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 CA070216008Blade · cracked(CAN) ON INSPECTION, A STAGE 4 BLADE WAS FOUND TO HAVE A 0.080 INCH CRACK THROUGH THE DOVE TAIL AREA ON THE TRAILING EDGE SIDE. OUR FILE NR SQID 07-00588 (TC NR 20070216008)SDR C8GA20070003Blades · damagedFLT 1723 FROM BOS TO TOL, DURING CLIMB-OUT, NR 2 ENGINE BEGAN TO VIBRATE AND WAS CONFIRMED WITH THE THROTTLE. ENGINE BEGAN TO COMPRESSOR STALL, ENGINE WAS SHUTDOWN AND AIRCRAFT LANDED WITHOUT INCIDENT IN TOL. POST FLIGHT INSPECTION REVEALED FOD DAMAGE TO THESDR WRLA2007036Blades · damagedJFK/BRU AIR TURNBACK DUE TO ENGINE VIBRATION HIGH ALERT ON NR 2 ENGINE AT 700 FT ON TAKEOFF NR 2 ENGINE COMPRESSOR READS 5.8 VIBRATION AND SOUND PRESENT. WHEN THROTTLE RETARDED VIBRATION CEASED. DUMPED FUEL AND RETURNED BACK FOR LANDING AT JFK. NR 2 ENGINE SDR AALA20070329Blade · failedORD INFLIGHT T289 - LEFT ENGINE COMPRESSOR STALL JUST AFTER LIFT OFF. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ON 17 FEB AT ORD DUE TO FAILURE OF NUMBER SIX HIGH PRESSURE COMPRESSOR BLADE. SYSTEM GROUND CHECKED NORMAL OPERATIOSDR DJFA2007019Seal · leakingTRIP NR 1141843 CREW REPORTED A NOXIOUS OILY SMELL WHEN ENGINE IS AT HIGH POWER SETTINGS CONTINUING THROUGH CLIMB THEN DISSIPATING DURING CRUISE. MAINTENANCE FOUND BROWN RESIDUE INTO BLEED DUCT WITH SOME CRYSTALLIZATION AND SUSPECTS LEAKING AT CENTRIFUGAL COMSDR 2007UALA00432Blade · failedNR 1 ENGINE STALLED INFLIGHT. [SUP 4-20-07] SURGE OCCURRED AT TOD; ENGINE REPLACED AT ORD. TEARDOWN REVEALED THAT 1 HP COMPRESSOR STAGE-7 BLADE FAILED IN THE AIRFOIL NEAR THE TIP. THE AMOUNT OF MISSING AIRFOIL WAS APPROXIMATELY 1-SQ.IN. FAILURE BEGAN ASSDR 2007UALA00363Compressor · stalledRTFL DUE TO NR 2 ENGINE COMPRESSOR STALL. [5-1-07] STALL OCCURRED AT TOP-OF-CLIMB AFTER TURNING-OFF THE ANTI-ICE VALVE. ALL CHECKS WERE PERFORMED PER THE AIRBUS TSM WITH NO FINDINGS. THE ENGINE PASSED POWER ASSURANCE RUN AND WAS RETURNED TO SERVICE. SUSPESDR 2007UALA00341Blade · failedCREW REPORTS ON TAKEOFF ROLL JUST BELOW 80 KNOTS, AUDIBLE COMPRESSOR STALL & REPORT OF FLAME FROM EXHAUST. [5-1-07] BORESCOPE INSPECTION OF THE HPC REVEALED DAMAGE STARTING WITH THE R3 BLADE (THE FIRST STAGE). SUSPECT ANOTHER R3 CLAPPER FAILURE RESULTING INSDR PCSA2062007SUCompressor · damagedFLIGHT 713 ABORTED THE TAKEOFF AFTER THE FLIGHT CREW EXPERIENCED A VIBRATION COMING FROM THE NR 1 ENGINE, THE AIRCRAFT RETURNED TO THE GATE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINES AND FOUND THE NR 1 ENGINE SHOWING EVIDENCE OF DAMAGE TOSDR C2XA07IA024Fan · fodFLIGHT 2055, ON APPROACH, THE CREW REPORTED A BIRD STRIKE FOLLOWED BY AN UNCOMMANDED SHUTDOWN OF THE NR 2 ENGINE. