE COMPRESSOR TIE RODS (P/N 3019371). COMPRESSOR SELF-DESTRUCTED. TIE RODS WERE INSTALLED "NEW" AJun 24, 2008SDR 2008UALA03581Compressor · stalledLEFT ENGINE COMPRESSOR STALL WHEN THROTTLES ADVANCED. ALSO OCCURRED DURING REVERSER OPERATION. UNABLE TO FIND ANY DAMAGE TO ACCOUNT FOR THE REPORTED STALL. ADDITIONALLY, NO SURGE FLAG WAS SET. BECAUSE OF REPEATED POWERPLANT INTERFACE MANAGEMENT UNIT (PIMU) Jun 24, 2008 · N648UA · Boeing 767322SDR SWAA083538Compressor · stalledCOMPRESSOR STALL ON NR 1 ENGINE, FLIGHT CREW REPORTED VIBRATION FOR THREE SECONDS AFTER STALL. REMOVED AND REPLACED NR 1 ENGINE PER MT.Jun 24, 2008 · N794SW · Boeing 7377H4SDR Q2S2008F00001Compressor · stalledWHILE THROTTLING ENGINE TO TAKEOFF POWER, ENGINE NR 1 HAD MULTIPLE COMPRESSOR STALLS. TAKEOFF POWER WAS 1.53, COMPRESSOR STALLS STARTED WHEN POWER WAS APPROACHING 1.35. AIRCRAFT RETURNED TO BLOCKS. (K)Jun 21, 2008 · N749SA · Boeing 747300SDR S9B2008F00001Compressor · noisyUNUSUAL NOISE NOTED IN COMPRESSOR SECTION NR 2 ENGINE, UPON START UP, REMOVED ENGINE FROM SERVICE WILL CLOSE SDR WHEN SOURCE OF NOISE IS FOUND AND CORRECTED. (K)Jun 20, 2008 · N562CP · Dhav DHC6300SDR SWAA083405Compressor · stalledDIVERSION/DECLARED EMERGENCY, CLIMBING THROUGH 3000' AGL NR 1 ENGINE COMPRESSOR STALLED, VIBRATION OCCURRED, ENGINE FLUCTUATED. R&R NR 1 ENGINE PER MT.Jun 18, 2008 · N735SA · Boeing 7377H4SDR AALA200801582Compressor · stalledDFW INFLIGHT T1413/11JUN. CREW REPORTED NR TWO ENGINE COMPRESSOR STALL ON CLIMB. CREW REDUCED POWER TO IDLE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NR TWO ENGINE ON 11JUN AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)Jun 11, 2008 · N7519A · Doug DC982SDR 2008FA0000441Bearing · failedPILOT REPORTED ENGINE CHIP LIGHT PRECAUTIONARY LANDING MADE TO INVESTIGATE. A CONSIDERABLE AMOUNT OF FERROUS MATERIAL WAS ON THE TOP AND BOTTOM CHIP DETECTORS. NO PENALTY RUNS WERE PERFORMED. AIRCRAFT WAS PLACED ONTO A TRAILER AND MOVED BACK TO BASE WHERE THEJun 4, 2008 · N3WV · Bell 407SDR C8GA20080016Compressor · stalledFLT 0001 FROM MIA-PTY. DURING APPROACH TO PTY THE NR 3 ENG COMPRESSOR STALLED AND ENG FLAMED OUT. THE ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED N1 UNMOVEABLE. REMOVED AND REPLACED THE NR 3 ENGINE. OPS AND LEAK CHECKS GOOD. NO OTHER DJun 3, 2008 · N89427 · Boeing 727227SDR AALA200801435Blade · failedORD INFLIGHT T780/30MAY. NR ONE ENGINE COMPRESSOR STALL DURING TAKEOFF POWER. CREW HEARD TWO LOUD REPORTS AND FELT AIRCRAFT VIBRATE. CABIN CREW AND PASSENGERS REPORTED BURST OF FLAME. ALL INDICATIONS NORMAL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. NMay 30, 2008 · N637AM · Boeing 757223SDR AALA200801433Blades · bird ingestionDFW INFLIGHT T2020/29MAY. FLIGHT ATTENDANTS REPORTED ENGINE VIBRATIONS IN AFT CABIN. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. VISUAL INSPECTION REVEALED BIRD INGESTION TO NR ONE ENGINE. REPLACED THREE PAIR FAN BLADES. SYSTEM GROUND CHECKED NORMAL OPERMay 29, 2008 · N432AA · Doug DC982SDR USAA920081146Compressor · stalledFLT NR 732 SFO-CLT - EMERGENCY LANDING, LEAVING CRUISE, NR 1 ENGINE HAD POSSIBLE COMPRESSOR STALL OR OTHER VIBRATION. COULD NOT MAINTAIN POWER. OPERATED AT REDUCED THRUST WITH NO INDICATION OF VIBRATION. MAINTENANCE FOUND THE NR 1 ENGINE BEYOND LIMITS DURINMay 26, 2008 · N173US · Airbus A321211SDR AALA200801371Blades · damagedABQ INFLIGHT T526/22MAY. NR ONE ENGINE EXPERIENCED BIRD STRIKE ON TAKEOFF. RETURNED TO ABQ AND LANDED WITHOUT INCIDENT. REPLACED THREE PAIRS OF BLADES. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)May 22, 2008 · N446AA · Doug DC982SDR CA080527002Stator · missing(CAN) COMPRESSOR ASSY WAS REMOVED FOR O/H, AT WHICH TIME IT WAS NOTED THE 6TH STAGE STATOR BAND WAS MISSING ONE BLADE, WITH IMPACT DAMAGE NOTED ON OTHER BLADES ALSO IN THE 6TH BAND. NO DAMAGE NOTED FWD OF 6 TH STAGE. BURNER CAN REMOVED AND TURBINE INSPECTED FOMay 21, 2008 · Bell 206BSDR 2008UALA02922Stator · crackedNR 1 ENG FOUND 1EA 9TH STG COMPRESSOR VANE CRACKED COMPLETELY THRU VIEWED FROM CONVEX SIDE. PER THE RECOMMENDATIONS OF MANUFACTURER ALL OPERATORS WIRE PW4000/72-35-25/CTS:ERC:08-5-08-1, PERFORMED A BORESCOPE INSPECTION OF THE SUBJECT ENGINE TO CHECK FOR HP COMay 20, 2008 · N229UA · Boeing 777222SDR ASAA0852978Compressor · dirtyGE REMOTE DIAGNOSTICS NR 2 ENGINE TREND DATA CONTINUES TO SHOW A GREATER THAN NORMAL EGT MARGIN LOSS. ACCOMPLISH NR 2 ENGINE SINGLE ENGINE COMPRESSOR CLEANING IAW AMM SUPPLEMEMT 72-00-00 P710. ACCOMPLISHED COMPRESSOR WASH ON NR 2 ENG REF MM SUPP 72-00-00 PGMay 16, 2008 · N570AS · Boeing 737890SDR HALA0800578Blades · damagedATB: FL 350 SMOOTH AIR LT ENGINE EXPERIENCED LOUD BANG, MODERATE VIBRATION AND LOUD GRINDING SOUNDS. SHUT DOWN ENGINE AND RETURNED TO OGG. INITIAL FINDINGS DURING LT ENG HPC BORESCOPE. FOUND 5TH AND 6TH STAGE COMPRESSOR BLADES AND STATOR DAMAGED. LT ENGINMay 14, 2008 · N591HA · Boeing 76733ASDR 2008UALA02705Blade · failedNR 2 ENGINE STALL. AMBER DECLARED, FLIGHT DIVERTED. ENGINE REPLACED. FOUND HPC 6TH STAGE BLADE FAILURE.May 11, 2008 · N441UA · Airbus A320232SDR UIEA200800182Fan Blade · bird ingestionBIRD STRIKE AT TAKEOFF TO FUSELAGE AND ENGINE NR 1 FAN BLADES. ACCOMPLISHED BIRD