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 CALA2013100391707Blade · out of limitsDURING ENG 2 FAN BLADE TAP TEST FOUND OUT OF LIMITS BLADE NR 11, WITH 1273 DB. REMOVED & INSTALLED BLADE NR 11 IAW MM.Oct 2, 2013 · N477UA · Airbus A320232SDR CALA2013093091581Inlet Bullet · crackedNR 2 ENG INLET CONE, TWO CRACKS RADIATING FROM TWO SEPARATE BOLTS GREATER THAN .5" IN LENGTH, IN ADDITION TO SEVERAL AREAS OF DELAM. IAW AMM 72-31-01. R & R NR 2 ENG COMPRESSOR INLET CONE IAW AMM 72-31-01, OK TO CONTINUE.Sep 29, 2013 · N567UA · Boeing 757222SDR CALA2013092691499Guide Vane · erodedNR 1 ENG FAN EXIT GUIDE VANES HAVE SEVERAL LE FOIL TAPE REPAIRS ERODED. REPLACED TAPES ON LE GUIDE VANES ON NR 1 ENG.Sep 26, 2013 · N128UA · Boeing 747422SDR CALA2013092591460Blade · damagedRT ENGINE FAN BLADE TIP REPAIRED. NEEDS NDT INSPECTION. REPAIRED AREA TO BE EDDY CURRENT INSPECTED IAW UA NTM PART 6, 72-31-401 WITHIN 6 FLIGHT CYCLES. CURRENT PTC 13948. BLADE NBR 1. ALSO IDENTIFIED WITH WHITE DOT. INSPECTION PERFORMED AMM 72-31-02 PARA Sep 25, 2013 · N660UA · Boeing 767322SDR CALA2013092591457Blade · nickedNR 12 1ST STAGE FAN BLADE ON NR 1 ENGINE HAS 1-16TH INCH NICK 12 INCHES FROM ROOT ON LE. ACCOMPLISHED BLEND REPAIR IAW AMM 72-31-02 & EDDY CURRENT INSPECTION IAW NTM PART 6-72-31-401.Sep 25, 2013 · N648UA · Boeing 767322SDR ASAA2013092596061Shim · wornDURING FAN LUBE OF NR 1 ENG ALL FAN BLADE SHIMS WERE FOUND TO HAVE MOLYDAG COATING WORN BEYOND LIMITS. ACFT GROUNDED. ALL SHIMS, FAN BLADE, NR 1 ENG REPLACED REF T/C 78472002.Sep 25, 2013 · N565AS · Boeing 737890SDR SIMA20130924006Compressor · stalledCREW REPORTED THAT ON INTIAL CLIMB, NR 2 ENGINE HP VIBRATIONS MAXED CLIMBING THROUGH 2000 FT. FELT COMPRESSOR STALL. IMMEDIATELY BROUGHT ENGINE TO IDLE AND INDICATIONS RETURNED TO GREEN. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCISep 24, 2013 · N806AE · Emb EMB135KLSDR DALA13046383723Engine · failedAFTER TAKEOFF, NR 2 ENGINE LOST POWER AND WAS SHUTDOWN. DIVERTED AFTER DECLARING AN EMERGENCY. MX FOUND METAL IN THE TAILPIPE AND TURBINE BLADE LODGED IN L/E OF RT HORIZONTAL STABILIZER. REPLACED NR 2 ENGINE AND RT HORIZONTAL STABILIZER L/E.Sep 20, 2013 · N393DA · Boeing 737832SDR CA130920009Diffuser · cracked(CAN) DURING A ROUTINE MAINTENANCE ACTION, A CRACK WAS DISCOVERED AROUND THE BLEED VALVE PORT. ACFT HAS BEEN REMOVED FROM SERVICE. UP-DATE: CRACK FOUND ON COMPRESSOR DIFFUSER MANIFOLD DURING DI .7500" LENGTH SPLITTING FROM BLEED AIR FITTING WELDED AREA.Sep 19, 