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 HALA2009092900442Blade · damagedETOPS SIGNIFICANT SYS - ON ETOPS 2 CHK FOUND ENGINE NR 2 BLADE NR 27 WITH NICK 0.500 LONG, 0.200 DEEP. ON NR 2 ENG - BLENDED FAN BLADE IAW AMM 74-31-02. OK FOR SERVICE.SDR CA090929007Wheel · cracked(CAN) DURING INSP 72-020-01-01 IT WAS FOUND THE 2 BLADE PLATFORMS HAD BEEN CRACKED AND BROKEN OFF AT THE BUSHING SURROUND.SDR CA091020004Case · cracked(CAN) CRACKS TO THE AFT FAN CASE PN 6052T01G08 WERE DISCOVERED PRIOR TO SCHEDULED ACFT ENG WATER WASH. 2 CRACKS ALONG THE HORIZONTAL AXIS OF THE FAN CASE CONTINUING DOWNWARD ALONG THE FLANGE. ENG HASE BEEN REMOVED FOR FAN CASE REPAIR.SDR CA090924008Case · cracked(CAN) UPON CLEANING OF FAN ASSY. DURING MX EVENT, IT WAS NOTICED THAT A 3 INCH CRACK AFT OF THE FAN STATOR RING WAS PRESENT. FURTHER INVESTIGATION REVEALED A CRACK PROPOGATING ALONG 2 BOLT HOLES THAT ATTACH THE FAN CASE TO THE THRUST REVERSER DEFLECTOR RING.SDR VNAA2009092300006Fan Blade · damagedCREW REPORTED, INGESTED SMALL BIRD(S) IN LEFT ENGINE. AIRCRAFT RETURNED TO DAY WITHOUT INCIDENT. MAINTENANCE INSPECTED LT ENGINE PER THE MANUFACTURER MAINTENANCE MANUAL AND REPLACE FAN BLADES. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFSDR UALA2009091602932Blade · damagedNR 1 ENG BIRD STRIKE, RTFL. ON CLIMBOUT, ABOUT 800FT, CREW HEARD A LOUD BANG FOLLOWED BY A BAD ODOR AND MILD ACFT VIBRATION. ACFT HAD A BIRD STRIKE ON THE LT SIDE NR 1 ENGINE. ALL INDICATIONS WERE NORMAL. NO CABIN PREP AND CREW MADE A NORMAL LANDING. NR 1 ESDR CA090924003Blade · damaged(CAN) COMPRESSOR STALL OF RT ENG DURING CRUISE. HIGH VIBS OF N3 UP TO 9.0 UNITS. OPERATED AT REDUCED PWR DURING DIVERSION FOUND HPC DAMAGED. STAGE NR 1 BLADES SEVERLY DAMAGED. MANY NICKS, TEARS AND DENTS AND MISSING MATERIAL ON ALL BLADES. ONE BLADE BROKEN OFSDR EYDAN128KGC1FODCompressor · distortedON 09/10/09 THE AIRCRAFT DEPARTED EWR ENROUTE TO OPF, DURING CLIMB IN ICING CONDITIONS; AT 33,400 FT, THE NR 1 ENGINE HAD A COMPRESSOR STALL AND STARTED TO ROLL BACK. THE CREW INITIATED A RELIGHT AND THE ENGINE RETURNED TO NORMAL OPERATION. MAINTENANCE INSPECSDR HALA2009083000396Fan Blade · damagedETOPS SIGNIFICANT SYS - FOUND NR 1 ENG, 1ST STAGE FAN BLADE HAS SMALL NICK ABOUT MID SPAN ON BLADE NR 13 L/E (AREA F). BLENDED AREA IAW AMM 72-31-02 WITHIN LIMITS EDDY CURRENT CK OK.SDR SWAA095605Compressor Blade · damagedDECLARED EMERGENCY, COMPRESSOR STALL, NR 2 ENG AT 41,000 FEET. RECOVERED IMMEDIATELY. NO OVERTEMP NOTED. DESCENDED WITH ENGINE AT REDUCED THRUST. LANDED WITH NR 2 ENG AT