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 C2XA09CL052Case · crackedDURING COMPLIANCE OF SB AE3007A-72-368 MAINTENANCE FOUND THE NR 2 ENGINE FAN CASE HAD MULTIPLE CRACKS AROUND THE CIRCUMFERENCE OF THE CASE. THE COMPOSITE CONTAINMENT RING WAS ALSO DELAMINATED. THE FAN CASE WAS REPLACED.SDR USAA2009042891000Blade · separatedFLT 500 YYC-PHX - COMPRESSOR STALLS - NR 2 ENGINE EXPERIENCED TWO RAPID COMPRESSOR STALLS CLIMBING THROUGH FL340 IN SMOOTH AIR, VCM. TEMPORARILY LOST POWER. ENGINE QUICKLY SELF RECOVERED. NO LIMITS EXCEEDED. ENGINE CONTINUED NORMAL POWER THEREAFTER. RAN 3SDR CA090421002Blades · damaged(CAN) EIR PT6A 2009-030 FIRST STAGE COMPRESSOR BLADE FAILURE.SDR HALA2009041900157Blade · nickedETOPS SIGNIFICANT SYSTEM, ON NR 2 ENGINE BLADE NR 32, FOUND NICK ON BLADE IN AREA F. BLENDED DAMAGED AREA PER AMM 72-31-02 DAMAGE IN AREA F W/IN LIMITS PER AMM 72-31-02 EDDY CURRENT DAMAGED AREA, NO CRACKS FOUND. OK FOR SERVICE.SDR HALA2009041900156Blade · fodETOPS SIGNIFICANT SYSTEM, ON WALKAROUND FOUND FOD ON BLADE NR 21 ON NR 1 ENG. BLENDED DAMAGED AREA PER AMM 72-31-02 DAMAGE IN AREA B DAMAGE OK PER AMM 72-31-02, NO CRACKS NOTED.SDR UALA2009042001135Compressor · stalledNR 1 ENGINE COMPRESSOR STALL ON ENGINE RUNUP, ENGINE SHUT DOWN, PER CREW. SAMC FLETCH PROG TEXT: - ITEM ROLLED FORWARD. SAMC TEXT: COMPRESSOR STALL AT APPROX 40 PERCENT, SHUTDOWN, PER CREW. INSPECTED ENGINE UNISON RINGS, CHIP DETECTORS AND BOROSCOPED FOR SDR HALA2009041200141Compressor · stalledNR 2 ENGINE COMPRESSOR STALLED DURING TAKEOFF ROLL. TGT OVERTEMP. NO HIGH ENERGY STOP. A/C RETURNED TO GATE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NR 2 ENGINE PER HALM144 AND HALM143. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.SDR HALA2009041100140Fan Blade · nickedETOPS SIGNIFICANT SYSTEM, FOUND NICK ON NR 2 ENGINE 1ST STAGE FAN BLADE. BLENDED AREA, WITHIN LIMITS PER AMM 72-31-02, EDDY CURRENT ACCOMPLISHED.SDR 2009F00026Compressor Wheel · damagedPILOT REPORTED NR 1 ENG LOW WARNING LIGHT AND NR 1 ENG LOW AURAL ACTIVATED WITH CORRESPONDING DECREASE IN ENG SOUND. NR 1 ENG N1 WAS AT 28 PERCENT AND TOT WAS RISING, REACHING APPROX 1000 DEGREES C. PROCEEDED TO PULL NR 1 ENG THROTTLE TO IDLE AND THEN TO OFF. SDR SWAA092297Compressor · stalledIN FLT ENG SHUT DOWN / AIR TURNBACK. NR 1 ENG COMPRESSOR STALL WITH VIBRATION FELT. REMOVED AND REPLACED NR 1 ENG PER MM.SDR ZZDA2009110Compressor · stalledLEFT ENGINE COMPRESSOR STALL. REMOVED AND REPLACED NR 1 ENGINE S/N 13321 WITH ENGINE S/N 13133.SDR 2009FA0000765Bearing · damagedTHE SUBJECT ENGINE WAS REMOVED FOLLOWING A COMMANDED INFLIGHT SHUTDOWN ON APRIL 5TH, 2009. SHUTDOWN