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.

SDR HALA2011112600542Blade · damagedETOPS SIGNIFICANT SYS - NR 2 ENGINE NR 1 FAN BLADE HAS SMALL NICK. BLENDED IAW AMM 72-31-02, NR2 ENG FAN BLADE NR1, PERFORMED EDDY CURRENT INSP, NO CRACK INDICATIONS NOTED. BLENDED IAW AMM 72-31-02, NR 2 ENG FAN BLADE NR 1, PERFORMED EDDY CURRENT INSP, NO CRNov 26, 2011 · N588HA · Boeing 7673CBSDR CA111128007Compressor · damaged(CAN) SIGNIFICANT ENG VIBRATION ON DEPARTURE, NR 2 ENG SHUTDOWN. ACFT DIVERTED, EMER DECLARED WITH ATC, CFR ON STANDBY. FLIGHT DEPARTED & THE ENG SURGED MULTIPLE TIMES AT 13 000 FT, WITH AUDIBLE BANGS & SMOKE, & LOSS ABOUT 40% OF POWER. THERE WERE NO ENG PANov 23, 2011 · Emb ERJ190100IGWSDR HALA2011111900535Blade · nickedETOPS SIGNIFICANT SYS - NICK ON NR 24 BLADE NR 1 ENGINE, 6.5" FROM TIP, ZONE C, .3125 X .7500 OF AN INCH. BENDED NR 24 BLADE IAW MM. BLENDING FPI 9006-3, NR 2. INSPECTED AND FOUND NO INDICATIONS. COMPLIED WITH TEST 11 IAW AMM 71-00-00-700-838-A. ENGINE VIBNov 19, 2011 · N384HA · Airbus A330243SDR HALA2011111900534Blade · nickedETOPS SIGNIFICANT SYS - NICK ON NR 1 ENGINE BLADE NR 19, 20.75" FROM THE TIP, ZONE B .1875 X .038 OF AN INCH. BLENDED NR19 FAN BLADE IAW MM. BLENDING, FPI IAW PS 900-6-3 NR 2. INSPECTED AND FOUND NO INDICATIONS, ER A-43-497939-14 REV A COMPLETED. OK FOR SERNov 19, 2011 · N384HA · Airbus A330243SDR FDEA201111184968Compressor · stalledAT ROTATION NR 1 ENG COMPRESSOR STALLED. HEARD A LOUD BANG WITH YAW AND TEMP AT 1097 DEGREES. N2 INDICATION HAD AN X WITH NO INFORMATION SHOWING. REMOVED AND REPLACED THE ENGINE.Nov 18, 2011 · N68050 · Doug MD1010FSDR AALA20111117AFW01Sleeve · debondedRIGHT ENGINE LP COMPRESSOR CASE KEVLAR WRAP AT THE 5 TO 7 POSITION AFT ADGE OF THE TEFLON SLEEVE DISBONDING. ACCOMPLISHED REPAIR PER EA ENGN-72-020363 ACCOMPLISHED.Nov 16, 2011 · N783AN · Boeing 777223SDR ASAA11510670Shim · wornCOATING WORN ON NR 2 ENG FAN BLADE SHIMS. ON NR 2 ENGINE 24 EA FAN BLADE SHIMS P/N 340 252 307 0 ARE NOW INSTALLED REF T/C 78472002.Nov 15, 2011 · N517AS · Boeing 737890SDR HALA2011114000517Blade · damagedETOPS SIGNIFICANT SYS - ON OVERNIGHT CHECK, FOUND NR 2 ENGINE, NR 33 BLADE FR. INDEX ON SPINNER HAS FOD DAMAGE. ACCOMPLISHED AMM 72-31-02, NR 2 ENGINE NR 33 BLADE FROM INDEX ON SPINNER.Nov 14, 2011 · N596HA · Boeing 767332SDR HALA2011111100516Blade · damagedETOPS SIGNIFICANT SYS - FOUND .2500 X .2500 BLADE DAMAGE ON NR 2 ENGINE FAN. IAW AMM 72-31-02-801 WITHIN LIMITS AREA B, 4" BELOW BLADE SHROUD. BLENDED IAW AMM 72-31-02-801. OK FOR SERVICE.Nov 11, 2011 · N596HA · Boeing 767332SDR CALA2011111100728Plug · out of positionUPON OPENING NR 2 ENGINE COWLING FOUND HPC STAGE 4 BORESCOPE PLUG "F" LAYING IN T/R HALF. REF L/P 8977608 AND L/P 8977609 FOR INSTALLATION OF BORESCOPE PLUG AND T/R THRUST LINK COVER. FOUND INSULATION BLANKET TORN