2013 · Bell 205A1SDR CALA2013092091303Tape · deterioratedNR 2 ENGINE EXIT GUIDE VANES HAS NUMEROUS REFLECTIVE TAPE DETERIORATING AT LE.Sep 19, 2013 · N668UA · Boeing 767322SDR CALA2013091891266Blade · chippedPOST WALK AROUND INSPECTION FOUND CHIP IN FAN BLADE OF ENGINE 1.Sep 15, 2013 · N478UA · Airbus A320232SDR CA130912006Blades · failed(CAN) ON ENGINE THROTTLE UP FOR TAKE OFF CREW REPORTED A BANG ON NR 2 ENGINE WITH HIGH EGT AND LOSS OF THRUST. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND HP AN LP COMPRESSOR WHEEL/BLADE FAILURE. ENGINE REPLACED.Sep 9, 2013 · Boeing 727225SDR CALA2013090991130Spinner · damagedLT ENGINE SPINNER HAS A PIECE OF MATERIAL MISSING, WITHIN LIMITS IAW AMM 72 31-01 25 HOUR FLYBACK. REPLACED INLET CONE FRONT SEGMENT IAW MM.Sep 7, 2013 · N507UA · Boeing 757222SDR 2013FA0000574Diffuser · crackedENGINE WAS MAKING A HIGH PITCHED NOISE. REMOVED ENGINE ASSY AND DISASSEMBLED. FOUND COMPRESSOR DIFFUSER VANE ASSY CRACKED IN SEVERAL SPOTS AT THE BRAZE JOINTS. THIS PART WAS O/H 529.2 HRS BEFORE. THIS IS THE 3RD VANE ASSY WE HAVE FOUND LIKE THIS. PROBABLESep 6, 2013SDR DALA13042753229Compressor · stalledDURING CRUISE, NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AT APPROXIMATELY 50 PERCENT N1. CREW DECLARED EMERGENCY AND FLIGHT WAS DEVERTED. ACFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED NR 1 ENGINE AND FUNCTIONAL CHECK WAS NORMAL.Sep 5, 2013 · N329NW · Airbus A320211SDR CALA2013082690723Blade · damagedNR 21 FAN BLADE, NR 1 ENGINE, FAILED TRANSIENT ACOUSTIC PROPAGATION TEST PER JOB CARDNR 4-2215. REMOVED & REPLACED NR 21 FAN BLADE PER AMM 72-31-11. PERFORMED NR 1 ENGINE RUNUP VIBRATION TEST PER AMM 71-00-00, VIBRATIONS WITHIN SERVICEABLE LIMITS.Aug 23, 2013 · N470UA · Airbus A320232SDR CALA2013082690721Blade · nickedNR 2 ENGINE FAN BLADE HAS NICK ON LEADING EDGE. BLENDED BLADE PER AMM 72- 31-11. IDT INSPECTION WAS ACCOMPLISHED. NICK WAS ON LEADING EDGE OF BLADE APPROX 1 -32ND OF AN INCH.Aug 23, 2013 · N457UA · Airbus A320232SDR CALA2013082390693Guide Vane · damagedGUIDE VANE AT 12 O'CLOCK POS BOTTOM FILLE, TOP ROW, FWD FASTENER HOLE. NUT PLATE STRIP BROKEN. SPEED TAPE HAS BEEN APPLIED AS AN INTERIM REPAIR IAW EC7233-01321. CHECK TAPE FOR SECURITY AT 2 CYCLE INTERVALS AND PERMANENT REPAIR IN 6 CYCLES. MF3120 CREATED TAug 22, 2013 · N221UA · Boeing 777222SDR 39LA2013082000004Compressor · stalledAT HOVER, MULTIPLE COMPRESSOR STALLS.Aug 19, 2013 · N725JH · Skrsky S61NSDR CALA2013081990510Blade · nickedNR 2 ENGINE