DETAILS: AT APPROX 39K, CREW NOTED NR 1 ENGINE THUMP AND VIBRATION, WITH OIL PRESSURE INDICATION IN RED (LOW). CREW PERFORMED ENGINE SHUTDOWN. ENG WAS RETURNSDR WRNA2009002Compressor · stalledSEVERE COMPRESSOR STALLS (2) DURING TAKEOFF AT ABOUT 100 KTS ON NR 2 ENGINE. TAKEOFF WAS REJECTED (ABORTED) AT ABOUT 100KTS, DURING BRAKING ACTION THE TOWER REPORTED FIRE IN NR 2 ENG, FIRE CK LIST WAS PERFORMED, DISCHARGING ONE (1) FIRE BOTTLE. AFTER LEAVINGSDR ASAA0955007Shim · wornNR 1 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES HARDWARE INSPECTION AND FAN LUBE REQUIRED. ACCOMPLISHED FAN BLADE LUBE PER T/C 78472002. FOUND FAN BLADE SHIM COATING WORN. REPLACED 24 EA FAN BLASDR DL764090538Blade · damagedCREW REPORTED LOUD NOISE AND AIRFRAME VIBRATION ASSOCIATED WITH RT ENGINE. DURING T/O SHOWED 4.0 FAN VIBS. FOUND BLADES 11 AND 12 WITH FOD FROM BIRD. REPLACED BLADES 1 12 30 AND 31. BOROSCOPE FOUND HPC STAGE 1 WITH A SHINGLED BLADE LOOSENED SAME PER M/M 72SDR IPXA09555196Compressor · stalledATB - RT ENG COMPRESSOR STALL AT 1000FT ON DEPARTURE. EMERGENCY DECLARED. REMOVED AND REPLACED RT ENGINE PER ENGINEERING REQUEST PER TC 5001. OPS TEST C/W PER TC 5002. SATISFACTORY AMM 71-00-00-5.SDR 2009FA0000251Blades · crackedDURING HOT SECTION INSP, 2 COMPRESSOR TURBINE BLADES, PN 3045741-01, WERE FOUND TO HAVE CRACKS IN THE T/E OF THE BLADE. THESE CRACKS WERE FOUND ABOUT HALF WAY UP THE T/E. ONE CRACK .3750 INCH IN LENGTH. THE OTHER WAS .1875 INCH IN LENGTH. CRACKS WERE FOUND BYSDR CA090326015Duct · cracked(CAN) WHILE ON CLIMB MODE, OBSERVED LT ENGINE OIL PRESS WITH RED INDICATION (8L), OIL TEMP INCREASING FOLLOWED AOM PROCEDURE AND CONTINUED WITH ENGINE SHUTDOWN. ENGINE OIL PRESS. STAYED AT 182P. REMOVED AND REPLACED LT ENGINE. FOUND CRACKED DUCT ON HPC STASDR CA090407013Stator Vane · unserviceable(CAN) DURING COMPRESSOR HALVES INSP, ONE STATOR BLADE OF THE LAST AXIAL COMPRESSOR STAGE WAS TORN AND WAS SIDEWAYS CONTACTING THE ONE NEXT TO IT. THE BLADE WAS ONLY HELD IN PLACE BY 5-10 PERCENT OF THE BLADE ROOT. THIS COULD HAVE CAUSED THE BLADE TO GO THRU THSDR A6WA200940143Fan Blade · damagedON CLIMB, BIRD STRIKE IN RT ENGINE IMMEDIATELY AFTER SMOKE ODOR IN CABIN, RETURNED TO DEPARTURE. LANDED OVERWEIGHT 47,500 IN., RATE OF DESCENT, 300 FT PER MINUTE. REMOVED AND REPLACED 10 FAN BLADES. DAMAGED ONES AND BLADES 180 DEGREE OUT IAW AMM 72-20.SDR UALA2009032400875Guide Vane · leakingOIL ODOR IN CABIN. FOUND THE EXIT GUIDE VANES OIL SPLASHED ALL AROUND THE AREA AND A SMALL PUDDLE RT UNDER THE 6:00 O'CLOCK POS UNDER THE EXIT GUIDE VANES. REPLACED NR 1 ENGINE.SDR CA090401012Compressor Blade · fractured(CAN) DURING T/O