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 HALA2011050400181Blades · damagedETOPS SIGNIFICANT SYS - ON OVERNIGHT NR 1 ENG FOUND NR 4, 5, 6, 7, 8, 9 AND 10 BLADES INBEDDED IN ACOUSTIC. REMOVED BLADES NR 4, 5, 6, 7, 8, 9 AND 10 IAW AMM 72-31-02. REPAIRED ACOUSTIC LINER IAW M105 594140. REINSTALLED FAN BLADES NBR 4,5,6,7,8,9 AND 10 IAW SDR HALA2011050400180Shroud · damagedETOPS SIGNIFICANT SYS - FAN CASE SHROUD DAMAGED AT 7 O`CLOCK POSITION NR 1 ENG. REPAIRED FAN CASE SHROUD IAW AMM 72-34-01 AND HAL M105 594140. PERFORMED IDLE VIBRATION RUN M105 594140. OPS CK GOOD.SDR QMLA2011050111052Gas Generator · noisyAFTER THE COMPLETION OF A THIRD PATIENT FLIGHT, THE ACFT FAILED TO START. DURING THE NORMAL START SEQUENCE AS THE FUEL WAS INTRODUCED INTO THE ENGINE, THE ENGINE FLAMED OUT WITH AN IMMEDIATE DROP IN T4 TEMPERATURE. THE MECHANIC BEGAN TROUBLESHOOTING THE ENGISDR IPXA1666285Blade · damagedINSPECTION TYPE:ETOP, BIRD STRIKE DEPARTING VCP AT 5000' MSL. EXCESSIVE LT ENGINE VIBRATION AND NOISE. RETURNED TO VCP. WILL ACCOMPLISH BORO INSP AND REPLACEMENT OF DAMAGED FAN ROTOR BLADES IAW FIM AND AMM.SDR UALA2011042902105Blades · damagedNR 2 ENGINE FOUND MOST HPC STAGE 13 & 15 BLADES WITH L/E IMPACT DAMAGE EXCEEDING LIMITS. EXCEED LIMITS IN AREAS 'A','B','C' AND 'E' THAT ARE ALLOWED. REQUIRES ENG CHANGE. REMOVED NR 2 ENG. THIS IS PRECAUTIONARY DUE TO ECM PARAMETER SHIFT. IF CAN CONTINUE SDR CHQA201100155Blade · detachedCREW REPORTED THAT WHILE AT FL280, THERE WAS A SIGNIFICANT VIBRATION/SHUDDER AND E1 ITT GAUGE WAS IN THE RED RANGE. CHECKLISTS WERE FOLLOWED AND E1 WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO KMDT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. THE ENGINE WAS CHSDR IXXA110035OControl Cable · out of rigDURING LEVEL OFF, NR 3 ENGINE COMPRESSOR STALLED WHEN THROTTLES WERE RETARDED,(N1-93 PERCENT, N2-91 PERCENT, F/F-3100, OAT-44 DEGREES AND M-.80/300KIAS). THE CREW DIVERTED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED TROUBLESHOOTING TREE NR 41, RERIGGED VSV AND SDR EIAA2011039Compressor · surgesDURING CLIMB ENGINE NR 1 HAD ENGINE COMPRESSOR SURGE AT 12,000 19,000 AND AGAIN AT 29,000. OPERATED ENGINE AT IDLE NO FURTHER STALLS, NO EXCEEDENCE OBSERVED. RETURNED TO ANC. REMOVED AND REPLACED NR 1 ENGINE PER EIA W/C F7001, F7202, F7207, F7209 OP'S CHECKSDR QMLA2011042411050Compressor · contaminatedIN CRUISE FLIGHT, UPON TURNING THE HEATER ON, SMOKE & FUMES FILLED COCKPIT AND CABIN. THE PROBLEM WAS SOME LT OVER RESIDUE FROM THE COMPRESSOR WASH. MECHANIC VERIFIED THE SYS INTEGRITY THEN RAN THE ACFT WITH THE HEAT ON AND DOORS OPEN TO VENTILATE SYS. RAN