IDLE. POST FLT REVEALED NO ABNORMALITIES (FOD) IN ENG. FOUND 3 HPC BLADES DAMAGED. SDR IPXA09157110Fan Blade · damagedINSPECTION TYPE:N/A CREW REPORTED POSSIBLE BIRD STRIKE WITH ASSOCIATED RT ENGINE VIBRATION REACHING 3.2. AFTER LANDING FOUND 2 FAN BLADES DAMAGED ON RT ENGINE. FOUND TWO BLADES DAMAGED BEYOND LIMITS. R&R BLADE SETS PER AMM. PERFORMED VIBE SURVEY.SDR USAA2009081892154Engine · bird ingestionFLT 407 PHX-ATL - DIVERSION / BURNING SMELL - DIVERTED INTO MEMPHIS DUE TO STRONG BURNING PLASTIC SMELL IN CABIN THROUGHOUT CLIMB AND INTO CRUISE. MAINTENANCE FOUND EVIDENCE OF BIRD INGESTION IN NR 1 ENGINE ON STAGE 3 HIGH PRESSURE COMPRESSOR. PERFORMED COMPSDR ASAA0956413Shim · wornNR 2 ENGINE FAN BLADE SHIMS NEED REPLACED PER T/C 78472002 STEP 4. REPLACED NR 2 ENGINE FAN BLADE SHIMS WITH PREFERRED SHIMS P/N 340 252 307 0 PER T/C 78472002.SDR CLCA08152009.1Engine · fodDURING TAKEOFF ROLL (MIA) NR 1 ENGINE VIBRATION OCCURRED FOLLOWED BY LOUD COMPRESSOR STALL. ABORTED TAKEOFF, ENGINE SHUT DOWN AND CAC EMERGENCY PROCEDURES FOLLOWED. RETURNED TO RAMP WITHOUT INCIDENT. INSPECTED NR 1 ENGINE, FOUND SEVERAL PARTICLES OF METAL ISDR 2009FA0000740Impeller · crackedCOMPRESSOR WAS RECEIVED TO REPAIR FOR DAMAGE TO ROTOR. UPON DISASSEMBLY AND INSP, DISCOVERED THAT A SECTION OF SHROUD BETWEEN THE NR 2 VANES AT THE FWD END OF THE IMPELLER (IDENTIFIED AS DIAMETER I) HAD BROKEN OFF. CAUSE COULD NOT BE DETERMINED. HOURS AND CSDR CA090825006Impeller · crackedUPON ENG TESTING DURING INSTALLATION OF ENG ON THE LT SIDE OF ACFT, A LOUD HOOTING AND WHISTLING WAS HEARD BY MX. UPON FURTHER INVESTIGATION WHICH INCLUDED A CLOSE LOOK AT 1ST STAGE IMPELLER THROUGH ENG INTAKE, SEVERAL CRACKS WERE FOUND ON IMPELLER. ENG HAD SDR UALA2009081002405Compressor · leakingABORTED TAKEOFF AT 50KTS DUE TO SMOKE IN THE COCKPIT. SMOKE AND OIL ODOR COMING OUT OF COCKPIT EYEBALLS ON TAKEOFF ROLL. ABORTED TAKEOFF, RETURNED TO GATE. 15 MIN IDLE RAN NR 1 ENG. NOTED: NR 1 ENG HAD JUST BEEN CHANGED DUE TO NR 5 BRG LEAKING OIL. COMPLETED SDR AALA20090808JFK01Compressor Blade · damagedJFK - INFLIGHT EWR-LAX. AIRCRAFT HAD BIRD STRIKE TO LEFT ENGINE AND LEFT ENGINE VIBRATIONS ON TAKEOFF. LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED BOROSCOPE INSPECTION AS PER MM 72-00-00-6. NO DISCREPANCIES NOTED. REMOVED ANDSDR HALA2009080400349Fan Blade · damagedETOPS SIGNIFICANT SYS - FOUND NICK ON NR 2 ENG 1ST STAGE FAN BLADE APPROX 8.5" FROM ROOT AREA F. REPAIRED FAN BLADE IAW TASK 72-31-02 WITHIN LIMITS. EDDY CURRENT CHECK OK.SDR DL757091300Compressor · seizedAIRCRAFT