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 CA130222006Compressor · damaged(CAN) STARTING RT ENGINE, FUEL FLOW .3 TO .4 ON START. ENGINE ACCELERATED TOWARDS IDLE, STARTER CUTOUT, FUEL FLOW DID NOT INCREASE AND ENGINE HUNG AND WOUND DOWN. ON RESTART ALL NORMAL. ACFT FLEW 1 LEG, AND THEN MAINTENANCE AT NEXT BS T/S. ENGINE REPLACED SDR UALA2013021500895Stator Vane · damagedNR 1 ENGINE STATOR VANE AT 11:30-12:00 POS MISSING CHUNK OF LEADING EDGE REF AMM 72-33-02, DAMAGE STATOR MEASURES BETWEEN .250 AND .500 "AXIAL LENGTH" TAPED AS REQ OK FOR SERVICE.SDR UALA2013021500894Stator Vane · damagedNR 2 ENGINE STATOR VANE AT 11:30 POS MISSING CHUNK OF LEADING EDGE. REF AMM 72-33-02 DAMAGE STATOR MEASURES BETWEEN .250 AND.500"AXIAL LENGTH" WITHIN LIMITS TAPED AS REQ OK FOR SERVICE.SDR CA130220004Link · failed(CAN) UPON STOWING THRUST REVERSER RT ENGINE FLAME OUT MESSAGE ILLUMINATED AND ITT SPIKED, AFTER CLEARING ACTIVE RUNWAY MESSAGE CLEARED AND ITT RETURNED TO NORMAL. RIGHT ENGINE REMAINED FLAMED-OUT. MAINTENANCE R & R THE RT ENGINE INBD AND OTBD VG TORQUE SHAFTSDR CA130214017Compressor · damaged(CAN) AFTER 40 MIN OF FLIGHT, PILOTS REPORTED LOUD BANG COMING FROM THE ALONG WITH HIGH ITT INDICATION OVERTEMP. THE FLIGHT CREW COMMANDED THE SHUTDOWN. ATB. EMERGENCY DECLARED. SINGLE ENGINE LANDING AT ORIGIN AIRPORT. MAINTENANCE CREW PERFORMED VISUAL INSPESDR CA130204009Compressor · damaged(CAN) THE FOLLOWING LANDING EVENT OCCURRED: RECEIVED LT ENGINE BLEED CAUTION MSG FOLLOWED BY LEFT ENGINE DEGRADED CAUTION MSG DURING FINAL, UPON LDG LT ENG FLAMED OUT, FLAMEOUT, CAUTION MSG WAS RECEIVED. THE CAPTAIN REPORTED THAT DURING APPROACH FLIGHT, THEY SDR P5CA2013012400003Compressor · stalledAT ROTATION, NR 2 ENGINE COMPRESSOR STALLED 4 OR 5 TIMES WITH A FLASH. REDUCED THRUST, ENGINE STABILIZED. CLIMBING THROUGH FL210, EGT NEAR REDLINE, REDUCED THRUST TO IDLE, THEN SHUT ENGINE DOWN TO AVOID OVERTEMP. FOUND LEVER ARM BROKEN, ENGINE REPLACEMENT RSDR CA130118010Blades · damaged(CAN) RT ENGINE APR ON N1 GAUGE MESSAGE ON TAKEOFF ROLL, REJECTED TAKEOFF AT BETWEEN 80-100 KNOTS, WAS A NOTICABLE SHUTTER IN THE AIRFRAME WHEN MESSAGE OCCURRED, NO OTHER ABNORMALITIES WITH PARAMETERS NOTED BY CREW, DAMAGE FOUND ON COMPRESSOR BLADES, ENGINE RSDR A6WA201301134010Fan · out of balanceRIGHT ENGINE FAN VIBRATION SHOWED 2.7 MILS IN FLIGHT AND HAD TURNED YELLOW. COULD NOT FEEL PRONOUNCED VIBRATION IN THROTTLE. CREW RAN QRH AND DETERMINED THAT ENGINE SHUTDOWN WAS NOT REQUIRED DUE TO NO OTHER ABNORMAL ENGINE