AND MISSING PIECES. REPLACED INSULATION BLANov 11, 2011 · N78004 · Boeing 777224SDR UALA2011111006148Guide Vane · damagedRIGHT ENGINE MULTIPLE EXIT GUIDE VANES DAMAGED AT THE 4 O'CLOCK TO 7 O'CLOCK POSITIONS. MAINT TEXT: TWO ADJACENT FAN EXIT VANE BETWEEN 4:00 AND 5:00 REMOVED, AN ADDITIONAL VANE REMOVED AT 6:00 POSITIONS. VANES TO BE REPLACED NO LATER THAN NEXT ENGINE SHOP VINov 9, 2011 · N646UA · Boeing 767322SDR UALA2011110305973Compressor Blade · damagedBOTH ENGINES HAVE NUMEROUS SMALL NICKS IN LEADING EDGE OF FAN BLADES. NR 2 ENG (SER # 727119) HAS A 11TH STAGE COMPRESSOR BLADE WITH TWO DENTS APPROX 3-4 INCHES FROM TIP. THE FIRST DENT IS .053 IN LONG BY .030 DEEP, THE SECOND DENT IS .041 LONG BY .025 DEEP.Nov 3, 2011 · N534UA · Boeing 757222SDR UALA2011110305972Compressor Blade · out of limitsENG 1 FAN BLADE TAP TEST OUT OF LIMITS AT ONE BLADE. DURING NR 1 ENGINE FAN BLADE TAP INSPECTION FOUND ONE COMPRESOR FAN BLADE OUT OF LIMITS. VALUE OBTAINED 1880 DB SEC. REPLACED FAN BLADE NBR 9 PER AMM AND ACPD FAN BLADE REDISTRIBUTION AS PER ENG CONTROLLERNov 3, 2011 · N823UA · Airbus A319131SDR AALA20111030TUL02Compressor · stalledTUL - CREW REPORTED LEFT ENGINE COMPRESSOR STALLED DURING DECELERATION. MULTIPLE, RAPID POPS WERE HEARD. LEFT EXHAUST GAS TEMPERATURE WAS HIGHER THAN RIGHT BUT NOT OUT OF LIMITS. EMERGANCY DECLARED FLIGHT RETURNED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOOct 30, 2011 · N351AA · Boeing 767323SDR VNAA2011102800025Compressor · stalledCREW REPORTED LOUD BANG (COMPRESSOR STALL) AND HIGH ITT FROM RIGHT ENGINE ON TAKEOFF FROM DCA. CREW SHUT DOWN ENGINE AND DIVERTED TO IAD. MAINTENANCE INSPECTED RIGHT ENGINE AND DETERMINED REMOVAL AND REPLACEMENT OF ENGINE REQUIRED. REMOVED AND REPLACED RIGHOct 25, 2011 · N213PS · Cndair CL6002B19SDR SWAA117355Compressor · stalledDIVERSION/INFLIGHT SHUTDOWN/DECLARED EMERGENCY. ON DESCENT NR 1 ENGINE SEVERAL COMPRESSOR STALLS WITH ENGINE ROLL BACK. SHUTDOWN ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER MT.Oct 25, 2011 · N515SW · Boeing 7375H4SDR UALA2011102505772Blade · nickedAPPEARS TO BE MULTIPLE NICKS ON SEVERAL FAN BLADES OF RT ENG AT 2-3 O'CLOCK POS FACING AFT. INSPECTED BLADES AND FOUND NUMEROUS BLADES WITH MINOR NICKS IN AREAS 2 AND 8. REPAIRED FIRST STAGE FAN BLADE PER AMM. ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT 72Oct 24, 2011 · N562UA · Boeing 757222SDR CALA2011102400684Plug · missingWHILE PERFORMING T/S ON NR 1 ENG, FOUND DAMAGE ON LEFT T/R FIRE BLANKET ALSO FOUND HIGH PRESS COMPRESSOR BOROSCOPE PLUG MISSING ON LEFT SIDE (8TH STAGE VANE H.P.C ROTOR). INSTALLED REPLACEMENT BOROSCOPE PLUG (J) PER AMM 72-00-00-290 812-G00, (NOTE) FIRE BLANKOct 24, 2011 · N78009 · Boeing 777224SDR SIMA201128702Compressor Blade · damagedON FLIGHT 3762 THE CREW REPORTED THAT AFTER TAKEOFF A BIRD STRIKE WAS NOTED. THE