JASC 7230
Service difficulty reports · 5,064
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 WI5R201901160001Rotor · fracturedDURING FIELD BORESCOPE INSPECTION FOR ITT SPLIT AND HIGH-PITCH WHINE NOISE, DAMAGE TO THE HPC ROTOR, 3RD STAGE STATOR VANE, AND 3RD STAGE IP ROTOR VANES WERE DISCOVERED.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WERE MISSISDR AALA202001159016Seal · leakingAIRCRAFT WAS GROUNDED: CLT-SJU, AIR RETURNING TO CLT ACCOUNT SMOKE/ CHEMICAL ODOR IN COCKPIT. FLIGHT DID DECLARE EMERGENCY. ACCOMPLISHED J/C 33L00021001 DETERMINED SOURCE OF ODOR TO BE NO.1 ENGINE STREAKING BEHIND FAN BLADES ON LPC INLET VANES. ACCOMPLISHED EASDR SWIA2020021848697Vane · crackedL/H ENGINE LOWER CASCADE VANE HAS SUSPECT CRACK. (MARKED) (C-CHECK) RO 2/14/2020 REPLACED LH ENG LOWER CASCADE REF CRJ700 AMM. OPS CHECKS GOODSDR WI5R20200110001Rotor · fracturedDURING FIELD TROUBLESHOOTING FOR A REPORTED ENGINE VIBRATION, BORESCOPE INSPECTION REVEALED POTENTIAL IP BLADE LIBERATION.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR ASAA2020011331842Actuator · leakingDURING CRUISE TOTAL FUEL REMAINING / QUANTITY STARTED DECREASING AT AN ABNORMAL RATE, FUEL USED SHOWED AN UNEVEN BURN. GROUNDED - YES. DIVERSION TIME 18 MINUTES - PERFORMED ENG WET MOTORING IAW AMM 71-00-00-00 ON NR 2 ENG FOUND RT VSV DRAIN POURING FUEL AT ABNSDR WI5R20200108001Rotor · fracturedDURING FIELD BORESCOPE INSPECTION FOR N1 LAG AND ITT INCREASE AT T.O., A 3RD STAGE IP ROTOR BLADE WAS DISCOVERED MISSING.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR WI5R20200107001Rotor · fracturedDUE TO AND ITT AND N2 SHIFT NOTED IN THE TREND MONITORING, THE ENGINE WAS BORESCOPE INSPECTED.
BOROSCOPE INSPECTION REVEALED SEVERAL 3RD STAGE IP ROTOR BLADES WITH CRACKS PROPAGATING FROM THE ROOT TRAILING EDGE.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OSDR ASAA2020010631793Platform · crackedWHILE ACCOMPLISHING TC 78472010-FAN BLADE LUBRICATION ON ENGINE #2 ESN 897410 FOUND TWO PLATFORMS THAT ARE CRACKED AND BROKEN OFF A FWD LUG. GROUNDED - YES. REMOVED AND REPLACED COMPLETE SET OF PLATFORMS 24 PCS. IAW TASK 1 STEP 35 OF TC 78472010.SDR ASAA2020010631790Engine · damaged#2 ENGINE SN-892792 AFT SIDE OF THE J-HOOK STAGE 3 VSV T/E @ 12 O'CLOCK HAS MISSING MATERIAL REF T/C CMPT-72EO-02015-3 GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE PER SHOP WO 1038123SDR UIEA2019123096162Vane · delaminatedLEFT ENGINE 7 O'CLOCK POSITION EXIT VANE WITH DELAMINATION. REMOVED DAMAGE FROM EXIT VANE IAW AMM 72-33-02.SDR AALA201912279020Link · brokenAIRCRAFT WAS GROUNDED: PILOT REPORTS ON INITIAL DECENT FROM FL 330 ECAM ENG 2 STALL FOLLOWED BY ENG 2 FAIL FOLLOWED BY SUCCESFUL RESTART FOLLWED BY ENG 2 FAIL ON ROLLOUT. MAINTENANCE ACCOMPLISHED TSM 73-00-00-810-866-A. VSV LINK STAGE 3 FOUND TO BE BROKEN. REMSDR WI5R20191219001Rotor · fracturedDURING TAKEOFF AND CLIMB, SPARKS WERE REPORTED COMING FROM THE TAILPIPE. FIELD BORESCOPE INVESTIGATION IDENTIFIED A MISSING 3RD STAGE IP ROTOR BLADE.