INDICATIONS PRESENT. CREW DECLAREDSDR VNAA2013011000003Compressor Blade · damagedCREW REPORTED LEFT ENGINE WOULD NOT ATTAIN CLIMB POWER WITHOUT EXCEEDING ITT LIMIT. MULTIPLE AIRFRAME VIBRATION / SHUDDERS WERE ALSO REPORTED, WITH ONE SEVERE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LEFT ENGINE AND FOUND SDR UALA2013010900171Blade · damagedNR 1 ENGINE HAS A DAMAGED FAN BLADE. REPAIRED IAW AMM 72-31-02 PAGE 801. INSPECTED AND HFEC PER MM 72-31-02-801. ADDITIONAL .020 BLEND-OUT REQUIRED PER MM 72-31-02-801. C ACCOMPLISHED ADDITIONAL .020 BLEND IAW AMM 72-31-02 PAGE 801.SDR HALA2013010900008Blade · nickedNR 1 ENGINE, 1ST STAGE COMPRESSOR BLADE NR 34 HAS NICK 2.6250 INCHES FROM TIP AREA A. BLENDED 1ST STAGE BLADE AIRFOIL IAW AMM 72-31-02. REPAIR WITHIN LIMITS. EDDY CURRENT INSPECTION OK.SDR HALA2013010900007Blade · nickedNR 1 ENGINE, 1ST STAGE COMPRESSOR BLADE, NR 33 HAS NICK 5.5 INCHES FROM TIP AREA A. BLENDED 1ST STAGE BLADE AIRFOIL IAW AMM 72-31-02. REPAIR WITHIN LIMITS. EDDY CURRENT INSPECTION OK.SDR HALA2013010900006Blade · bentNR 1 ENGINE, 1ST STAGE COMPRESSOR BLADE NR 27 HAS BENT AREA 17 INCHES FROM TIP AREA F. BLENDED 1ST STAGE BLADE AIRFOIL IAW AMM 72-31-02. REPAIR WITHIN LIMITS. EDDY CURRENT INSPECTION OK.SDR HALA2013010900005Blade · nickedNR 1 ENGINE, 1ST STAGE COMPRESSOR BLADE, NR 29 HAS NICK 17 INCHES FROM TIP AREA F. BLENDED 1ST STAGE BLADE AIRFOIL IAW AMM 72-31-02. REPAIR WITHIN LIMITS. EDDY CURRENT INSPECTION OK.SDR CA130110001Adapter · restricted(CAN) ON DESCENT, FLIGHT CREW NOTICED A STRONG BURNING PLASTIC ODOR IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND FLIGHT CREW DONNED THEIR OXYGEN MASK. SOME ELECTRICAL SYS AND ENGINE BLEEDS WERE TURNED OFF. AFTER FEW MINUTES THE ODOR DISSIPATED. ACFT LANDEDSDR CA130109010Housing · failed(CAN) THE BEARING HOUSING WAS REMOVED FROM COMPRESSOR ASSEMBLY DUE TO LOW POWER, AND WAS INDUCTED INTO THE SHOP. BEARING HOUSING AND NUT, WITH SHEARED PORTION OF THREADED STUD. THE SMALL LINE OF CLEAN METAL CAN BE SEEN, AND THAT IS ALL THAT EXISTED TO RETASDR CA130107011Linkage · loose(CAN) REF PILOT FLIGHT 2 SNAG 1 DATED JAN-3-2013 LT ENGINE EXCEEDANCE POSTED ON FINAL APPROACH, INITIALLY HEARD A LOW CLUNK NOISE. THEN LT ENGINE OPERATED ERRATICALLY INCLUDING HIGH ITT ,N2 OVER 100 PERCENT. LEFT ENGINE SEEMED VERY SENSITIVE TO THROTTLE MOVEMSDR CA130117002Blades · broken(CAN) AFTER TAKING OFF FROM HELIPAD AT 400 FT ABOVE GROUND LEVEL, AN ABNORMAL NOISE SIMILAR TO ENGINE SURGE NOISE WAS HEARD BY PILOTS FOLLOWED BY ODOR