RIGHT ENGINE HAD VIBRATION AND WENT INTO YELLOW AND THEN WENT BACK TO GREEN. THE FLIGHT ATTENDANT REPORTED A SMOKE ODOR. THE CREW DECLARED AND EMERGENCY AND RETURNED TO IAH. Oct 13, 2011 · N533AE · Cndair CL6002C10SDR UALA2011101305559Compressor Blade · bentINGESTED RED TAIL HAWK IN RT ENGINE. DURING INSPECTION BIRD STRIKE OF RT ENG FOUND ONE FAN BLADE TIP BENT OUT OF LIMITS. REMOVED DAMAGED BLADE AND 2 OTHERS TO FACILITATE REPAIR TO ACOUSTIC LINING BEHIND FAN BLADES. REPLACED DAMAGED BLADE AND OPPOSITE AND REOct 13, 2011 · N548UA · Boeing 757222SDR UALA2011101105520Liner · damagedNR 1 ENGINE FAN EXIT LINER SEGMENT AT 4 O'CLOCK POSITION OUTER LAYER PEELING BACK. REMOVED ALL LOOSE OUTER MESH. ACCOMPLISHED TAP TEST OF LINER SEGMENT, NO DELAMINATION OR ANY OTHER DAMAGE FOUND. CHECKED ALL FASTENERS, ALL SECURE. OK TO CF AS PER EVA- 8138Oct 10, 2011 · N786UA · Boeing 777222SDR CA111007001Compressor · stalled(CAN) WHILE ON FINAL APPROACH TO A WELL SITE, THE PILOT HEARD A LOUD BANG FOLLOWED BY A SEVERE AIRFRAME VIBRATION. AN AUTOROTATION WAS INITIATED AND A NORMAL LANDING ENSUED WITH NO FURTHER INCIDENT. THE ACFT WAS INSPECTED BY MX PERSONNEL BUT NO APPARENT DEFEOct 5, 2011 · Snias AS350DSDR CALA2011100400634Compressor · stalledAFTER TAKEOFF EXPERIENCED (LEFT) ENGINE SURGE/COMPRESSOR STALL W /EXCEDENCE OF EGT (941) AT 800FT-RETARDED THRUST LEVER COMPRESSOR STALL STOPPED. R&R#1 ENG PER WORK CARD 19-7100-1-0900 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1467730 S/N OFF 01526 IPC REFEROct 1, 2011 · N17133 · Boeing 757224SDR UALA2011093005304Blade · nickedNR 1 ENGINE HAS 2 BLADES NICKED. BLENDED BLADES.Sep 29, 2011 · N648UA · Boeing 767322SDR UALA2011092905280Blade · crackedDURING HFEC INSPECTION FOUND CRACK IN THE MIDSPAN SHROUD ON BLADE NR 1 AND NR 3 IN NR 1 ENGINE. REPLACED NR 1 ENGINE FAN BLADES NR 1 & 19 NR 3 & 21.Sep 29, 2011 · N644UA · Boeing 767322SDR REXA201100641Blade · lack of lubeLT ENGINE FAN VIBE. LUBE FAN BLADES IAW AMM PERFORM GROUND FAN VIBE, OPS CHECK GOOD.Sep 29, 2011 · N147PQ · Cndair CL6002D24SDR CA110930012Blade · missing(CAN) TWO STATOR BLADES FOUND MISSING ON THE 6TH STAGE OF THE COMPRESSOR HALVES.Sep 27, 2011 · Bell 206LSDR UALA2011092705211Blade · damagedDURING LANDING, NR 1 ENGINE INGESTED WHAT APPEARS TO BE FLOCK OF BIRDS. HIT TWO HAWKS ON RUNWAY JUST WHEN APPLYING REVERSE. FELT THUMPS THEN NOTICED LEFT ENGINE HAD DIED. ALL BLADES & INLET DAMAGE. NR 2 ENGINE HAS MULTIPLE BLADE DAMAGE.Sep 26, 2011 · N526UA · Boeing 757222SDR CA110926004Modulator · unserviceable(CAN) PILOT REPORTED INCREASE IN COMPRESSOR SPEED AND DROP IN ROTOR RPM ON APPROACH. PILOT MANAGED TO LAND WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND THE AIRFLOW MODULATOR DEFECTIVE DUE TO A BROKEN BLEED AIR TRANSFERT TUBE.Sep 23, 2011 · Snias AS350BASDR UALA2011092305155Blade · nickedLEFT