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THESDR CA070314014Compressor · seized(CAN) FLAMES WERE SEEN EXITING THE ENGINE EXHAUST AND THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED COMPRESSOR SEIZURE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070314014)SDR 2007UALA00265Blades · damagedENGINE NR 1 STALL DISPLAYED ON UPPER ECAM SCREEN DURING STEADY STATE CLIMB OR CRUISE. ENGINE NOT SHUTDOWN. BORESCOPE INSPECTION OF THE HPC REVEALED DAMAGE TO R6 BLADES BEYOND SERVICEABLE LIMITS. ENGINE WAS CHANGED.SDR UG8A2007GM001Stator · crackedDURING VOLUNTARY COMPLIANCE WITH MFG SB 72-1706 (BORESCOPE INSPECTION OF HP COMPRESSOR 7TH STAGE STATOR VANE) A CRACKED STATOR VANE WAS DISCOVERED.SDR UG8A2007GM002Stator · crackedDURING VOLUNTARY COMPLIANCE WITH MFG SB 72-1706 (BORESCOPE INSPECTION OF HP COMPRESSOR 7TH STAGE STATOR VANE) A CRACKED STATOR VANE WAS DISCOVERED.SDR 2007UALA00218Blades · damagedRTFL DUE TO A BIRD STRIKE IN THE NR 1 ENGINE. BLADES BENT AND DAMAGED. :REPLACED FAN BLADES PER MM 72-21-04. NR 1 ENGINE WAS NOT SHUT DOWN UNTIL ON GROUND.SDR ABXA070019Blade · damagedON TAKEOFF FROM ILN, DURING LANDING GEAR RETRACTION, GOT SUBSTANTIAL IMPACT SOUND FROM LEFT ENGINE AREA, AND BURNING SMELL AFTER SOUND. NO ENGINE ABNORMALITIES OR EXCEEDANCES. LANDED UNDER WEIGHT. C/W BIRD STRIKE INSPECTION BORESCOPE & BLADE REPLACEMENT ON SDR DXTA200701871Bearing · damagedSTRONG FUMES IN THE COCKPIT, NO VISIBLE SMOKE. FUMES STRONGEST WITH ENGINE POWER HIGH. FUMES ARE LOCALIZED IN COCKPIT AREA NOT NOTICEABLE IN CABIN AREA. NO DIVERT. INSTALLED LT ENGINE NEW FAN SHAFT, BEARING AND SEAL IAW ROLLS ROYCE MM 72-21-20. RAN AIRCRASDR 0700219953Compressor · stalledDURING TAKEOFF ROLL, AT APPROXIMATELY 100KTS, NR 1 ENGINE COMPRESSOR STALLED. TAKEOFF WAS ABORTED AND THE AIRCRAFT SKIDDED OFF THE RUNWAY. THE AIRCRAFT IS BEING REPAIRED AND THE NR 1 ENGINE IS BEING REPLACED.SDR CA070514057Blade · damaged(CAN) DURING DESCENT ENGINE OIL PRESSURE REDUCED ACCOMPANIED BY AN INCREASE IN INTER-TURBINE TEMPERATURE. ENGINE POWER WAS REDUCED AND A LANDING ACCOMPLISHED AT LOW POWER. SUBSEQUENT INSPECTION REVEALED COMPRESSOR TURBINE BLADE DAMAGE. MFG WILL MONITOR INVESDR CA070114002Bolt · cracked(CAN) ENGINE WAS INDUCTED INTO SHOP FOR SCHEDULED MAINTENANCE. DURING THE SHOP VISIT THE FAN DISK WAS REMOVED FROM THE FAN ASSEMBLY AND ROUTED FOR OVERHAUL. THE DISK ATTACH BOLTS (QTY 30) WERE ROUTED FOR NDT INSPECTION. FPI DETECTED ONE FAN DISK ATTACH BOLT WSDR 2007UALA00071Compressor · stalledNR 1 COMPRESSOR STALL IN DESCENT. [SUP 4-17-07] CAUSE WAS CIT SENSOR NOT RESPONDING TO TEMPERATURE CHANGE. REPLACED CIT SENSOR AND