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT THREE OF THE 3RD STAGE IPC ROTOR BLADES WERE MISSING.SDR AALA2019123199017Blade · damagedAIRCRAFT WAS GROUNDED: PILOT REPORTS CLIMBING THRU 8-9000FT LARGE BANG LEFT ENGINE WITH A/C SHAKING, INDICATIONS INDICATED ENGINE SHUTTING DOWN. CHECK LIST FOLLOWED TO SHUT DOWN ENGINE. F/A REPORTS LARGE BANG WITH ELECTRIC POWER LEFT SIDE GOING OFF. EMERGENCY SDR WI5R20191218002Rotor · fracturedDURING A PRE-BUY BORESCOPE INSPECTION A MISSING IP BLADE AND HPC DAMAGE WAS NOTED.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR WI5R20191218001Rotor · fracturedDURING FIELD BORESCOPE INSPECTION FOR INCREASED ITT DURING CLIMB, SEVERAL IPC BLADES WERE DISCOVERED MISSING.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT THREE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR ASAA2019121643614Pin · migratedWHILE ACCOMPLISHING #1 ENG INSPECTION ESN #897741 FOUND STAGE 3 3 O'CLOCK POSITION ANTI-ROTATION PIN ROTATED AND MIGRATED OUT REF T/C SBCFM56-7B-72-0986-1. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE REF WO #1012101 AND TASK CARDS 78471000, 78471001, 784540SDR UIEA2019121326063Blade · nicked#2 ENGINE #14 C1 FAN BLADE HAS A NICK IN THE TIP AREA.(<P>BLENDED NICK IN TIP AREA ON #2 ENG #14 C 1 FAN BLADE IAW AMM 72-31-02-308-003. REMOVED APPROXIMATELY .030", WITHIN LIMITS.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>(NOTE: LP 1075824 - M6: DMI 121960 OPENEDSDR P5CA2019121320227Compressor · stalledAT 20,000 FT, NR 1 ENGINE COMPRESSOR STALLED. ENGINE WAS SHUT DOWN. ATB. REMOVED AND REPLACED THE NR 1 ENGINE IAW AMM 71-00-02. PERFORMED IDLE RUN AND LEAK TESTS IAW AMM 71-00-00, OPS CHECKED SATISFACTORY.SDR U2RA2020113060002Liner · corrodedRIGHT ENGINE HAS CORROSION DAMAGE AT 6 O'CLOCK POSITION UNDER LOW PRESSURE COMPRESSOR ROTOR PATH LINER - REMOVED AND REPLACED ENGINE PER AIRCRAFT MAINTENANCE MANUAL 71-00-02.SDR U2RA2020011360001Liner · corrodedLEFT ENGINE HAS CORROSION DAMAGE AT 6 O'CLOCK POSITION UNDER LOW PRESSURE COMPRESSOR ROTOR PATH LINER - REMOVED AND REPLACED ENGINE PER AIRCRAFT MAINTENANCE MANUAL 71-00-02.SDR SWAA2019120939413Compressor · stalledDECLARED EMERGENCY----------------------------------------------------------#1 ENGINE COMPRESSOR STALLS WITH VIBRATION UP TO 38 IN IDLE. STALLS OCCURRED WITH POWER IN MID RANGE. NO ENGINE LIMITS EXCEEDED. / R&R #1 ENGINE PER MT.SDR AALA2019120549008Actuator · faultyAIRCRAFT WAS GROUNDED: PILOT REPORTS APPLIED T/O POWER ENG 2 COMPRESSOR VANE FAULT. EXIT RWY AND SHUTDOWN. CLASS 2 MESSAGE, ENGINE 2 FADEC. MAINTENANCE PERFORMED REMOVAL AND INSTALLATION OF ENGINE 2 VSV ACTUATOR IAW JOB CARD 26T40075005 AND 26L00071014. OKAY FSDR NM1Y2019111300001Spool · damagedDURING ROUTINE HPC MODULE SHOP VISIT AT SAFRAN AIRCRAFT ENGINE HPC SPOOL 2-6 WAS SENT TO OUR REPAIR STATION FOR INSPECTION AND OVERHAUL.