ENGINE FOUND NICKS ON SEVERAL FAN BLADES. REF MM 72-31-02 PAGE 612. BLENDED BLADES LEFT ENGINE REF MM.Sep 23, 2011 · N532UA · Boeing 757222SDR UALA2011092605179Blades · nickedLEFT ENGINE FOUND NICKS ON SEVERAL FAN BLADES. CHECKED AND FOUND 3 BLADES ON LEADING OF BLADE ON NR 2 INDEX AREA. BLENDED BLADES LEFT ENGINE.Sep 23, 2011 · N532UA · Boeing 757222SDR UALA2011092605160Blades · nickedON LEFT ENGINE FAN, FOUND NICKS ON SEVERAL BLADES. CHECKED FOUND 3 BLADES ON LEADING OF BLADE ON NUMBER TWO INDEX AREA. ACCOMPLISHED EDDY CURRENT INSPECTION OF BLENDED FAN BLADES ON NR 1 ENG PER MM. NO CRACKS FOUND. ACCOMPLISHED FINAL BLEND OF BLADES.Sep 23, 2011 · N532UA · Boeing 757222SDR DXTA2011092604737Blade · bentAT THE MOMENT OF GEAR RETRACTION ON TAKEOFF, HEARD A LOUD POP AND A HUMMING NOISE BEGAN, GOT A MASTER WARNING AND AN ENGINE VIBRATION R CAS MESSAGE. PULLED THE POWER BACK AND THE CAS MESSAGE EXTINGUISHED. FOUND BENT FAN BLADE ON RT ENGINE. SUSPECT BIRD INGESep 23, 2011 · N387QS · Cessna 680CESDR ASAA11510401Balance Weight · out of toleranceNR 1 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION LEVELS TO BE TRENDING HIGHER THAN EXPECTED CURRENT LEVELS NEAR 1.2 UNITS. ACCOM FIM TASK 71 00 00 750 803 F00 TEST 14B. VERIFIED WGHT INSTALLED ON NR 1 ENG MATCHED WITH AVM WGHT CONFIG. USED LAST FLISep 22, 2011 · N577AS · Boeing 737890SDR IXXA110061OFan · lack of lubeDURING TAKEOFF ROLL, THE LT ENGINE FAN VIBRATION 2.5. WHEN INFLIGHT AT 370 ENGINE VIBRATION IS 5.1. THE CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FAN LUBE IAW AMM 72-31-02. AFTER FAN LUBE ENGINE VIBRATION AT .9, WITH IN LIMITS IAW ERSep 21, 2011 · N763CX · Boeing 767232SDR CA111013005Link · broken(CAN) ACFT EXPERIENCED COMPRESSOR STALLS WHILE ON APPROACH. FORCED LANDING CARRIED OUT AT ALTERNATE LANDING LOCATION. PINS (LINKS) ON FLOW FENCE RING FOUND BROKEN. FLOW FENCE RING FOUND TO HAVE GROOVED COMPRESSOR HSG.Sep 19, 2011 · Snias AS350B2SDR ASAA11510393Screw · out of toleranceNR 1 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION LEVELS TO BE TRENDING HIGHER THAN EXPECTED CURRENT LEVELS NEAR 1.2 UNITS. ACCOMPLISHED ON NR 1 ENG ON BOARD FAN TRIM REF MM 71 00 00 750 803 FOO. FOLLOWING BALANCE WEIGHT CHANGES: NR 10 PO11 TO P07 NSep 19, 2011 · N581AS · Boeing 737890SDR HALA2011091400401Blade · nickedETOPS SIGNIFICANT SYS - NR2 ENG NR 10 BLADE AREA A AT TIP IS NICKED. BLEND OUT DAMAGED AREA ON TIP OF NR 2 ENG NR 10 BLADE, WITHIN LIMITS IAW MM 72-31-02. PERFORMED FLORESCENT PENETRANT INSP AND HIGH FREQ EDDY CURRENT INSP, IAW AMM 72-31-02. NO CRACK FOUND.Sep 14, 2011 · N582HA · Boeing 76733ASDR CA110928003Compressor · malfunctioned(CAN) DURING CLIMB THROUGH FL300, A THUMPING NOISE WAS HEARD AND THE ACFT STARTED TO "FISHTAIL". THE CREW OBSERVED A HIGH TEMPERATURE ON THE RT ENGINE AND A "HOT" SMELL IN THE CABIN. THE POWER WAS REDUCED TO APPROX 50 PERCENT WHICH TOOK CARE OF THE TEMPERATUSep 13, 2011 · Cessna 560XLSDR CA110908003Compressor · failed(CAN) THE OPERATOR HAD A COMPLAINT OF LOW POWER. UPON DISMANTLE OF THE COMPRESSOR THE FOLLOWING CONDITIONS WERE FOUND. COMPRESSOR CASE CORRODED, MISSING PLASTIC AND CRACKED PLASTIC. 