MAIN ENGINE CONTROL UNIT. MEC BENCH TEST FOUND NO FAULTS. CIT SENSOR DID NOT RESPOND TO TEMPERATURE CHANGE. BOTH UNITS MADESDR SWAA070119Compressor · stalledINFLIGHT SHUTDOWN/AIR TURNBACK, ON LEVEL OFF AT 10,000 NR 1 ENGINE STARTED TO COMPRESSOR STALL. SECURED NR 1 ENGINE PER QRH. REMOVED AND REPLACED NR 1 ENGINE PER MT.SDR 2007UALA00044Compressor · stalledNR 2 ENGINE COMPRESSOR STALL. ENGINE CONTINUES STALLING WHENEVER THROTTLE ADVANCED BEYOND IDLE. ENGINE REPLACED AT KIX. SHOP DISASSEMBLY SHOWED HEAVY HP COMPRESSOR BLADE DAMAGE RESULTING FROM LIBERATION OF 14 BROKEN VARIABLE STATOR VANE INNER TRUNNION 'BUTTONSDR P5CA0701511Compressor · damagedDURING TREND MONITORING OF NR 3 ENGINE, A SHIFT IN PARAMETERS WAS NOTICED. AN INSPECTION ON THE NR 3 ENGINE WAS REQUESTED AND THE AIRCRAFT WAS DIVERTED TO PIK FOR A BORESCOPE INSPECTION. INSPECTED NR 3 ENGINE AND FOUND 11TH STAGE DAMAGE. REMOVED AND REPLACESDR PCSA10420071Compressor · damagedFLIGHT 743 DURING THE TAKEOFF ROLL FROM MIA THE CREW EXPERIENCED A VIBRATION ON THE NUMBER 3 ENGINE, THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED BACK TO THE GATE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 3 ENGINE AND FOUND THE C-2 COMPRSDR CNMA20070001Compressor · damagedNR 2 ENGINE FAILED ON TAKEOFF ROLL AT 70KTS TAKEOFF ABORTED. N1 WAS 103.0 EGT PEGGED. RAN ENGINE FIRE SEVERE DAMAGE CHECK LIST NO FIRE. R & R NR 2 ENGINE IAW 10UN-201. ENGINE S/N 517-533 INSPECTION REVEALED NO SIGNS OF FOD TO THE COMPRESSOR SECTION BUT HEAVYSDR DL76G061059Blade · damagedDURING T/O FROM ATL, NR 2 ENG HAD SURGE EVENT RETURNED TO ATL FOR INSPECTION. REMOVED HPC 1 - 2 - 3 AND 12 BORO PLUGS. PERFORMED BOROSCOPE INSP NR 2 ENG S/N 704750 HPC STAGES 1 AND 12 AND HPC STG 1 FOUND DAMAGE TO HPC STG 1 BLADES BEYOND AMM LIMITS, REF ITESDR CA070111016Fan Blade · separated(CAN) DURING CLIMB AT APPROXIMATELY 35,000 FEET, THE CREW HEARD A LOUD BANG AND THE LT ENGINE SHUTDOWN. THE CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. AN INSPECTION OF LT ENGINE REVEALED ONE FAN BLADE HAD FRACTURED JUST ABOVE THE ROOT. THE BLADE ROOSDR AALA20061304Compressor · stalledORD - DURING CLIMB ABOUT 2000 ABOVE GROUND LEVEL AIRCRAFT EXPERIENCED VIBRATION. CREW HEARD GRINDING SOUND FOLLOWED BY A SECOND JOLT. RIGHT ENGINE INSTRUMENTS DROPPED THEN WENT BACK UP. RETARDED AUTO THROTTLE TO IDLE AND JOLTS STOPPED. CAPTAIN SHUT DOWN RISDR DL757061042Engine · failedWINDING UP FOR T/O HEARD AUDIBLE ENGINE SURGE/STALL PASSENGERS OBSERVED FLAMES COMING FROM LEFT ENGINE. A/C RETURNED TO GATE. MTC INSPECTED TAIL PIPE FOUND BB SIZED DEBRIS. WILL NEED ENGINE CHANGE. REPLACED NR 1 ENG PER ROUTINE CARD DECK TRANS 