THE FPI INSPECTION REVEALED UNUSUAL CIRCUMFERENTIAL LINEAR INDICATION IN THE STAGE 6 HOOK FILLET.
THIS SPOOL 2-6 (P/N 3SDR HALA2019110300466Compressor · stalledOPEN - ENG 1 COMPRESSOR STALL, LOUD BANG, POWER LOSS FOLLOWED BY HIGH VIBE. // R&R #1 ENGINE.SDR ASAA2019103101187Pin · missingDURING ACCOMPLISHMENT OF SBCFM56-7B-72-0986-1 BORESCOPE INSP, METALLIC HYBRID #1 ENGINE STEP 7 FOUND STAGE 3 PIN AT 9 O'CLOCK MISSING AND DAMAGED ON THE ROTOR, REQUIRES ENGINE CHANGE. GROUNDED - YES. REMOVED AND REPLACED ENGINE REF SHOP W/O # 1009709, N/R # 00SDR AALA201910189013Blade · damagedAIRCRAFT WAS GROUNDED: PILOT REPORTS AT CRUISE ECAM ENG 1 E10 FAULT ANNUNCIATED WITH ENGINE 1 FIRE LIGHT FLASHING, FAULT LIGHT ASSOCIATED AUTOTHURST ECAM MESSAGES FAULT WENT AWAY AFTER 3 MIN (THIS EVENT OCCURED TWICE). MAINTENANCE FOUND EVIDENCE OF A BIRDSTRIKSDR WI5R201910190001Blade · fracturedTREND DATA INDICATED A ABRUPT SHIFT IN ITT AND N2 PARAMETERS. FIELD BORESCOPE INVESTIGATION IDENTIFIED A MISSING 3RD STAGE IP ROTOR BLADE.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.
THE ROTOR (P/N 119345 S/SDR WI5R2019101900018Blade · damagedDISASSEMBLY REVEALED HPC ROTOR LIBERATED THE OUTER TIP OF TWO MAIN BLADES ABOUT THE SIZE OF A THUMB NAIL. THE ROTOR IS NOT ORIGINAL TO THE ENGINE AND HAS 4886 HOURS AND 6308 CYCLES. THE ENGINE HAS 9006 HOURS AND 11949 CYCLES. THERE WAS ALSO DAMAGE NOTED TO SDR 19EA20191115819Compressor · damagedITT SPIKED ON #1 ENGINE ENROUTE. SELECTED 85% POWER - ENGINE #1 WOULD ONLY RESPOND TO 45%. LEFT ENGINE ITT 100 DEGREES HIGHER THEN THE RIGHT ENGINE AFTER SHUTDOWN.SDR IPXA2019100447543Blade · nickedLEFT ENGINE, 1 X FAN BLADE LEADING EDGE NICK DAMAGE AT 564 MM FROM ROOT. BLEND REPAIR C/O IAW AMM 72-31-02. C/W INSPECTION OF THE LT ENGINE ONE FAN BLADE IAW AMM 72-31-02. NO CRACK NOTED. OK FOR CONTINUED SERVICE.SDR AALA2019100219001Solenoid Valve · leakingAIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO LAX ON ACCOUNT POSSIBLE COMPRESSOR STALL ON #1 ENGINE. EMERGENCY DECLARED. MAINTENANCE ACCOMPLISHED FULL ENGINE BORESCOPE INSPECTION IAW AMM 72-00-00-200-012, AMM 72-00-00-200-013, AMM 72-00-00-200-014, AMM 72-00-00-20SDR AALA201909309024Compressor · leakingAIRCRAFT WAS GROUNDED: PILOT REPORTS CABIN ODOR BEGAN AFTER TAKEOFF SEEMED TO DISSIPATE DURING CLIMB OUT AND AT CRUISE ODOR RETURNED PASSING THRU APPROXIMATELY 11000 FT, SEEMED STRONGER