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 WI5R201902010001Rotor · fracturedDURING FINAL APPROACH, THE CUSTOMER REPORTED A 'BANG' WITH AN ACCOMPANIED YAW. FIELD TROUBLESHOOTING SUGGESTED A MISSING IPC BLADE AND POTENTIAL DAMAGE TO COMPONENTS DOWNSTREAM OF THE IPC ROTOR. DISASSEMBLY OF THE ENGINE IN THE REPAIR STATION CONFIRMED FIELD FSDR CA190220016Compressor · failed(CAN) CREW REPORTED A LOUD BANG AND VIBRATION FELT BY THE CREW AND PASSENGERS JUST AFTER TAKE OFF AT APPROXIMATELY 1500` AGL, WHILE THE LANDING GEAR WAS IN TRANSIT. NO ABNORMAL INDICATIONS OR CAS MESSAGES RECEIVED, AND NO OBVIOUS SIGNS OF FOD STRIKE. LH ENGINESDR VE7A201902050001Bearing Seal · leakingABOUT 10 MINUTES IN CRUISE FLIGHT, LIGHT SNOW WAS NOTED AND THE OAT WAS AROUND 0 SO I TURNED ON THE ENGINE ANTI-ICE AND PITOT HEAT. APPROXIMATELY 2 MINUTES AFTER THE SWITCHES HAD BEEN TURNED ON, LIGHT SMOKE WAS OBSERVED IN THE CABIN. AS THE DETERMINATION TO WHSDR SWAA2019020129114Compressor · stalledAIR RETURN, NR 1 ENGINE COMPRESSOR STALL IN CLIMBOUT. R&R NR 1 ENGINE PER MT.SDR ASAA2019012927979Blade · damagedWHILE ACCOMPLISHING TC 78472002, FOUND NR 12 BLADE ON NR 2 ENGINE MISSING CU-NI OUTSIDE OF AREA "X" ON FWD CONVEX SIDE PRESSURE FACE. GROUNDED - YES. REPLACED NR 12 BLADE AND NR 24 BLADE ON NR 2 ENG.SDR ASAA2019012827968Spacer · debondedNR 1 ENG FAN LUBE, FOUND SPACERS AT NR 7, NR 18, NR 24 TO BE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED FAN BLADE SPACERS AT NR 7, NR 18, AND NR 24 IAW T/C 78472010.SDR ASAA2019012427914Seal · missingREF T/C 78472010 NR 2 ENGINE FAN BLADE LUBRICATION. FOUND PLATFORMS MISSING RUBBER SEALS BEYOND LIMITS. P/N: 340-001-816-0. 24 EACH. GROUNDED - YES. REPLACED ALL PLATFORMS ON NR 2 ENGINE FAN PER T/C 78472010.SDR ASAA2019012427913Blade · crackedWHILE ACCOMP T/C SBCFM56-7B-72-1033-1, FAN BLADE ROOT ULTRASONIC INSPECTION FOUND BLADE NR 3 S/N DD453914-J 32% INDICATION 5.25" FROM LE CONVEX SIDE. BLADE NR 11 S/N DD454177-5 31% INDICATION 1.25" FROM LE CONVEX SIDE. ALL BEYOND 30% REJECT, ENGINE NR 2 S/N 89SDR ASAA2019012427912Shim · wornDURING FAN LUBE ALL NR 2 ENGINE FAN BLADE SHIMS HAVE WEAR. GROUNDED - YES. REPLACED ALL NR 2 ENGINE SHIMS PER T/C 78472010.SDR AALA201902019022Sensor · malfunctionedRT ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS, WHEN ADVANCING POWER FROM FLIGHT IDLE TO POWER, OCCURRED THREE TIMES. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE RIGHT ENGINE, ENGINE CONTROL IAW SIC 73-94-02 AND CIT SENSOR IAW AMM 73-21-02. MAINTSDR AALA2019012549001Actuator · faultedNR 2 ENGINE COMPRESSOR VANE LIGHT ECAM STAYED ON LONGER THAN 60 SECONDS AND DID NOT GO OUT UNTIL ENGINE SHUTDOWN. REJECTED TAKEOFF AT LESS THAN 80 KNOTS. THE AIRCRAFT WAS GROUNDED. MAINTNEANCE PERFORMED TROUBLESHOOTING IAW TSM 75-30-00-810-844-A, AND REPLACSDR JYDR20190124023Disk · crackedENGINE WAS AT REPAIR STATION FOR OVERHAUL. NDT WAS COMPLIED WITH ON THE 3RD STAGE DISK REFERENCE OIS 352 REV N, 3/3/2015. 7EA. CRACK INDICATIONS WERE FOUND FROM A TIE-ROD HOLES USING EDDY CURRENT (REF SPM 585005 REV 143, 01/JUN/2018). THERE WERE 0 CRACK INDISDR ASAA2019012227898Blade · damagedNR 2 ENGINE FAN BLADES 2,3,18,23 AND 24 CU NI COATING DAMAGED BEYOND LIMITS. GROUNDED - YES. REPLACED DAMAGED BLADES AND ASSOCIATED PAIR PER TASK CARD.SDR ASAA2019012127897Case · corroded2 ENG INLET AND FAN BLADES-DETAILED INSPT. FOUND 24 EACH NUTPLATES HAVE CORROSION UNDER THEM ON O/B AFT SECTION OF FAN CASE FROM 2:30 TO 11:00 O'CLOCK POS. ALF. GROUNDED - YES. REMOVED AND REPLACED ENGINE.SDR WI5R2019012300001Rotor · fracturedDURING TROUBLESHOOTING FOR A REPORTED COMPRESSOR STALLS DURING FLIGHT AND RAPID ITT INCREASE, A BORESCOPE INSPECTION REVEALED SOME MISSING IPC BLADES AND FOD DAMAGE TO COMPONENTS DOWNSTREAM OF THE IPC ROTOR. DISASSEMBLY CONFIRMED 6 MISSING BLADES.SDR 2019FA0000023Compressor · damagedPILOT REPORTED A LOUD BANG SOUND FOLLOWED BY AIRCRAFT YAWING ON APPROACH. AFTER LANDING, THE RIGHT ENGINE FAN WAS TURNED THROUGH BY HAND AND A METAL TINGING SOUND COULD BE HEARD. BORESCOPE INSPECTION REVEALED MISSING IP COMPRESSOR BLADE MISSING. THIS IS THE 3RSDR ASAA2019011727966Fan · out of balance2 ENGINE TREND DATA SHOWS AN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES FAN LUBE REQUIRED. GROUNDED - YES. ACCOMPLISHED T/C 78472002 ON NR 2 ENG. REPLACED ALL PLATFORMS, SHIMS AND NR 12 AND 24 BLADES. REMAPPED BLADES PER BLAMAP VERSDR WI5R201901170001Rotor · fracturedDURING TROUBLESHOOTING FOR A REPORTED N1 SLOW ROTATION, A BORESCOPE INSPECTION REVEALED A MISSING IPC BLADE AND FOD DAMAGE TO COMPONENTS DOWNSTREAM OF THE IPC ROTOR. INSPECTION OF THE ENGINE IN THE REPAIR STATION HAS CONFIRMED THE CONDITION.SDR ASAA2019011627817Shim · wornNR 2 ENG FAN BLADE SHIMS COATING WORN OUT OF LIMITS. GROUNDED - YES. REPLACED ALL BLADE SHIMS ON NR 2 ENGINE FAN.SDR ASAA2019011627816Blade · damagedNR 2 ENGINE NR 8 FAN BLADE HAS BLADE ROOT CU-NI DAMAGE OUT OF LIMITS. BLADE SN DM094190-F. GROUNDED - YES. REPLACED NR 8 FAN BLADE AND ITS PAIR NR 20 PER AMM 72-21-02-000-802.SDR 2019FA0000009Compressor · damagedPILOT REPORTED LEFT ENGINE START SLIGHTLY SLOWER THAN NORMAL ACCOMPANIED BY ABNORMAL SOUND. ALL ENGINE PARAMETERS WERE NORMAL AND A TAKEOFF POWER CHECK WAS GOOD. THE AIRCRAFT WAS FLOWN TO MAINTENANCE BASE AND PILOT NOTED ONLY A VERY SMALL SPLIT IN ITT INDICATISDR JYDR20190107007Tab · brokenENGINE WAS AT REPAIR STATION FOR SCHEDULED OVERHAUL. DURING TEAR DOWN A BROKEN TAB LOCK WAS DISCOVERED ON THE 4TH STAGE COMPRESSOR DISK. THIS CAUSED THE 4TH STAGE BLADE TO SHIFT AND RUB ON THE 4TH STAGE STATOR. THIS REPAIR STATION PREVIOUSLY SUBMITTED AN SDR, SDR WI5R2019010700001Rotor · fracturedDURING PRE-BUY INSPECTION A MISSING 3RD STAGE IP ROTOR BLADE WAS DISCOVERED. DISASSEMBLY OF THE ENGINE CONFIRMED TWO MISSING 3RD STAGE BLADES.SDR AALA201901059002Engine · malfunctionedAIRCRAFT WAS GROUNDED: CLIMBING THROUGH 30,000, 2 BANGS HEARD AND ECAM MESSAGE DISPLAYED COMPRESSOR STALL NR 2 ENGINE. EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED #2 ENGINE AND PERFORMED SATISFACTORY OPERATIONAL CHECK.SDR SWAA2019010928193Vane · crackedDURING BOROSCOPE INSPECTION FOUND APPROXIMATELY 3 CRACKED ON STAGE 1 LOWER PRESSURE TURBINE NGV 1 SEG W/4 VANES CRACKED 3 SEG. R&R NR 2 ENGINE PER MT.SDR COZA20190106126Bushing · broken10EA VARIABLE STATOR VANE SECOND STAGE ACTUATOR BUSHINGS FOUND MISSING OR BROKEN ON ENGINE. ENGINE REMOVED AND SENT TO SHOP.SDR AALA201901039018Blade · damagedCLIMBING THORUGH 30,000 FT, TWO BANGS, ECAM COMPRESSOR STALL ON THE NR 2 ENGINE. FOLLOWED ECAM/ECAM CLEARED. THE AIRCRAFT WAS GROUNDED. REPLACED THE 2 ENGINE IAW JC 26L40071001. INSPECTION REVEALED DAMAGE TO MULTIPLE STAGES OF HIGH PRESSURE COMPRESSOR BLSDR AALA201901029004Actuator · faultedNR 2 ENGINE COMPRESSOR VANE ECAM MESSAGE DISPLAYED DURING TAKEOFF. WARNING REMAINED FOR MORE THAN 60 SECONDS, FLIGHT REJECTED TAKEOFF AT 90 KIAS. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED VSV ACTUATOR ON THE NR 2 ENGINE IAW JC 26T40075005, AND PERFORMSDR UIEA2018122602940Spinner · worn#2 ENGINE SPINNER REQ REPAINT AS PER CUSTOMER REQ.(<P>REMOVED,PAINTED & REINSTALLED #2 ENGINE SPINNER IAW B767 AMM 72-31-01 & ENGINE MANUAL (GEK 92451) TASK 72-21-10-300-802-0.