6T103.SDR CA061214004Blade · missing(CAN) RECEIVED THIS ENGINE WITH A DEFECT OF LOW POWER. IT WAS RUN ON THE TEST STAND TO CONFIRM THE POWER OUTPUT WHICH WAS 1440 SHP. WHEN THE ENGINE WAS DISASSEMBLED THEY FOUND THAT A BLADE WAS MISSING FROM THE COMPRESSOR 4TH STAGE. THERE WAS NO DAMAGE TO THESDR AALA20061215Blade · failedDFW INFLIGHT T1883/08DEC - AT FLIGHT LEVEL 100, FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN. A FEW MINUTES LATER HEARD LOUD BANG FROM RIGHT ENGINE. RIGHT ENGINE SPOOLED DOWN ON ITS OWN. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED NUMBER SDR EOO2006F00001Snap Ring · damagedREMOVED COMPRESSOR FOR INSPECTION, FOUND DAMAGED SNAP RING GROOVE IN IMPELLER SPUR GEAR ADAPTOR SHAFT. SENT UNIT OUT FOR REPAIRS. (K)SDR AALA20061194Blades · damagedORD - ON TAKE OFF, AIRCRAFT YAWED TO THE RIGHT. FLIGHT ATTENDANTS REPORTED LOUD PBP BEFORE FLIGHT CREW ABORTED TAKEOFF. BRAKE TEMPERATURES DID NOT EXCEED 150 DEGREES. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. REPLACED NUMBER THREE AND FOUR MAIN LANDINGSDR AALA20061175Compressor · stalledDFW - ON TAKEOFF ROLL CREW HEARD LOUD BANG AND AIRCRAFT YAWED TO THE RIGHT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 07 DEC 2006 AT DFW DUE TO STEADY STATE COMPRESSOR STALLS. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR SWAA064744Blade · damagedINFLIGHT SHUT DOWN / DECLARED EMERGENCY / DIVERSION. DURING CLIMB NR 2 COMPRESSOR STALLED, SHUT DOWN NR 2 ENGINE PER QRH. FOUND DAMAGED COMPRESSOR BLADES. REMOVED AND REPLACED NR 2 ENGINE PER MM AND MT.SDR CA061204006Blades · cracked(CAN) SEE REPORT ATTACHED CRACK INDICATIONS WERE FOUND ON THE CT BLADES AT OVERHAUL. CRACKS WERE FATIGUE RELATED ON ALL THE CT BLADES. HOWEVER, THE ATTACHED REPORT STATES THAT THE CT BLADES DID NOT FAIL IN CREEP AS DETAILED IN MFG SILS, DUE TO OVERTEMP OR EXCSDR CA061208005Compressor · stalled(CAN) IN CRUISE, 2 HOURS FROM DESTINATION THE ENGINE STALLED AND EGT WAS RISING. WHEN EGT REACHED 1010 DEG. C, THE ENGINE WAS SHUTDOWN. THE OIL PRESSURE WENT TO ZERO AND BOTH N1 AND N2 ROTORS WERE ROTATING. DFDR DATA SHOWS: N2 VIBRATION WAS HIGH (3.5 TO 5.5 SDR CA061206003Blades · damaged(CAN) UNUSUAL NOISE AND VIBRATION FROM LT ENGINE. FOUND FAN BLADES NRS: 8,9,10,11,22,23,24 AND 25 BENT AND DAMAGED. AIRFRAME HOURS=5306:19. CYCLES=3929. (TC NR 20061206003)SDR AALA20061145Compressor · damagedTUL - ON CLIMB, LEFT ENGINE LOW PRESSURE ROTOR SPEED STARTED TO FLUCTUATE DRAMATICALLY ACCOMPANIED BY LOUD BANGING NOISES. BROUGHT THRUST LEVER BACK TO 1.3 TO 1.2 AND ENGINE STABILIZED. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. NO REMARKABLE EXHAUST GAS SDR DHL2006754003Compressor · stalledON T/O AT ILN, REJECTED T/O AT 60 KTS, COMPRESSOR STALL NR 2 ENG AUTO PACK TRIPPED. RESET PACKS. RAN CHECKLIST. ALL INDICATIONS NORMAL. NORMAL T/O ON SECOND ATTEMPT. CREW ADVISED MTX THAT THERE WAS 20+ MPH CROSSWINDS, PERFORMED INLET AND EXHAUST VISUAL INSDR HALA0600880Blade · nickedON ETOPS WALK AROUND MECHANIC FOUND A NICK ON NR 24 1ST STAGE FAN BLADE ON NR 2 ENGINE, DEPTH: .188, WIDTH: .500, 5 3/16" FROM BLADE TIP. REPAIRED BLADE NR 24 BY BLENDING PER AMM 72-31-02.SDR CA061124001Compressor · damaged(CAN) ENGINE TEARDOWN RELATED TO AN IFSD AND A POSSIBLE COMPRESSOR FAILURE. TEARDOWN NOT YET CONCLUSIVE. IT WAS NOT A COMPRESSOR FAILURE BUT APPEARS TO BE FAILURE OF ONE OR MORE CT BLADES AND THEN CAUSED A STRUCTURAL FAILURE OF THE GAS GENERATOR CASE, WHICH TSDR CA061123003Impeller · cracked(CAN) "IMPACT DAMAGE AND A CRACKED IMPELLER". A CRACK IN THE OUTER IMPELLER WAS FOUND. (TC# 20061123003)SDR CA061120005Fan Blade · bent(CAN) ON APPROACH CREW SAW LARGE WHITE BIRD , FELT AND HEARD THUMP ON LEFT SIDE OF AIRCRAFT. MAINTENANCE INSPECTION FOUND #1 ENGINE INLET BYPASS FAN BLADES POSITIONS 1 THRU 5 DAMAGED AND BENT. BORESCOPE OF ENGINE COMPRESSOR FOUND NO OTHER DAMAGE. AIRCRAFT WILLSDR CA061120009Duct · ruptured(CAN) ENROUTE TO DESTINATION, #2 ENGINE FIRE WARNING. CHECKLIST ACCOMPLISHED, ENGINE SHUTDOWN. 13TH STAGE SADDLE DUCT FOUND RUPTURED, REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC# 20061120009)SDR CA061118001Engine · bird ingestion(CAN) AFTER GEAR-UP SELECTION THE AIRCRAFT ENCOUNTERED A VIBRATION, FELT THROUGHOUT ENTIRE PLANE,THAT WOULD INCRESE/DECREASE WITH THROTTLE MOVEMENT. AIRCRAFT RETURNED TO THE ORIGINATING DEPARTURE STATION AND LANDED SAFELY. MAINTENANCE FOUND NR 1 ENGINE FAN BLASDR F222007F00000Compressor · stalledPILOT REPORTED FLAMES MOMENTARILY COMING FROM THE LT AND RT ENGINE EXHAUST STACKS. THE PILOT DECIDED TO LAND AT AN AIRPORT THAT WE ALSO SERVE AS AN AIR AMBULANCE AND SWAP PLANES TIL THE CAUSE COULD BE DETERMINED. THE PILOT REPORTED IT TO MAINTENANCE AS A COMSDR CA061128005Compressor · damaged(CAN) ON POWER APPLICATION FOR TAKEOFF, THE #2 ENGINE ACCELERATED NORMALLY TO TAKEOFF POWER. AS THE AIRCRAFT BEGAN TO CLIMB ONTO THE STEP, THE F/O OBSERVED A FLASH OF LIGHT AND HEARD A BANG FROM THE ENGINE. THE TAKEOFF WAS REFECTED AND THE AIRCRAFT RETURNED SDR AALA20061023Compressor · stalledORD - HEARD LOUD BANG AND RIGHT ENGINE EXHAUST GAS TEMPERATURE INCREASED TO 800C. CREW SHUT DOWN ENGINE. SINGLE ENGINE TIME TEN MINUTES. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 09 NOVEMBER AT ORD DUE TO COMPRESSOR STALLS.
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