DESCRIBED AS DIRTY SOCK SOUR MILK SMELL. MAINTENANCE ACCOMPLISHED JOB CARDSDR VNAA2019092511101Blade · damagedDURING TAKE OFF FROM RUNWAY 36R AT 100 KNOTS THE CREW BELIEVED THEY BLEW A TIRE AND REJECTED THE TAKE OFF. THE AIRCRAFT TAXIED BACK TO THE GATE UNDER IT'S OWN POWER. MX INSPECTED AND FOUND DAMAGE TO RT ENGINE FAN BLADES. BORESCOPE INSPECTION REVEALED ENGINESDR HALA2019091900380Compressor Blade · crackedETOPS - #2 ENG DURING PHASED ARRAY INSPECTION FOUND BLADE #12 HAS CRACK, REPLACED #2 ENG #12 LP COMP BLADE.SDR UIEA2019091905543Blade · nicked#2 ENGINE, #10 FAN BLADE NICKED ON LEADING EDGE AREA "D". BLENDED #2, ENG #10 FAN BLADE LEADING EDGE IAW AMM 72-31-02. INSPECTED BLADE, NO CRACKS NOTED. REQUIRES DYE PENETRANT INSPECTION TO NON MEL 117872. LP 1111411 - M4: COMPLETED THE FLUORESCENT PENETRANT ISDR HALA2019091700377Engine · leakingECAM ENG. 1 CHIP DETECTED AFTER LANDING, STRANGE ODOR. DURING BOROSCOPE FOUND OIL LEAKING AT HPC STAGE 2. // ACCOMPLISHED #1 ENGINE CHANGE PER J321-72-HWI 02. OPS AND LEAK CHECK GOOD. VERIFICATION FLIGHT FOR #1 ENGINE CHANGES COMPLETED SATISFACTORY.SDR ASAA2019091530703Elastomer · tornWHILE ACCOMPLISHING TC 78472010 FOUND THAT ALL THE PLATFORMS RUBBER ON #1 ENG IS RIPPING. GROUNDED - YES. REPLACED ALL PLATFORMS ON #1 ENG REF TC 78472010 FAN BLADE LUBE.SDR AALA201909179001Compressor · leakingAIRCRAFT WAS GROUNDED: PILOT REPORTS MUSTY ODOR DURING TAKEOFF, INITIAL CLIMB, THEN DISSIPATED. MUSTY ODOR CAME BACK BELOW 10,000 FT DURING LANDING. MAINTENANCE FOUND OIL LEAK AT #2 ENGINE LOW PRESSURE COMPRESSOR. AN ENGINE CHANGE HAS BEEN DECLARED. MAINTENANSDR ASAA2019091330704Elastomer · missingWHILE ACCOMPLISHING TC 78472010 ON #2 ENGINE FOUND PLATFORM #18 MISSING THE ELASTOMER FROM ONE ENTIRE SIDE. GROUNDED - YES. REPLACED #2 ENGINE #18 PLATFORM REF TC 78472010.SDR ASAA2019090930663Blade · damaged#2 ENG SN 962761 FAN BLADES 1,2,6,7,10,11,14,17,18,21,23,24, HAS CU-NI DAMAGE REF TC 78472010. GROUNDED - YES. REPLACED ALL 24 BLADES PER T/C 78472010. ACCOMPLISHED VIBE SURVEY REF T/C 78472010.SDR ASAA2019090730638Actuator · leakingDURING WALKAROUND NOTICED FUEL DRIPPING FROM #2 ENGINE. GROUNDED - YES. OPENED #2 ENG COWLS. FOUND FUEL DRIPPING FROM LEFT VSV DRAIN TUBE AT 3 DROPS PER MIN. HAD CREW RUN #2 ENGINE AT IDLE. NO LEAKS NOTED DURING IDLE RUN. AFTER SHUT DOWN NO LEAKS NOTED FROM DRSDR UIEA2019090605451Retainer · crackedRT ENG 7 O'CLOCK POSITION SEAL RETAINER CRACKED AND A SECTION WAS MISSING. REMOVED & REPLACED SEAL RETAINER IAW AMM 71-00-00.SDR ASAA2019083030596Blade · damagedWHILE ACCOMPLISHING T/C 78472010 # 2 ENG S/N 804247 FOUND CU NI IN COATING DAMAGE BEYOND LIMITS ON BLADE #14 & # 23. GROUNDED - YES. REPLACED DAMAGED BLADES AND BLADE PAIRS.SDR ASAA2019082930600Actuator · failed#1 ENG RT VSV ACTUATOR LEAKING. GROUNDED - YES. RIGHT VSV ACTUATOR REMOVAL UP TO 5.F(1) REF AMM TASK 75-31-01-000-802-F00. COMPLETED REMOVAL OF RIGHT VSV ACTUATOR ON #1 ENGINE REF AMM 75-31-01-000-802-F00. REPLACED RIGHT VSV ACTUATOR ON #1 ENGINE PER TASK 75-3SDR WI5R2019082200001Blade · fracturedWHILE TROUBLE SHOOTING FOR A REPORTED UNUSUAL VIBRATION IN FLIGHT, A BORESCOPE INSPECTION DISCOVERED A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR HALA2019082000346Compressor · damagedETOPS SIGNIFICANT SYSTEM - DURING PDC, FOUND #2 ENG LP COMPRESSOR BLADE ATTRITION LINING TO BE DISBANDED FROM LP COMPRESSOR FRONT CASE.// REMOVED AND REPLACED ENGINE #2 PER TASK CARD 7100-9401-02-HAL. OPS AND LEAK CHECK OK. OK FOR SERVICE. FUNCTIONAL CHECK FLISDR UIEA2019081505175Blade · damaged#2 ENG LE FAN BLADE DENT MARKED WITH DOT.(<P>UPON FURTHER EVALUATION, FOUND DAMAGE TO BE NICK IN AREA "D" OF BLADE WITH ALLOWABLE DAMAGE TO 0.060". MEASURED 0.040". ASSET # 0017552 WITHIN ALLOWABLE LIMITS IAW AMM 72-31-02. NO ACTION REQUIRED.</P>)SDR AALA2019081549011Actuator · failedAIRCRAFT WAS GROUNDED: PILOT REPORTS ON INITIAL TAKEOFF ROLL FLEX POWER, ENG 2 COMPRESSOR VANE ECAM. REJECTED TAKEOFF LESS THAN 80 KTS. MAINTENANCE REPORTS IAW TSM 75-30-00-810-846-A13 & 844-A13 AND 853-A. ACCOMPLISHED SUP INFO FLOW CHART. FAULT CODE SVATK 3 TSDR UIEA2019081635046Packing · leakingFOUND ENG SN:707422 NO. 1 BEARING MANIFOLD OIL LEAK.(<P>REPLACED NO. 1 BEARING MANIFOLD PACKING. PERFORMED ENG IDLE RUN LEAK CHECK. RESULT CONDITION CHECK NORMAL AND NO LEAK FOUND IAW 72-31-03-004-001 & 72-31-03-404-005.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>PSDR AALA201908129016Actuator · intermittentAIRCRAFT WAS GROUNDED: PILOT REJECTED TAKEOFF DUE TO ECAM "ENGINE 1 COMPRESSOR VANE". MAINTENANCE TROUBLESHOT IAW TSM 75-30-00-810-852-A. VSV SYSTEM INTERACTION ISSUE ON ENG 1. FOUND THE VSV ACTUATOR INTERMITTENTLY FAULTY. REMOVED AND REPLACED THE VSV ACTUATOR
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