FAN BLADE NICKED. ACCOMPLISHED INITIAL BLEND. PERFORMED EDDY CURRENT INSPECTION ON BLENDED FAN BLADES. NO CRACK INDICATIONS FOUND. ACCOMPLISHED FINAL BLEND ON BLADES IAW MM.Aug 18, 2013 · N118UA · Boeing 747422SDR 2013FA0000464Compressor Wheel · crackedCRACK LENGTH OF APPROXIMATELY 2 MM, FOUND ON ROTOR DISC HPC. DETECTED DURING FPI.Aug 12, 2013SDR CALA2013080590166Blade · bentNR 2 ENGINE HAS ONE FAN BLADE WITH L/E TIP BENT. REMOVED .25 CURL FROM FWD L/E TIP AT AREA "A". REMOVED AN ADDITIONAL .020 MATERIAL AFTER EDDY CURRENT INSPECTION.Aug 4, 2013 · N647UA · Boeing 767322SDR CALA2013080590138Blade · nickedNUMEROUS BLADES ON NR 1 ENGINE HAVE NICKS. REPAIRED BLADES IAW AMM, EDDY CURRENT ACCOMPLISHED.Aug 2, 2013 · N562UA · Boeing 757222SDR JYDR2013FA0000421Compressor Wheel · crackedCOMPRESSOR WAS BEING OVERHAULED. DURING NDT CRACKS WERE FOUND AT THE TIE ROD HOLES.Jul 26, 2013 · N154AC · Skrsky S64ESDR JYDR2013FA0000420Compressor Wheel · crackedCOMPRESSOR WAS BEING OVERHAULED. DURING NDT CRACKS WERE FOUND AT THE TIE ROD HOLES.Jul 26, 2013 · N229AC · Skrsky S64ESDR UALA2013072405216Case · crackedNR 2 COMPRESSOR INTERMEDIATE CASE CRACKED. FOUND TO BE AIRWORTHY FOR FERRY FLIGHT. NR 2 ENGINE COMPRESSOR INTERMEDIATE CASE CRACKED AT NR 3 SUPPORT STRUT CLAMP-UP PLATES.Jul 24, 2013 · N665UA · Boeing 767322SDR USAA2013072200017Blade · damagedABOUT 800 FT AFTER TAKEOFF, NR 2 ENGINE STALLED. ALL ENGINE INDICATIONS NORMAL THROUGHOUT FLIGHT. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. FLIGHT LANDED WITHOUT INCIDENT. PERFORMED BORORSCOPE INSPECTION AND DISCOVERED NUMEROUS DAMAGED COMPRESSOR BJul 18, 2013 · N753US · Airbus A319112SDR 2013FA0000416Lock · brokenENGINE REMOVED, DURING DISASSEMBLY MINOR DAMAGE WAS NOTED ON THE BLADES AND VANES AFT IF 5TH STAGE. THE DAMAGE WAS CAUSED BY A 5TH STAGE DISK TAB LOCK THAT HAD BROKEN AND ALLOWED THE BLADE TO MOVE AFT IN THE DISK MAKING CONTACT WITH THE 6TH STAGE STATOR.Jul 18, 2013 · N218AC · Skrsky S64ESDR UALA2013071705024Fairing · damagedDURING TRANSIT WALK AROUND CHECK, FOUND INTERMEDIATE CASE FAIRING AT 5 O'CLOCK POSITION, RT ENGINE (REAR VIEW) UPPER FAIRING COVER BEGAN TO SEPARATE WITH SEVEN RIVETS SHEARED. ACCOMPLISHED INSPECTION IAW AMM 72-34-05, FOUND WITHIN LIMIT, SECURED WITH SPEED TAJul 17, 2013 · N674UA · Boeing 767322SDR ASMF201308010Blade · damagedDURING TRANSIT CHECK, MX PERSONNEL DETECTED FOD DAMAGED ON 2 FAN BLADES OF THE RT ENGINE. MX PERSONNEL PERFORMED A FOREIGN OBJECT DAMAGE INSPECTION IAW MM TASK 