</P>)SDR AALA2018042419924Shroud · separatedAIRCRAFT WAS GROUNDED: ON TAKEOFF ROLL, JUST ACHIEVING TAKEOFF THRUST, AT ABOUT 30 KNOTS, EICAS MESSAGES "ENGINE FAIL RIGHT" AND "ENGINE CONTROL RIGHT" DISPLAYED, AND THERE WAS A LOUD BANG, INDICATING A POSSIBLE COMPRESSOR STALL. FLIGHT ATTENDANTS ALSO REPORTESDR UIEA2018121802873Engine · vibrationDURING CLIMB OUT RT ENGINE VIB 3.6 IN CRUISE 2.1 2.3. PERFORMED TRIM BALANCES PROCEDURRES IAW AMM 72-31-00 WITHIN SERVICEABLE LIMITS.SDR JYDR20181214347Disk · crackedENGINE WAS RECEIVED AT REPAIR STATION FOR HOT SECTION AND AIRWORTHINESS COMPLIANCE (AD) UNDER WO 164822. DURING COMPLIANCE WITH AD 97-02-13 NDT INSPECTION, 2 EACH CRACKS WERE FOUND AT TIE ROD HOLES. AD CALLS FOR FIRST INSPECTION AT 3000 HOURS AND 1500 HOURS THSDR SIMA2018121211003Compressor · contaminatedDURING CLIMB THROUGH APPROXIMATELY 9,000FT VMC AIRCRAFT CLEAN CONFIG NO ICING. M.W. FOR AFT LAV SMOKE ILLUMINATED. PAX AND CREW NOTICED ODOR. ALERT EXTINGUISHED AFTER APPROXIMATELY 1 MINUTE OR SO. ODOR LIKENED TO BURNING EXHAUST. LDG WT UNDER 64,000 #'S.-C/A-NSDR WI5R201812120001Rotor · fracturedDURING TROUBLESHOOTING FOR SUDDEN ITT SPLIT BETWEEN LH AND RH ENGINES, BORESCOPE INSPECTION DISCOVERED A MISSING 3RD STAGE IPC ROTOR BLADE AND POTENTIAL DAMAGE TO THE HPC ROTOR. DISASSEMBLY OF THE ENGINE CONFIRMED A MISSING 3RD STAGE BLADE.SDR UIEA2018121002813Compressor · stalledNR 3 ENGINE COMPRESSOR STALLED 2X AFTER TAKE OFF+ WOULD TEMP OUT AT NORMAL THRUST SETTING. AT IDLE WOULD RUN IN NORMAL PARAMETERS. R&R ENG NR 3.SDR UIEA2018120902804Blades · damagedON WALK AROUND FOUND DAMAGE TO NR 1 ENGINE. REMOVED AND REPLACED COMPLETE FAN SET ON ENGINE NR 1 IAW AMM 72-31-02-4. HIGH POWER ENGINE RUN ACCOMPLISHED. NO FURTHER VIBE FELT.SDR QEMY201811300001Disc · crackedIPC ST 6-7 DISC (UL36824 DN55923 EQUIPMENT 101935052) EXHIBITS 2X HOLES WITH CRACK INDICATIONS. THE 2X HOLES HAD BEEN ENLARGED DURING SB72-9594 EMBODIMENT. DISC IS LIFE RESTRICTED WITH 3 CYCLES AVAILABLE. SB72-9594 WAS EMBODIED AT 2005 VISIT. DISC ROUTED TO MRSDR ASAA2018112327080Elastomer · debondedWHILE ACCOMPLISHING T/C 78472010 ENG NR 1 S/N 896974. FOUND NR 12 FAN BLADE SPACER ELASTOMER DISBONED ON BOTH SIDE. GROUNDED - YES. REMOVED AND REPLACED ON NR 1 ENGINE FAN BLADE SPACER (12) REF T/C 78472010.SDR ASAA2018112327079Blade · wornWHILE ACCOMPLISHING T/C 78472010 FAN LUBE ENG NR 1 S/N 896974 FOUND CU-NI-IN COATING OUT OF LIMITS ON FAN BLADES NR 3 CV SIDE .56, NR 4 CV SIDE .57, NR 8 CV SIDE .6, NR 11 CV SIDE .65, NR 13 CV SIDE .81, & NR 18 CV SIDE .71. GROUNDED - YES. ON NR 1 ENG REMOVEDSDR ASAA2018112327078Blade · damagedBLADE NR 17 ON NR 1 ENGINE HAVE LEADING EDGE TIP CURL. GROUNDED - YES. REMOVED AND REPLACED ON NR 1 ENG BLADE NR 17 AND IT'S OPPOSITE PAIR REF T/C 78472010.SDR ASAA2018112327077Elastomer · tornWHILE ACCOMPLISHING T/C 78472010 ENG NR 1 S/N 896974 FOUND 2 EA PLATFORMS NR 14 & NR 19 ELASTOMER SEALS TORN ON BOTH SIDES. GROUNDED - YES. REMOVED AND REPLACED ON NR 1 ENG 2 PLATFORMS (NR 14 & NR 19). REF T/C 78472010.SDR WI5R201811190001Rotor · fracturedDURING SHUTDOWN AN UNUSUAL SQUEAL WAS NOTED. INVESTIGATION REVEALED THE N1 SPOOL COULD NOT ROTATE AND BORESCOPE INSPECTION DISCOVERED A MISSING 3RD STAGE IP ROTOR BLADE.