ROLL, THE PILOT HEARD A LOUD NOISE AND THE ENGINE VIBRATION WARNING LIGHT CAME ON. AS THE ACFT WAS ALREADY AT V1 SPEED, THE PILOT REDUCED THE POWER AND CONTINUED THE T/O. EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO ORIGIN WHERE A SINGLE ENSDR ASAA0954754Shim · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENG FOUND FAN BLADE SHIMS MISSING MOLYDAG COATING GREATER THAN 25 PERCENT REF MM 72-21-02-200-801-F00 PARA I (1)(A). 24 EA SHIMS P/N 340-252-307-0 ORDERED ON FR 16675. A CONTINUE IN SERVICE LIMIT OF 250 CYCLES IS PESDR DXTA2009031303542Monopole · failedSHORTLY AFTER TAKEOFF, LT EEC FAILED WITH BOTH EEC'S IN MANUAL. LT ENGINE WOULD COMPRESSOR STALL WHEN N1 REDUCED BELOW 70 PERCENT AND N2 BELOW 85 PERCENT. NO NOTICEABLE RISE IN ITT WAS OBSERVED WITH POWER INCREASES. A SPLIT OF APPROX 2 INCHES IN POWER LEVERS TSDR HALA2009030500085Fan Blade · dentedETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE FAN ROTOR BLADE 21 HAS DENT APPROX 5.5 INCHES FROM ROOT AREA AT LEADING EDGE. BLENDED NR 1 ENGINE FAN ROTOR BLADE 21 IAW M/M 72-31-02-801 SEE L/P 316815 ITEM 70. ACCOMPLISHED FLUORESCENT PENETRANT TEST OF NR 1 ENGINE, BSDR R61A20090008Fan Blade · damagedON CLIMBOUT OF CLE CREW RECEIVED A RIGHT ENG VIB EXCEEDANCE OF 4.0. CREW FOLLOWED QRH AND SHUTDOWN ENGINE, DECLARED EMERGENCY INTO CMH. CMH MAINTENANCE FOUND SEVERAL FAN BLADES DAMAGED UPON INITIAL INSPECTION. ENGINE WAS BOROSCOPED, AND SEVERAL BLADE SETS RSDR USAA2009030290477Blade · failedFLT 180 - WHILE CLIMBING THROUGH 23,000 FT THE FLIGHT CREW FELT 6 TO 12 STRONG JOLTS AND RECEIVED ECAM MESSAGES "NUMBER 1 ENGINE FAIL" THEN "NUMBER ONE ENGINE STALL". THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO MCI FOR MAINTENANCE. COMPLIED WITH (DSDR IPXA09555156Structure · chafedINSPECTION TYPE:C NR 2 V-BAND GROOVE HAS A CHAFED MARK AT 11 O'CLOCK POSITION. HAND BLEND CHAFE AREA IAW EO535-7230-32641 PG 4 APP A PG 1, 2 PER SP TASK70-42-11-300-001. HFEC REQRK IAW NTM51-00-19PT6 PER EO 535-7230- 32641P1 NO CRACK FOUND. APPLY CHROMATE CSDR IPXA09555155Structure · chafedINSPECTION TYPE:C NR 2 V-BAND GROOVE HAS A CHAFED MARK AT 11 O'CLOCK POSITION. HAND BLEND CHAFE AREA IAW EO535-7230-32641 PG 4 APP A PG 1, 2 PER SP TASK70-42-11-300-001. HFEC REQRK IAW NTM51-00-19PT6 PER E0535-7230- 32641P1 NO CRACK FOUND. APPLY CHROMATE COSDR IPXA09555047Structure · chafedINSPECTION TYPE:C NR 2 ENGINE V-BAND GROOVE HAS CHAFED MARK AT 1'OCLOCK POSITION. HAND BLENDED CHAFED AREA IAW EO535-7230-32641P4 APP Z PG 1, 2 ST 1 PER SPM TASK 70-42-11-300-001. HFEC REWORK AREA IAW NTM51-00-19PT6 PER EO 535-7230-32641 P1, NO CRACK FOUND. SDR IPXA09555046Structure · chafedINSPECTION