1ST STAGE COMPRESSOR WHEEL, CHAMFER BLEND BEYOND LIMITS. 2ND/3RD STAGE CSep 8, 2011SDR HALA2011090800399Blade · bentETOPS SIGNIFICANT SYS - NR 2 ENGINE 1 FAN BLADE BENT ON L/E .3750" FROM TIP, 2" LONG. BEND IS .1250" IN DEFLECTION AFT. R & R NR 5 AND 24 FAN BLADE IAW AMM 72-31-02-004-001 N00. PERFORMED TEST 8 VIBRATION SURVEY IAW AMM 71-00-00-725-008-N00. NO TROUBLE FOUNSep 8, 2011 · N583HA · Boeing 76733ASDR CA110915002Bearing · faulty(CAN) ON A RUNNING TEST RUN ENGINE NR 1 LOST HP AND TIT STARTED TO RAPIDLY CLIMB, PILOT E-HANDLE, LANDED WITH NR 1 ENGINE FEATHERED. ON GROUND INSPECTION, THE COMPRESSOR BLADES WERE RUBBING AGAINST THE CASE. SUSPECT FAULTY BEARING.Sep 7, 2011 · Cvac 440SDR MASA2011090563639Pin · defectiveNR 2 ENGINE 1.9 VIBE CRUISE FL 350. R2 ALL BLAD PINS AND PERFORMED FAN BLADE LUBE.Sep 5, 2011 · N917FJ · Cndair CL6002D24SDR ASAA11510338Shim · wornNR 2 ENGINE FAN BLADE LUBE 1EA FAN BLADE PLATFORM AND 24 FAN BLADE SHIMS REQUIRE REPLACEMENT. 1EA FAN BLADE PLATFORM MFG P/N 340 001 8YY 0 ARE INSTALLED 24EA FAN BLADE SHIMS MFG P/N 340 252 302 0 ARE INSTALLED ON NR 2 ENGINE.Sep 3, 2011 · N532AS · Boeing 737890SDR ASAA11510337Shim · worn23 EACH FAN BLADE SHIMS COATING WORN NR1 ENG. REPLACED 23 EACH FAN BLADE SHIMS NR 1 ENG. REF TASK CARD 78472002.Sep 1, 2011 · N519AS · Boeing 737890SDR HEEA20110830002Diffuser · separatedENGINE WAS REMOVED DUE TO CYCLED WHEELS. COMPRESSOR DISASSEMBLED DUE TO CRACKED SCROLL. DIFFUSER FOUND TO HAVE SEPARATED PLATE. REPLACED DIFFUSER.Aug 30, 2011 · N206FS · Bell 206L3SDR MASA2011082903593Fan Blade · lack of lubeENG 2 FAN VIBE 1.8 AT FL340;C/W FAN BLADE, TANG & PIN LUBE, OPS CHECK AT MAX PWR IS 0.1.Aug 27, 2011 · N912FJ · Cndair CL6002D24SDR CA111109006Compressor · stalled(CAN) DURING A TEST FLIGHT, AFTER THE ENGINE WAS REPAIRED FOR COMPRESSOR STALLS, WE EXPERIENCED ONE MINOR STALL. WE THEN BEGAN TO RETURN TO BASE WHEN THE ENGINE EXPERIENCED A SERIES OF RAPID STALLS, THE TOT INCREASED OVER 900 DEGREES, ENGINE POWER WAS DEGRADAug 26, 2011 · Bell 206L1SDR ASAA11510296Shim · wornNR 2 ENG FAN BLADE SHIMS RUBSTRIP WORN OFF ALL 24 BLADES. REPLACED ALL 24 FAN BLADE SHIMS FOR ENG NR 2 PER TASK CARD 78472002 24.Aug 24, 2011 · N531AS · Boeing 737890SDR CA111109005Compressor · stalled(CAN) PILOT REPORTED THE ENGINE ASSY WAS EXPERIENCING MINOR COMPRESSOR STALLS. THIS WOULD OCCUR ON APPROCH TO LANDING, ABOVE 5000 FT. THE COMPRESSOR ASSY WAS REMOVED AND SENT FOR INVESTIGATION.Aug 21, 2011 · Bell 206L1
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