STRIKE INSPECTION FOR FUSELAGE AND NR 1 ENGINE AND OVERWEIGHT LANDING CHECKS AS PER IAW 05-51-14, 05-51-39 AND 72-00-00 FOR FAN BLADES CHANGED AND ENGINE INSPECTION. REPLACED NRMay 6, 2008 · N506MC · Boeing 7472D3BSDR AALA200801178Blade · damagedDFW INFLIGHT T2452/02MAY - NUMBER ONE ENGINE COMPRESSOR STALL AND VIBRATIONS ON TAKEOFF AND CLIMB. REDUCED ENGINE TO IDLE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND ONE FAN BLADE DAMAGED. REPLACED TWO SETS OF FAN BLADES. SYSTEM GROUND CHECKED NMay 2, 2008 · N406A · Doug DC982SDR COMA0870017Fan Blade · stuckFLIGHT 5311 - EN ROUTE FROM CVG TO COS, N1 VIBE ON NR 1 ENGINE WENT TO 1.9. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO MCI AND LANDED SAFELY. REMOVED AND REPLACED ALL FAN BLADES ON NR 1 ENGINE.Apr 28, 2008 · N398CA · Cndair CL6002C10SDR 2008UALA02373Blades · damagedNR 1 ENG HPC STG 7 HAS SEVERAL DAMAGED BLADES BEYOND LIMITS AND ARE NOT BLENDABLE. ALSO, HPC STAGE 12 HAS 1 BLADE WITH CRACK BEYOND LIMITS. ENGINE CONDITION MONITORING (ECM) DETECTED AN ENGINE GASPATH PARAMETER SHIFT. SUBSEQUENT BORESCOPE INSPECTION (BSI) FApr 23, 2008 · N214UA · Boeing 777222SDR 2008UALA02199Fan Blade · damagedNR 2 ENGINE SEVERAL FAN BLADES DAMAGED NR 11, 25 AND 30. LEADING EDGE CLOSE TO TIP.Apr 16, 2008 · N653UA · Boeing 767322SDR 08FDEA01419Compressor · stalledNR 3 ENGINE COMPRESSOR STALL IN CRUISE SHAKING. AIRCRAFT FLUCTUATION OF N1,-THROTTLE AT IDLE N137 PERCENT EGT 600-700 DEG INFLIGHT ENGINE SHUTDOWN, RESIDUAL FUEL FLOW AFTER SHUTDOWN 800 LBS FF. REMOVED AND REPLACED THE #3 ENGINE. PERFORMED IDLE AND FLT IDLEApr 15, 2008 · N315FE · Doug DC1030FSDR CA080414005Duct · damagedMETAL SWARF FOUND INSIDE COOLING PASSAGES OF DUCT ASSY.Apr 11, 2008SDR VNAA0804007Fan Blade · stuckCREW REPORTED A LEFT HAND ENGINE VIBRATION MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT HAND ENGINE FAN BLADES. MAINTENANCE FOUND AND UNSTUCK A FAN BLADE IN ACCORDANCE WITH THE GE CF34-8C MApr 9, 2008 · N716PS · Cndair CL6002C10SDR 2008UALA02050Blade · crackedCRACK FOUND IN THE 5TH STAGE COMPRESSOR BLADE ROOT OF THE NR 1 ENGINE. REPLACED ENGINE.Apr 9, 2008 · N641UA · Boeing 767322SDR DLM88080565Compressor · stalledPOSSIBLE COMPRESSOR STALL LT ENGINE ON TAKEOFF ROLL, REJECTED TAKEOFF ROLL AT 75 KTS. MTC IN PROGRESS REPLACING LT ENGINE.Apr 7, 2008 · N922DL · Doug MD88SDR UIEA200800112Fan Blade · dentedNR 4 ENGINE 2 EACH FAN BLADES WITH DAMAGE WITH DENT. DYE PENETRANT CHECK OF BLADES FOUND DENTS WITHIN LIMITS OF TASK 72-31-02-206-001-J00. NO CRACKS FOUND.Apr 6, 2008 · N492MC · Boeing 74747UFSDR 2008UALA01935Compressor · malfunctionedR