TYPE:C NR 2 ENG V-BAND GROOVE HAS CHAFED MARK AT 1 O'CLOCK POSITION. HAND BLND CHAFED AREA IAW EO535-7230-32641 PG 4 APP A PG 1, 2 STP1 PER SPM TASK70-42-11-300-001. HFEC REWRK IAW NTM51-00-19PT6 PER EO535-7230- 32641P1, NO CRACK FOUND. APPLIED CSDR CA090227011Cone · separated(CAN) A/C WAS IN CRUISE AT 5000 FT WHEN A LOUD POP WAS HEARD ACCOMPANIED BY A SINGLE TORQUE OSCILLATION. PILOT REDUCED HIS POWER TO LAND. A BURNING OIL ODOR WAS DETECTED ON THE DESCENT. THE PILOT LANDED NORMALLY WITH FULL POWER AVAILABLE ON LANDING. INVESTIGATSDR CA090313009Blades · broken(CAN) ENGINE EXPERIENCED A COMPRESSOR STALL IN CRUISE. PILOT RETURNED TO BASE, AS THE ENGINE WAS LOADED UP FOR LANDING 2 MORE COMPRESSOR STALLS OCCURRED. ACFT WAS LANDED AND SHUTDOWN WITHOUT FURTHER INCIDENT. COMPRESSOR WAS SENT TO REPAIR SHOP WHERE IT WAS NOTSDR UALA2009031000582Compressor · stalledNR 2 ENGINE COMP STALL WITH ASSOCIATED BANG. RTFL. REPLACED NR 2 ENGINE DUE TO DECLINING PERFORMANCE MARGIN.SDR CA090223012Compressor · contaminated(CAN) SMOKE AFT LAV ON CLIMB-OUT. CREW RETURNED TO DEPARTURE AIRPORT. ENGINE COMPRESSOR WASH HAD BEEN CARRIED OUT DURING MX NIGHT PREVIOUS TO FLIGHT DEPARTURE. MX CARRIED OUT POST COMPRESSOR WASH CHECK LIST IAW AMM 72-00-00. NO FUTHER DEFECT NOTED. TEST FLISDR ZZDA2009056Compressor · stalledLEFT ENGINE COMPRESSOR STALLED AND TGT REDLINED ON SHUT DOWN. TGT-1180 C. EMERGENCY LANDING MADE. REMOVED AND REPLACED NR 1 ENG ON W/O 190329 TASK CARD 603. AUTO LAND ACCOMPLISHED ON W/O 190329 TASK CARD 625.SDR 2009FA0000232Seal · crackedSUBJECT ENGINE WAS RECEIVED DUE TO HIGH TIME. DURING DISASSEMBLY AND INSP OF THE HPC THE DIFFUSER AIRSEAL PN 56H192, SN CENCBG1041 WAS FOUND WITH LINEAR CRACKS IN THE BOLT HOLE FLANGE ID, IAW CIR MANUAL PN 51A750 INSP CHECK 02 (NDI) NO CRACKS ARE ALLOWED. ENSDR ABXA200902130012Compressor · stalledCLIMBING OUT OF KIX AT FL340, THE RIGHT ENGINE COMPRESSOR STALLED 3 TIMES, PULLED BACK THE RIGHT THROTTLE JUST A LITTLE AND THE STALLS STOPPED. THE ANTI-ICE WAS OFF, A/T WERE ON. AIRCRAFT CONTINUED TO CLIMB AND THERE WERE NO POWER CHANGES. THERE WERE NO ABNSDR CA090216007Compressor · stalled(CAN) SURGE/IFSD/AIR RETURN. DURING CLIMB OUT OF DEPARTURE AIRPORT AT 5000 FEET, LOUD BANG REPORTED ACCOMPANIED BY ACFT YAW AND ENG L COMPRESSOR STALL ALERT. ENGINE AUTO SHUTDOWN. ACFT RETURNED TO DEPARTURE. INITIAL FINDINGS NOT AVAILABLE AS OF THIS WRITING. ESDR UALA2009031000387Compressor · damagedNR 1 & NR 2 ENGINE FOD. CREW REPORTED, WALK-AROUND AFTER ARRIVAL IN JAC, FOUND FOD DAMAGE TO THE NR 1 & NR 2 ENGINES. ACP A BORESCOPE INSPECTION WITH NO LIMITING DEFECTS NOTED. REPLACED COMPLETE FAN SET