71-00-00-800-802-F00, DETECTING 2 FAN BLADES DAMAGED, 1 OUTLET GUIDE VANE CRACKED AND INNER BARREL Jul 16, 2013 · N858AM · Boeing 7378Q8SDR CA130729004Compressor · overspeed(CAN) DURING T/O ROLL, THE HIGH COMPRESSOR ROTOR HAD AN OVERSPEED AND THE CREW ABORTED THE T/O. DATA DOWNLOAD SHOWED THAT THE BLEED VALVE LIKELY MALFUNCTIONED, CAUSING A LARGER BLEED THAN EXPECTED AND LEADING TO THE OVERSPEED. THE ENGINE WILL BE SENT FOR REPAJul 15, 2013 · Cessna 560XLSDR AC2A07907102013Compressor · stalledDURING CLIMB OUT, WHILE PASSING THROUGH 200 FT, THE HELICOPTER EXPERIENCED A COMPRESSOR STALL. TORQUE READINGS WERE MAXED OUT AND THE ACFT EXPERIENCED A RT THEN LT YAW.Jul 10, 2013 · N31079 · Bell 206L3SDR UALA2013071004807Liner · damagedATTRITION LINER AT 3 O'CLOCK POSITION HAS 1 INCH OF FILLER MATERIAL MISSING FROM PREVIOUS REPAIR. REPAIRED FAN CASE LINER IAW AMM MT 72-017.Jul 9, 2013 · N485UA · Airbus A320232SDR UALA2013071004816Blade · bentON WALK AROUND, NR 2 ENGINE BLADE FOUND BENT AT LOCATION MID SPAN AREA. FOUND AREA WITHIN LIMITS. BEND IS SMOOTH AND CONTOUR.Jul 9, 2013 · N558UA · Boeing 757222SDR 2013F00141Support · fracturedENGINE WAS REMOVED FROM THE ACFT DUE TO A CHIP LIGHT. ON REMOVAL OF THE COMPRESSOR FOUND THAT THE REAR SUPPORT WAS THE SOURCE OF THE METAL. THE AREA OF THE REAR SUPPORT ADJACENT TO THE NR 2 BEARING RETAINING RING GROOVE WAS FOUND TO BE FRACTURED WITH PIECES Jul 3, 2013SDR UALA2013070304649Fairing · crackedNOSE CONE NR 2 ENGINE CRACKED. CRACK IN FAIRING ASSY. FROM 1 BOLT HOLE ALL THE WAY THRU TO THE REAR EDGE, OUT OF LIMITS IAW AMM. REPLACED INLET CONE FAIRING IAW AMM.Jul 2, 2013 · N421UA · Airbus A320232SDR HALA2013070200084Blade · nickedDURING PDC CHECK, FOUND NUMEROUS BLADES NICKED ON NR 2 ESN: 729046. REF L/P 516463, ITEM 1: BLADE NR 30 ON NR 2 ESN 729046 IS NICKED BEYOND REPAIRABLE LIMITS. ACCOMPLISHED BLADE BLEND REPAIR IAW AMM 72-31-02-308-003-N00 TO AFFECTED BLADES. HFEC INSP ACCOMPLIJul 2, 2013 · N592HA · Boeing 7673CBSDR 2013FA0000424Bearing · failedA/C WAS ON A BRAVO TOUR, PILOT HEARD A BANG FOLLOWED BY A POWER LOSS AND ENTERED A AUTOROTATION TO THE RIVER EMERGANCY FLOATATION ACTIVATED AND A LANDING WAS MADE. FOUND NR 2 ENGINE COMPRESSOR BEARING FAILED.Jun 30, 2013 · N405MR · Bell 206L4SDR CA130717003Blades · damaged(CAN) DURING ROUTINE FUEL NOZZLE CHANGE, A BOROSCOPE INSPECTION OF THE HOT SECTION WAS CONDUCTED. IT WAS DISCOVERED THAT ALL THE CT BLADES HAD DAMAGE ON THE OUTER TIP OF THE BLADES. IT IS UNCLEAR IF THIS WAS