OF FUEL IN THE CABIN, RAPID RISE OF NR 2 ENGINE INTER TURBINE TEMPERATURE, ITT, AND ENGINE OIL TEMPERATURE, BSDR AALA20121227006Blades · damagedCUR - CREW REPORTED BIRD STRIKE TO LEFT ENGINE. FLIGHT RETURNED CUR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. INSPECTION REVEALED DAMAGE TO FIRST STAGE FAN BLADES. REPLACED FAN BLADE SET. SYSTEM GROUND CHECK NORMAL OPERATION.SDR QMLA2012122112196Blades · damagedVISUAL INSPECTION OF ENGINE COMPRESSOR BLADES SHOWED EVIDENCE OF DAMAGE. DETERMINED DAMAGE TO BE OUT OF LIMITS.SDR QMLA2012122112195Blades · damagedVISUAL INSPECTION OF ENGINE COMPRESSOR BLADES SHOWED EVIDENCE OF DAMAGE. DETERMINED DAMAGE TO BE OUT OF LIMITS.SDR 2013FA0000036Tie Rod · looseENGINE WAS REMOVED FOR COMPRESSOR FOD. ON DISASSEMBLY AT AN APPROVED CRS, IT WAS DETERMINED THE COMPRESSOR TIE BOLTS HAD LOST THE TIE ROD STRETCH (TORQUE) ON 4 OF THE 6 TIE BOLTS. RESULTING IN COMPRESSOR BOWING (IMBALANCE) RESULTING IN COMPRESSOR RUB DOD. PSDR P4YA2012121500001Blade · damagedAFTER TAKEOFF, NR 1 ENGINE LOST POWER, LOUD REPORT FROM ENGINE AND LANDED IMMEDIATELY. MX INSPECTED NR 1 ENGINE AND FOUND 1ST AND 2ND STAGE COMPRESSOR BLADE DAMAGE DUE TO FOD. R & R NR1 ENGINE.SDR CA121206005Fan · iced(CAN) CREW REPORTED HIGH RT ENGINE FAN VIBRATES. REPORTED VIBES AT 1.7 TO 1.9 AND THEN JUMPING TO ABOVE 3.5 BRIEFLY. THEY WERE NOT IN ICING CONDITIONS BUT PERFORMED ICE SHEDDING PROCEDURE IN QRH WITHOUT ACCEPTABLE RESULT. CREW ELECTED TO DIVERT AND DECLAREDSDR CA121211003Compressor · seized(CAN) CREW COMPLAINED OF POPPING NOISE WHEN GOING FROM IDLE TO FLY CONDITION. MECHANIC CONFIRMED NOISE AND COMMENCED COMPRESSOR WASHES AND RINSES. DURING THE RINSE CYCLE SPOOL DOWN THE MECHANIC NOTED A LOUD AND ABRUPT GRINDING NOISE. HE TRIED TO ROTATE THE CSDR UALA2012120607063Blade · deformedF/O NOTICED DEFORMATION ON ENGINE 2 BLADE 10. REMOVED AND REPLACED NR 2 ENGINE LP COMPRESSOR FAN BLADE NR 10 PER AMM 72-31-11-000-010 AND 72-31-11-400-010. RAN NR 2 ENGINE TO POWER FOR VIBRATION CHECK PER AMM 71-00-00-700-022 AND 77-32-34-869-010. ALL CHECKSDR EPUA20121212001Shroud · dislodgedDURING DESCENT ON LAST FLIGHT OF DAY, ENGINE TORQUE BEGAN TO DROP OFF. THIS CAUSED THE ACFT TO YAW TO THE RT. ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ENGINE AND DETERMINED THAT A COMPRESSOR TURBINE SHROUD SEGMENT HAD BECOME DISLODGED FROM THE SHROUD ASDR UALA2012112106721Blade · chippedCHIPPED FAN BLADE RIGHT ENGINE. BLADE MARKINGS WORN OFF, LEFT CHIPPED BLADE AT 6 O`CLOCK POSN. BLENDED 2 BLADES ADJACENT TO EACH OTHER REF AMM. BLADES ARE MARKED FOR EDDY CURRENT INSPECTION. DUE TO BLADE REPAIR, NEED EDDY CRNT INSP. CF EDDY CURRENT DUE TOSDR CA121125002Compressor · damaged(CAN) DURING CRUISE FLIGHT, THE PILOT REPORTED TURBULENCE FOLLOWED BY ENGINE STALL WITH N1 SPEED GOING DOWN AND TEMPERATURE GOING UP. THE PILOT ELECTED TO SHUTDOWN AND SECURE THE ENGINE BEFORE PERFORMING AN UNEVENTFUL LANDING AT DESTINATION. POST FLIGHT OF DSDR UALA2012111906690Blade · damagedFOD DAMAGE FOUND ON NR 2 ENGINE FAN BLADES 10 EA LOCATIONS (MARKED WITH MASKING TAPE) NEAR FAN SHROUD: 1 EA. TEAR APPROX .125" LENGTH, THE REMAINING NINE BEING NICKS. REPLACED COMPLETE SET OF BLADES.SDR COEA2012111605900Blade · failedENGINE FIRE/AIR TURNBACK, ENCOUNTERED A SLIGHT YAW TO LEFT AND A MOMENTARY TORQUE DECREASE OF 5 PERCENT ON NR 1 ENGINE. AFTER PILOT SMELLED AN ODOR. GAUGES READ NORMAL EXCEPT ITT FOR NR 1 ENGINE HAD INCREASED TO 780 DEGREES. WITHIN 30 SECONDS, SMOKE DETECTESDR UALA2012111606631Blade · nickedLEFT ENGINE FAN BLADE HAS A NICK. BLEND 1ST STAGE FAN BLADE NUMBER UNKNOWN. ACP'D EDDY CURRENT PER NDTM 72-31-401, NO CRACKS INDICATED.SDR UALA2012111406552Compressor · stalledRIGHT ENGINE COMP STALL, FLIGHT DIVERTED. REPLACED NR 2 ENGINE.SDR UALA2012111306540Compressor Blade · damagedWHILE ACCOMPLISHING EM3658, FOUND DISTRESS BEYOND MM72-00-00-601 LIMITS TO THE 5TH, 6TH, AND 7TH STAGE HPC BLADES. NUMEROUS NICKS, DENTS, TEARS, AND ONE THIRD OF A 7TH STG HPC BLADE MISSING. RVI PICS POSTED. REPLACED NR 1 ENGINE, S/N 727948.SDR UALA2012111306542Guide Vane · missingNR 1 ENGINE INLET GUIDE VANE MISSING AT 6 O'CLOCK POSITION. FOUND 1 VANE MISSING AT THE 6 O'OCLOCK POSITION OK TO CONTINUE TO THE NEXT ENGINE SHOP VISIT REF MM-72-33-02.SDR U2RA201211120003Blades · debondedNR 1 ENGINE, NR 14 FAN BLADE FOUND TAP DISPLAY MORE THAN 600 DB AT SEC "C" OUT OF LIMITS IAW SB RB211-72-9660. GENERATED FROM TASK CARD 72-136-01-01.SDR AALA20121107032Compressor · stalledIND INFLIGHT DCA-LAX. CREW REPORTED MULTIPLE COMPRESSOR STALLS ON LEFT ENGINE AFTER RECEIVING LEFT EEC/ENG LIMITER MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED IND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT IND ON 11/10SDR USAA2012111400020Blade · damagedBIRD STRIKE SHORTLY AFTER GEAR RETRACTION. LOUD BUZZING FROM NR 2 ENGINE THAT BENT 4 BLADES ON THE N1 FAN. ENGINE DID NOT SHUTDOWN. PERFORMED BIRD STRIKE INSPECTION - REMOVED AND REPLACED A FULL SHIP SET OF FAN BLADES AND ANNULUS FILLERS PER 72-31-11-000-01SDR AALA20121104001Blade · misrepairedCLIMBING OUT THROUGH ABOUT 5000 FEET A VERY STRONG ODOR WAS PRESENT IN THE COCKPIT AND CABIN. THE QRH PROCEDURE FOR SMOKE, FIRE OR FUMES WAS FOLLOWED. SMELL STARTED TO DISSIPATE BUT RETURNED A COUPLE OF TIMES. CREW RETURNED TO ORD. FOUND EXCESSIVE LUBRICANSDR UALA2012103106284Blade · damagedNR 1 ENGINE, NR 18 FAN BLADE DAMAGED, MID-SPAN. BLADE IS ACTUALLY NR 6. BLADES HAVE BEEN REMOVED PER MM. NEW BLADE HAS BEEN RECORDED AS NR 6 POS AND ALL SER NR'S AND WEIGHTS HAVE BEEN SENT TO TOMC FOR RE-DISTRIBUTION SOLUTION. ACCOMPLISHED BLADE INSTALLATSDR CA121029001Drum · cracked(CAN) HPC FRONT DRUM ASSY WAS FOUND CRACKED IN CENTER LINE IN SLOPE OUT INSIDE EBW WELD STAGE 5/6 DURING OVERHAUL PROCESS.SDR 2013FA0000038Tie Rod · looseENGINE WAS REMOVED FOR COMPRESSOR SEIZED AND COMPRESSOR FOD. UPON DISASSEMBLY AT CRS, IT WAS DETERMINED THE COMPRESSOR TIE BOLTS WERE FOUND TO HAVE NO STRETCH ON 4 OF 6. RESULTING IN COMPRESSOR IMBALANCE AND SEVERE RUB, SEIZING. POSSIBLE CAUSE: IMPROPER ASSSDR UALA2012102306070Blade · nickedNR 1 ENGINE HAS 2 EA FAN BLADES NR 22 AND 26, HAS NICKS BEYOND LIMITS. CONTINUED TO BLEND ALL 36 BLADES PER AMM. REPAIRED ALL 36 BLADES PER MM.SDR TRBA20121019001Valve · inoperativeDURING MX INSPECTION, FOUND ODOR OF OIL IN THE ACFT. R & R P2.5/P3 VALVE ASSY ON LT ENGINE IAW MM-72-30-00 (COMPRESSOR SECTION), ADDED TOTAL OF (3) WASHERS TO SHAFT.SDR UALA2012101805954Blade · out of toleranceENG2 FAN BLADE CHG OUT OF TIME. BLADE REPLACED AFTER BLADE DISTRIBUTION PERFORMED. ACP VIB SURVEY AND VIBS WERE WITHIN LIMITS.SDR UALA2012101705941Blade · bentNR 1 ENG HAS DAMAGE. FOUND ON 2SV NR 1 ENGINE HAS 2EA BENT FAN BLADES. REPLACED ENGINE.SDR UALA2012101905977Engine · bird ingestionFOUND EVIDENCE OF BIRD STRIKE ON NR 1 ENGINE INLET AT 2:00 POS AND 1:00 ON ENGINE CORE. FOUND NO EVIDENCE OF RUBBING ON THE FAN ATTRITION LINERS. FOUND NO DAMAGE ON THE FAN BLADES. NI ROTATION OK ENGINE NR 1 SERIAL V10483 REQUIRES LPC AND HPC BORESCOPE INSPSDR 2012F00218Compressor · damagedAFTER TAKEOFF, HEARD A LOUD POP. ON LANDING DISCOVERED NOSE OF ACFT ENCOUNTERED BIRD STRIKE. LEFT ENGINE INGESTED BIRD CAUSING DAMAGE TO 3 N1 COMPRESSOR BLADES.SDR CA121016007Compressor · stalled(CAN) WHILE ON A TRAINING MISSION, ABRUPT POWER CHANGES WERE BEING CONDUCTED WHEN COMPRESSOR STALL WAS NOTED ON THE NR 2 ENGINE. THE TRAINING MISSION WAS CANCELLED AND THE ACFT RETURNED TO BASE WITHOUT FURTHER INCIDENT. WHILE TROUBLESHOOTING THE COMPRESSOR
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