ENG HPSOV EICAS. FOUND HIGH PRESSURE SHUT OFF VALVE AND HIGH PRESSURE CONTROLLER TO BE FAULTY. REPLACED NR 2 ENG HPSOV PER MM 36- 11-07 PG 401, NO HELP. BITE CHECK AIR SUPPLY CONTROLLER. REPLACED NR 2 ENG HPC PER MM 36-11-08. RAN ENGINES PER JRH. NR 2 BLApr 5, 2008 · N654UA · Boeing 767322SDR YTRR040408001Compressor Wheel · crackedON DEPARTURE PILOT EXPERIENCED A DECELERATION OF THE ENGINE AND LOSS OF POWER. ON INSPECTION FOUND THE NR 2-3 COMPRESSOR WHEEL HAD SHED A BLADE WHICH SUBSEQUENTLY DESTROYED THE REMAINING COMPRESSOR WHEELS. NO FOD DAMAGE NOTED AS NR 1 COMPRESSOR WHEEL STILL IN Apr 4, 2008 · N18HT · Bell 206B3SDR DL764080554Blade · brokenAFTER START OF THE RIGHT ENGINE NOTICED TO HAVE N2 VIBS OF 5.0 AND CAN BE FELT. UNUSUAL SOUND ALSO. RETURNED TO GATE. NO METAL IN TAIL PIPE. CHIP DETECTORS CLEAN BUT ENG HAS RUMBLE SOUND WHEN RUNNING. BOROSCOPE REVEALED 1ST HPC BLADE BROKEN OFF. ENGINE Apr 4, 2008 · N844MH · Boeing 767432ERSDR HALA0800491Fan Blade · damagedETOPS SIGNIFICANT SYSTEM, LT ENGINE FAN BLADE HAS NICK ON NR 22 BLADE. BLENDED FAN BLADE PER AMM TASK 72-31-02. EDDY CURRENT. NO IND NOTED. OK TO CONTINUE. FAN BLADE WITHIN LIMITS OF AMM 72-31-02.Apr 3, 2008 · N585HA · Boeing 7673G5SDR HALA0800477Fan Blade · damagedETOPS SIGNIFICANT SYSTEM, LT ENG FAN BLADE NR 25 HAS NICK. REPAIRED PER AMM TASK 72-31-02. EDDY CURRENT GOOD. NO CRACKS IND NOTED.Mar 31, 2008 · N589HA · Boeing 76733ASDR HALA0800476Blade · damagedETOPS SIGNIFICNAT SYSTEM, LT ENG FAN BLADE HAS NICK NR 36. REPAIRED PER AMM TASK 72-31-02. EDDY CURRENT GOOD. NO CRACKS IND NOTED.Mar 31, 2008 · N589HA · Boeing 76733ASDR HALA0800474Blade · damagedETOPS SIGNIFICANT SYSTEM, LT ENG FAN BLADE HAS NICK ON NR 18. REPAIRED PER AMM 72-31-02. EDDY CURRENT CHECKED. NO CRACKS IND NOTED.Mar 31, 2008 · N589HA · Boeing 76733ASDR HALA0800473Blade · damagedETOPS SIGNIFICANT SYSTEM, RT ENG FAN BLADE 22 HAS NICK. REPAIRED PER AMM TASK 72-31-02. EDDY CURRENT GOOD. NO CRACKS IND NOTED.Mar 31, 2008 · N589HA · Boeing 76733ASDR HALA0800472Blade · damagedETOPS SIGNIFICANT SYSTEM, RT ENG FAN BLADE 25 HAS NICK. REPAIRED PER AMM TSK 72-31-02, EDDY CURRENT GOOD. EDDY CURRENT CHECKED. NO CRACKS IND NOTED.Mar 31, 2008 · N589HA · Boeing 76733ASDR CA080409006Blades · failedON APPROACH, THE CREW NOTED ENGINE TEMP AT APPROX 900 DEGREES FOLLOWED BY SOME NOISES. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED. INITIAL INVESTIGATION REVEALED LOSS OF COMPRESSOR TURBINE BLADE MATERIAL AND SHROUD SEGMENT MATERIAL, THE ENGINE WAS SENT Mar 30, 2008 · Bell 412
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