WAS ON TAKEOFF ROLL ACHIEVED APPROXIMATELY 20 KNOTS, CREW HEARD LOUD BANG AND AIRCRAFT VEERED LEFT. PASSENGERS REPORTED FIRE/SPARKS COMING FROM NUMBER 1 ENGINE. ENGINE SHUT DOWN ON ITS OWN WHEN THROTTLE WAS RETARDED. FIRE DEPARTMENT SPRAYED STRAIGHSDR AALA20090729STL01Fan Blade · damagedAT 1100" AGL BIRD STRIKE RIGHT ENGINE. INITIAL EPR DROP OF .60, RECOVERED AFTER DELAY OF 10 SECONDS (COMPRESSOR STALL). SMOOTH OVERWEIGHT LANDING AT 152,500. ENGINE WAS OPERATED AT IDLE. PRELIMINARY VISUAL 13 FAN BLADES BENT/DAMAGED. INSPECTION TO COMPLETSDR DL76L091283Compressor Blade · crackedFOUND ONE 5TH STAGE BLADE CRACKED OUT OF LIMITS DURING OPN 50169 5TH BLADE BORO INSP. PERFORMED BORESCOPE INSP PER OP 50169. FOUND BLD ROOT CRACKED CAT C - ENG REMOVAL REQUIRED BEFORE FURTHER FLIGHT. QC1418 BORO PLUGS / TURNING PAD COVER RE-INSTALLED / 5179SDR HALA2009072700331Fan Blade · bentETOPS SIGNIFICANT SYS - FOUND NR 1 ENGINE FAN BLADE NR 30 DAMAGED. BENT. INSPECTED BLADE AND DETERMINED TO BE WITHIN LIMITS IAW AMM 72-31-02-206-070-N00 ON NR 1 ENG BLADE 30. OK FOR SERVICE.SDR HALA2009072700330Fan Blade · bentETOPS SIGNIFICANT SYS - FOUND NR 1 ENGINE FAN BLADE 29 DAMAGED. (BENT) INSPECTED BLADE AND DETERMINED TO BE WITHIN LIMITS IAW AMM 72-31-02-206-070-NOO ON NR 1 ENG BLADE 29. OK FOR SERVICE.SDR HALA2009072700329Fan Blade · damagedETOPS SIGNIFICANT SYS -FOUND NR 1 ENGINE FAN BLADE 33 DAMAGED, NICKED. PERFORMED BLADE BLENDING PROCEEDURE IAW AMM TASK 72-31-02-308-003-N00 ON NBR 1 ENG BLADE 33. OK FOR SERVICE.SDR DL75E091197Blade · bentCREW REPORTED, SAW A BIRD DURING T/O ROLL AND THEN HEARD A BANG. F/O THEN TOLD CAPT THAT THE RT ENG WAS ROLLING BACK DUE TO EPR DROP FROM 1.4 TO 1.25. THE CAPT THEN ABORTED T/O. THE F/O SAID THE EPR RECOVERED JUST AFTER THAT, BUT THE CAPT WAS ALREADY DOING TSDR HALA2009071500298Rub Strip · missingETOPS SIGNIFICANT SYS. DURING WAC FOUND NR 2 ENG RUB STRIP UNDER FAN BLADE MISSING SECTION 1 INCH X 1 INCH, 0.025 INCH DEEP, 0930 POSITION. OK TO GO IAW AMM 72-33-04-206-001.SDR UALA2009071502094Blades · crackedENGINE THRUST ISSUE, RTFL. REPLACED MEC. FAILED PWR RUN. BORO FOUND 2 STG 5 COMP BLADES CRACKED, ENG CHG ACCOMPLISHED, IDLES & LK CHKS. ENG REPLACED ON ACCT OF CRACKED COMPRESSOR BLADE.SDR CA090713001Seal · failed(CAN) ETR PW100 0500 INTERTURBINE AIR SEAL FAILURE.SDR AALA20090705MIA01Compressor · stalledMIA - AIR INTERRUPT NUMBER TWO ENGINE COMPRESSOR STALL. ENGINE GAS TEMPERATURE AT 990 DEGREES FOR EIGHT SECONDS. EMERGENCY DECLARED, RETURNED TO MIA WITHOUT INCIDENT. SINGLE ENGINE TIME LESS THAN 15 MINUTES. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED FLISDR ASAA0956126Fan Blade · nickedWHILE ACCOMPLISHING TC 78472002, NR 2 ENG FAN LUBE ESN 894 258. FOUND 5 EA PN 340 001 814 AND 1 EA PN 340 001 816 PLATFORMS WITH NICKS AT FWD LUG FACE GREATER THAN .008 INCH GROUNDED YES. REPLACED 6 EA DAMAGED PLATFORMS WITH NEW PLATFORMS PN 340 001 816 REF. SDR ASAA0956125Shim · wornWHILE ACCOMPLISHING FAN LUBE TC 78472002 NR 2 ENG SN 894 258 FOUND EXCESS MOLYDAG COATING WORN ON ALL 24 SHIMS. REF STEP 56 ON TC GROUNDED YES. REMOVED 24 EACH FAN BLADE SHIMS PN 340 252 306 0 AND INSTALLED 24 EACH NEW SHIMS PN 340 252 307 0. REF TC 78472002 SDR C2XA09CL087Blade · fracturedCLE - FLT 2135 - THE CREW REPORTED A NR 2 ENGINE UNCOMMANDED SHUTDOWN IN FLIGHT. ENGINE WOULD NOT RESTART AND THE AIRCRAFT DIVERTED INTO CVG AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOSDR CA090617007Plenum · cracked(CAN) WHEN ACFT WAS DOWN FOR HEAVY MX, MECHANIC HAD NOTICED THAT THE RT ENGINE HAD A CRACK ON THE PLENUM AROUND THE BLEED AIR PORT. ENGINE WAS REMOVED AND FORWARDED TO THE COMPANY’S ENGINE SHOP FOR REPAIR. PART WAS REPLACED AND ENGINE WAS REINSTALLED ON THE SDR HALA2009061500236Fan Blade · damagedETOPS SIGNIFICANT SYSTEM, RT ENGINE FAN BLADE NR 6 FOUND WITH NICK'S ON THE LEADING EDGE, 2 1/2 INCHES FROM THE TIP. LEADING EDGE AREA "A"-3/16 INCHES BY 1/4 INCHES LONG. PERFORMED BLENDING ON RT ENGINE FAN BLADE NR 6 IAW B7
67 AMM 72-31-02.SDR P5CA2009061101599Blades · damagedCREW REPORTED VIBRATION FROM NR 1 ENGINE ON CLIMB. CREW DUMPED FUEL AND RETURNED TO LAX. FOUND EVIDENCE OF BIRD STRIKE IN NR 1 ENGINE INLET. ACCOMPLISHED BIRD STRIKE INSPECTION PER AMM 72-00-00 AND 05-51-14. REPLACED 7 DAMAGED FAN BLADES PER AMM 72-31-02.SDR CA090606003Compressor · fod(CAN) ON T/O ROLL, RT N1 DROPS FROM 86 PERCENT TO 50 PERCENT. TAKEOFF ABORTED. MX INSP REVEALED FOD DAMAGES ON FAN AND COMPRESSOR. A CIRCULAR CUT WAS FOUND ON NR 4 WHEEL TIRE. IT IS SUSPECTED THAT AN FOREIGN OBJECT EMBEDDED IN THE NR 4 WHEEL TIRE RELEASED FROMSDR DXTA2009060803683Fan · vibrationLT ENGINE VIBRATION AT FL 400. VIBRATION STARTED WHEN THROTTLE WAS RETARDED FROM 98.3 TO 97 PERCENT N1. THROTTLE MOVEMENTS HAD NOT EFFECT ON VIBRATION. SOUND DECREASED AS ACFT DESCENDED. REMOVED FAN BLADES FAN HUB AND RE INDEXED FAN HUB 180 DEGREES FROM ORIGISDR ASAA0955838Shim · damagedWHILE ACCOMPLISHING ASA T/C 78472002 ON NR 2 ENGINE FOUND 24 EACH SHIMS MISSING MOLYDAG COATING GREATER THAN 25 PERCENT. REF MM 72 21 02 200 801 F00 PARA L. REMOVED AND REPLACED 24 EACH SHIMS, INSTALLED SHIM