FSDR MASA2011042202484Unknown · malfunctionedRT ENG DEGRADED CTN IN FLT. MX RAN ENGINE 3 TIMES NO FURTHER FAULTS NOTED.SDR AALA20110420TUL12Compressor · stalledCREW REPORTED LEFT ENGINE COMPRESSOR STALLED DURING CLIMBOUT. ENGINE RETURNED TO IDLE WITH HIGH EGT. LEFT ENGINE SHUT DOWN (SINGLE ENGINE TIME 15 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. UPONSDR UALA2011042001909Blade · damagedDUE TO FAN BLADE NR 21 WAS DAMAGED, REPLACED. NR 2 ENG S-N V10523 LPC BLADE 21 MOMENT WT 2498.0 AND PERFORMED VIB SURVEY REF MM. PEAK VIB .7 N1 AND .2 N2. OPERATIONAL TEST NORMAL.SDR TRBA2011037Compressor · damagedSTRONG SMELL OF OIL FILLED COCKPIT AND CABIN ON APPROACH WITH POWER PULLED BACK LESS THAN 10 PERCENT IN ATTEMP TO ISOLATE THE SOURCE. IT APPEARS TO BE COMING FROM THE NR 1 PACK/BLEED AFTER FOLLOWING APPROPIATE CHECK LISTS. DURING BOROSCOPE INSPECTION OF L/H SDR CA110408002Vane · damagedDURING TAXI OUT ENG NR 1 FLAMED OUT, ECAM ACTIONS COMPLETED AND THE ACFT RETURNED TO GATE AS WAS MET BY MX. INVESTIGATION BY ENGINE SHOP REVEALED COMPRESSOR VANE FAULT.SDR USAA20110408BA031Compressor · damagedCLT FLT 732 EN ROUTE CLT TO LGW. DURING CLIMB FROM 8,000 FEET TO 14,000 FEET, THE FLIGHT CREW HEARD A LOUD BANG AND FELT THE AIRCRAFT SHUDDER. THIS WAS FOLLOWED BY AN EXTREMELY HIGH NUMBER TWO ENGINE EGT INDICATION AND A DROP IN OIL PRESSURE. THE CREW INISDR UALA2011040601658Fan Blade · debondedENG 2 N1 VIBES HIGH, CHECKED ALL CHIP DETECTORS ON NR 2 ENG, NO DEBRIS FOUND. POS 2 FAN BLADE TAP TEST REQ'D DUE TO HIGH N1 VIBE. PER T-S NEED TAP TEST PER AMM. ACP'D TAP TEST PER MM. FAILED ONE EA MARKED BLADE WITH 2979 DB PER SEC. NEED TO REPLACE N1 VIBRSDR MASA2011040802369Blade · lack of lubeNR 2 ENG VIBE AT 1.8 MLS IN FLT. MX PERFORMED BLADE LUBE.SDR IPXA1565868Compressor · stalledCOMPRESSOR STALL RT ENGINE AFTER T/O LEVEL AT 4000'. PERPFORMED ACCELERATION AND DECELERATION TEST NR 11. SYS TESTS NORMAL. REF MM 71-00-00-5.SDR UALA2011040601666Blade · bird ingestionLEFT ENGINE BIRD STRIKE. CONFERRED WITH ENGINE DESK. ENGINE WILL NEED TO BE REPLACED. REPLACED NR 1 ENGINE ACCT ONE 6TH STG HPC BLADE HAS A TEAR IN A BLADE TIP CURL. RPL'D ENGINE PER MT71-01SDR UALA2011040501643Fairing · out of rigLEFT ENG OUTER SUPPORT STATOR VANE MISSING AEROFOIL SHAPED FAIRING. INBOARD SIDE OF ENGINE LOWER INTERMEDIATE STRUT FAIRING LOCATED AT 5.30 POSITION IS MISSING THE UPPER FAIRING SKIN. OK TO CF PER MM. MUST BE REPLACED BEFORE THE 51ST HOUR OF OPERATION PER MSDR CA110405003Impeller · cracked(CAN) HIGH PRESSURE IMPELLER FAILURE, SECTION APPROX 40 X 40 MM RELEASED FROM QTY 1 VANE. DOWNSTREAM IMPACT DAMAGE TO ADDITIONAL