DISASSEMBLY OF THE ENGINE CONFIRMED TWO MISSING 3RD STAGE BLADES.SDR HEER201811165403Compressor · stalled#2 ENGINE FAILED FOLLOWING A COMPRESSOR STALL. REPLACED #2 ENGINE DUE TO COMPRESSOR BLADES DAMAGED.SDR AMYR2018111500001Compressor Blade · brokenTROUBLESHOOTING A SUDDEN HIGH ITT SPLIT BETWEEN LT AND RT ENGINE AS REPORTED BY THE PILOT. PER LMM 71-00-00 FAULT ISOLATION FOR HIGH ITT, PERFORMED A BORESCOPE OF HP AND IP COMPRESSOR AND FOUND SIGNIFICANT DAMAGE TO BOTH HP AND IP COMPRESSORS. APPEARS THERE WASDR ASAA2018110826825Pin · missingWHILE ACCOMPLISHING TC SBCFM56-7B-72-0986-1 INSP OF METALLIC HYBRID VSV SYS FOUND HPC STG 3 VSV PIN MISSING AT 3 OCLOCK POSITION WITH FOD DAMAGE BEYOND AMM 72-00-00-200-804-F00 STAGE 3 & STAGE 4, WITH NICKS ON ROTOR SHAFT DUE TO LIBERATION OF PIN. MIG 2C 40-00SDR WI5R201811090001Blade · fracturedDURING TAKE-OFF A LOUD BANG WAS REPORTED. POST FLIGHT BORESCOPE INSPECTION REVEALED A MISSING 3RD STAGE IP BLADE. DISASSEMBLY OF THE ENGINE CONFIRMED ONE MISSING 3RD STAGE BLADE.SDR ASAA2018110426729Spacer · migratedNR 2 ENGINE NR 6 BLADE SPACER HAS MIGRATED OUT. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE, NR 6 FAN BLADE PLATFORM REF AMM 72-21-02/401. REMOVED AND REINSTALLED REAR AND FRONT SPINNER CONE REF AMM 72-21-01/401.SDR AALA2018103109023Actuator · defectiveNR 2 ENGINE COMPRESSER VANE 60-80 KTS REJECT TAKE OFF. THE AIRCRAFT WAS GROUNDED. REPLACED ENGINE 2 VSV ACTUATOR PER JOB CARD 26T40075005. POWER ASSURANCE TEST PER JOB CARD 26L00071014. AIRCRAFT OK FOR SERVICE.SDR WI5R2018102900000Blade · fracturedDURING TAKEOFF, THE PILOT REPORTED A LOUD BANG AND A 50 DEG C ITT SPLIT. BORESCOPE INSPECTION INDICATED A MISSING 3RD STAGE IP BLADE. IN ADDITION, A ZONE 2 ITT EXCEEDANCE WAS RECORDED IN THE FADEC FILES, 915.6 DEG C FOR 2.8 SECONDS. DISASSEMBLY OF THE ENGINSDR ASAA2018102926640Pin · migratedWHILE ACCOMPLISHING METALLIC/HYBRID VSV SYSTEM BORESCOPE INSPECTION (REF TASK CARD SBCFM 56-7B-72-0986-1) FOUND THE NR 3 STAGE 9 O'CLOCK SLAB SIDED PIN TO BE ROTATED AND MIGRATING OUT. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE REF W/O 430266.
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