P/N 340 252 307 0 PER T/C 78472002.SDR ASAA0955821Shim · wornTWENTY FOUR (24) FAN BLADE SHIMS REQUIRE REPLACEMENT DUE TO WEAR, NR 1 ENGINE. INSTALLED 24 FAN BLADE SHIMS. P/N 340 252 307 0 PER T/C 78472002.SDR UALA2009060101549Blade · dentedCREW REPORT: ON PREFLIGHT FOUND DIME SIZED DENT ON LEADING EDGE OF LEFT ENGINE NR 26 1ST STAGE BLADE. BLENDED SMALL DING ON NR 1 ENGINE, BLADE NR 26 LEADING EDGE, MARKED.SDR HALA2009053000211Blade · nickedETOPS SIGNIFICANT SYSTEM - FOUND NR 1 ENG BLADE NR 34 HAS SMALL NICK ON LEADING EDGE 2 INCHES FROM TIP (AREA A). INSP AND BLENDED BLADE PER AMM 72-31-02. EDDY CURRENT CK OK.SDR REXA200900057Compressor · contaminatedDURING CLIMBOUT THE SMOKE AFT LAV ILLUMINATED. AFT CABIN ATTENDANT REPORTED AN ODOR BUT NO SMOKE ALTHOUGH THE SMOKE DETECTOR ACTIVATED. THE FLIGHT CREW DONNED OXYGEN MASKS, PERFORMED THE QRH AND REQUESTED A RETURN TO DEPARTURE. AN OTHERWISE NORMAL APPROACH ASDR R61A20090027Compressor · damagedCREW REPORTED SEVERE VIBRATION, PARTIAL LOSS OF THRUST, AND E-1 CONTROL FAULT MSG DURING CRUISE TO PHL. CREW SHUTDOWN E-1 AND DECLARED EMERGENCY INTO MDT. LANDED WITHOUT INCIDENT, AND MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MX PERFORMED BOROSCOPE ON E-1SDR ZZDA2009166Compressor · stalledCOMPRESSOR STALL RIGHT ENGINE AT FL 180 WITH CLIMB POWER CHANGE TGT 1149. REMOVED AND REPLACED RT ENG PER TASK CARD 603. RAN ENGINE & LEAK & OPS CHECK GOOD.SDR HALA2009052300195Fan Blade · damagedNR 1 ENG BLADE (FAN) NR 28 HAS NICK ON L/E 7.5 INCHES FROM TIP, 3/16 INCH DEEP. BLENDED BLADE PER MM72-31-02 BLEND WITHIN LIMITS. OK FOR SERVICE.SDR DL764090852Guide Vane · damagedDURING OPS 5003 BORO FOUND 1 EACH 1ST STAGE NGV DAMAGED BEYOND M/M LIMITS.SDR C8GA20090064Fan · bentFLT 706 FROM ILN TO MSP, DURING TAKEOFF ROLL THE NR 3 ENGINE HAD A COMPRESSOR STALL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 3 ENGINE HAD INGESTED A GOOSE. THE C1 AND C2 FSDR ASAA0955443Screw · defectiveNR 1 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION LEVELS TO BE TRENDING HIGHER THAT NORMAL AFTER LAST FAN LUBE. TESTED AAVM AND FOUND SCREW LOCATION NR 1 14 30 34 NEEDING REPLACEMENT. REMOVED AND REPLACED BALANCE SCREWS 1 AND 14, REMOVED P11 INSTALLESDR CA090429001Fan Blade · bent(CAN) ON THE TAKEOFF ROLL,THE ACFT SUSTAINED A BIRD STRIKE FROM A MEDIUM SIZED BIRD. THE BIRD WAS INGESTED INTO THE NR1 ENGINE. AFTER TAKEOFF THERE WAS A CONSTANT BUZZING NOISE WHICH WAS ABNORMAL. THE ENGINE PARAMETERS FOR BOTH ENGINES APPEARED TO BE NORMAL WI
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