ON BOTH ENGINES.SDR QXEA2009020300081Actuator · leakingSFO - FUEL STREAMING FROM LT ENGINE LOWER DRAIN. DETERMINED TO BE COMING FROM THE SLAVE COMPRESSOR VARIABLE GEOMETRY ACTUATOR. REMOVED AND REPLACED LT ENGINE SLVGA PER CRJ700 AMM TASKS 75-30-03-000-801-A01 AND 75-30-03-400-801-A01. LEAK CHECK GOOD. RAN ENGSDR UPS09654454Compressor · stalledINSPECTION TYPE:ETOP RTO LT ENG COMPRESSOR STALLED. PULLED HARD LEFT AT 80 KTS. TOWER REPORTED FLAMES FROM LEFT ENGINE AFTER ABORT. A/C OOS. ***SDR FILED OPEN***SDR SWAA090513Blades · damagedDURING SCHEDULED HC2 CHECK, FOUND NR 1 ENGINE HPC BLADES DAMAGED. REMOVED AND REPLACED NR 1 ENGINE PER MT.SDR HALA2009011500021Blades · damagedETOPS SIGNIFICANT SYSTEM, FOUND NICKS ON BLADES 321 AND NR 22 ON NR 2 ENG BLADE NR 21 3/32 BY 1 3/4 INCH BLADE 22 1/16 BY 1 1/4 INCH. BLENDED FAN BLADES NR 21 AND NR 22 PER AMM 767 72-31-02. NICKS IN AREA A ON BOTH BLADES. EDDY CURRENTED. NO CRACK INDICATISDR SWAA090323Compressor · damagedABORTED TAKEOFF, ON TAKEOFF ROLL, NR 1 ENGINE APPARENTLY COMPRESSOR STALLED. SEVERAL LOUD BANGS ACCOMPANIED BY AIRFRAME VIBRATIONS AND A BRIGHT FLASH. TAKEOFF REJECTED. IDLE INDICATIONS APPEARED NORMAL. FOUND NUMEROUS HPC 7-8TH STAGE BLADE DAMAGED. CHANGESDR DL76L090043Blade · failedNR 1 ENGINE DUE FAILED BORO 7 STG HPC. INSP 7TH STAGE HPC BLADE ROOT FOUND 1 BLADE DAMAGED .185 IN AREA C. BEYOND AMM LIMITS. NR 1 ENGINE CHANGE REQUIRED.SDR VNAA2009011400004Engine · bird ingestionCREW REPORTED POSSIBLE BIRD STRIKE ON FINAL TO DAY. MX INSPECTED ACFT FOR BIRD STRIKE AND FOUND IT TO BE CONTAINED TO LT ENGINE ONLY. MX COMPLIED WITH BIRD STRIKE INSPECTION ON LT ENGINE AND FOUND FAN BLADES DAMAGED. MULTIPLE FAN BLADES WERE CHANGED ALONG WSDR AALA2009010300149Blades · damagedMDE INFLIGHT - CREW REPORTED OVER TEMPERATURE INDICATION ON ENGINE NUMBER ONE PASSING VECTOR ONE. PERFORMED EMERGENCY SHUTDOWN OF ENGINE NUMBER ONE. RETURNED TO MDE AND LANDED OVERWEIGHT WITH HOT BRAKES. RIGHT MAIN BRAKES PLUGS MELTED. UNABLE TO MOVE AIRCRSDR DXTA2009010103451Fan Blade · damagedON PREFLIGHT WE DISCOVERED DAMAGE TO 2 OF THE LT ENGINE FAN BLADES THERE IS ALSO DAMAGE TO THE ENGINE SHROUD AT THE 7 O`CLOCK POSITION. REPLACED 3 FAN BLADES, FAN EXIT VANE RING, FAN CASE, AND INLET COWL. PERFORMED A SATISFACTORY 5 POINT GROUND PERFORMANCE RUSDR CA090109009Blades · damaged(CAN) ON TAKEOFF, A JUMP IN EPR AND WAS OBSERVED AS WELL AS A MOMENTARY ILLUMINATION OF THE LOW OIL PRESSURE LIGHT ON THE NR 3 ENGINE. THE ENGINE WAS SHUTDOWN AFTER THE TOWER REPORTED SEEING SPARKS. ON EXAMINATION DAMAGE WAS FOUND TO THE C1 AND C2 BLADES AND S
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