CAUSED BY FOD, ITT OVERTEMP OR MATERIAL FAILURE. THEJun 28, 2013 · Cessna 208BSDR UALA2013062604426Blade · damagedNR 1 FAN BLADE ON RT ENGINE HAS NICK NEAR THE TIP. INSPECTED AND REPAIRED NR 1 ENG FAN BLADE IAW MM.Jun 24, 2013 · N526UA · Boeing 757222SDR UALA2013062604431Blade · bentBENT FAN BLADE NR 1 ENGINE. L/E AREA BEND AT AREA AT CIRCUMFERENTIAL DEVIATION (X)=0.1875 IN, AXIAL LENGTH OF BEND (Y) IS 2.0 IN, RADIAL LENGTH OF BEND (Z) IS 5.0 IN, WITHIN ACCEPTABLE BLADE BEND LIMITS OF AMM 72-31-11-200-010. B PARA 4.B(9)(B)(1)(2)(3) EDOJun 24, 2013 · N829UA · Airbus A319131SDR UALA2013061904268Blade · damagedNR 2 ENGINE BLADE, NR 16 DAMAGED. REPLACED NR 2 ENG BLADE, NR 16 AND MATE BLADE NR 34 WITH MATCHED PAIR IAW MM72-31-02.Jun 19, 2013 · N563UA · Boeing 757222SDR UALA2013061904266Blade · damagedNR 2 ENGINE BLADE NR 12 DAMAGED. REPLACED BLADE AND MATE BLADE WITH MATCHED PAIR IAW MM 72-31-02.Jun 18, 2013 · N563UA · Boeing 757222SDR UALA2013061904265Blade · damagedNR 2 ENGINE BLADE NR 14 DAMAGED BEYOND LIMITS. REPLACED NR 2 ENG BLADE NR 14 AND MATE BLADE NR 32 WITH A MATCHED PAIR IAW MM 72-31-02.Jun 18, 2013 · N563UA · Boeing 757222SDR UALA2013061904249Blade · damagedFOUND NR 2 ENG FAN BLADE NR 8 DAMAGED BEYOND REPAIRABLE LIMITS. REPLACED NR 8 AND NR 26 BLADES WITH MATCH SET. ACCOMPLISHED INSTALLATION OF COMPRESSOR INLET CONE IAW MM 72-31-01-401.Jun 18, 2013 · N563UA · Boeing 757222SDR UALA2013061904267Blade · damagedNR 2 ENGINE NR 30 BLADE DAMAGED. REPLACED NR 2 ENG BLADE NR 30 AND MATE BLADE NR 12 IAW MM 72-31-01.Jun 18, 2013 · N563UA · Boeing 757222SDR UALA2013061904256Blade · dentedNR 2 ENGINE, NR 12 BLADE DENTED. DRESSED DENT REF MM 72-31-02. DAMAGE WAS APPROX 3" FROM BLADE TIP.Jun 18, 2013 · N565UA · Boeing 757222SDR UALA2013061204006Liner · peelingDURING WALK AROUND, FOUND ON LEFT ENGINE AT ONE O`CLOCK, ACOUSTIC LINER PEELING OFF FAN EXIT SEGMENT. REPLACED CLOTH PATCH.Jun 7, 2013 · N667UA · Boeing 767322SDR UALA2013060603920Blade · bulgedDURING ACFT WALK AROUND, FOUND ON RT ENGINE BLADE NR 2 BULGED .5" LONG BY .0937" DEEP ON THE L/E. BULGE IS LOCATED 6 INCHES FROM ROOT OF THE BLADE. PERFORMED BLENDING OF NR 2 BLADE DAMAGE IAW AMM.Jun 5, 2013 · N665UA · Boeing 767322SDR UALA2013060503903Rub Strip · out of toleranceNR 1 ENGINE AT 6 O'CLOCK POSITION HAS MISSING REPAIR AREA ON FAN BLADE RUBSTRIP. REPAIRED FAN CASE RUBSTRIP REPAIR NR 1 ENG AT 6 O'CLOCK POSITION.Jun 5, 2013 · N215UA · Boeing 777222
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