VANES. ITEM HAS BEEN REMOVED FROM SERVICE & MFG HAS BEEN CONTACTED FOR FURTHER INFORMATION.SDR UALA2011040101571Blade · chippedNR 1 ENG ONE EACH BLADE L/E TIP CHIPPED (SIX O'CLOCK POSITION). BLADE HAS PIECE MISSING AROUND .093 DEEP AND .156 LONG, BLADE IS OUT OF LIMITS PER MM. TALKED TO OPBEMC, BLADE OUT OF LIMITS. REPLACED DAMAGED BLADE PER EG 5443-1. REMOVED DAMAGE BLD S-N CBDUSDR UALA2011033101547Fan Blade · damagedNR 2 ENG N1 FAN 3EA FAN BLADES EVIDENCE OF FOD DAMAGE. NEED TO DRESS BLADES. REPAIRED 3 EA FAN BLADES (MARKED ON BLADE ROOT) ON NR 2 N1 FAN.SDR MASA2011040102298Compressor · lack of lubeENG 1 FAN VIBE UP TO 1.7 IN TRANSIENT. MX C/W FAN BLADE LUBE, ENGINE RUN CHECK VIBE IS 0.3 MILS.SDR USAA2011032591231Compressor Blade · damagedFLT 51 - PHX - RTO - ON TAKEOFF ROLL AT ABOUT 110 KNOTS, CREW REPORTED A LOUD BANG AND THE AIRCRAFT VEERED SHARPLY TO THE RIGHT - TAKEOFF WAS REJECTED. PASSENGERS REPORTED SEEING FLAMES COMING OUT OF THE RIGHT ENGINE. MAINTENANCE FOUND NR 2 ENGINE HIGH PRESSDR ASAA1179237Compressor · stalledON TAXI OUT NR 1 ENGINE HAD A LOW PITCH RUMBLE LOUDER THAN NORMAL. ON T/O NR 1 ENGINE HAD LOUD BANGING COMPRESSOR STALLS ABORTED T/O AT ABOUT 40 KNOTS AIRCRAFT ON TAXI WAY REPORTED FIRE COMING OUT OF BACK OF NR 1 ENGINE. COMPRESSOR STALLS BEGAN JUST PRIOR TO SDR USAA20110315BB017Seal · crackedPHX FLT 26 EN ROUTE OGG TO PHX. THE CREW NOTED AN ODOR THAT STARTED ON THE GROUND, AND CONTINUED THROUGH CLIMB. THE ODOR DISSIPATED AT CRUISE ALTITUDE. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT ENGINE HAS OIL LEAKING FROM THESDR MASA2011031402141Compressor Blade · lack of lubeENG 2 VIBE 1.8 AT 82% & 2.2 AT 87% N1. MX C/W FAN BLADE LUBE AND REPLACED BLADE PINS.SDR IXXA110027OMec · defectiveAT THE TOP OF CLIMB OUT AT FLIGHT LEVEL 36,000 FT WHEN THROTTLES WERE PULLED BACK FROM CLIMB POWER TO CRUISE POWER NR 3 ENG MOMENTARILY COMPRESSOR STALLED. ALL OTHER ENGINES PARAMETERS WERE NORMAL AND NR 3 COMPRESSOR STALLED AGAIN 10 MINUTES LATER AT CRUISE WSDR USAA2011031491044Actuator · stalledFLT 88 - CREW REPORTED NR 1 ENGINE COMPRESSOR STALL ON CLIMB WITH MAX EGT 720+ FOR ONE MINUTE. SHUT DOWN ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. THE ROOT CAUSE WAS IDENTIFIED AS THE VSV ACTUATOR WHISDR DALA1119280136Rib · crackedNR 1 ENGINE AFT FAN ASSY / AFT FAN CASE FWD RIB CRACKED AT 12 O'CLOCK POSITION DURING INSTALLATION. NR 1 ENGINE AFT FAN CASE CRACKED FWD T RIB REPAIRED IAW ER/A 488809-14 REV ORIGINAL.SDR UALA2011030301048Liner · debondedNR 2 ENG, MECH FOUND FACE SHEET FOR SOUND ABSORBING LINER DISBONDED. DAMAGED FACE SHEET LOCATED AT 9:00 POSITION (ALF) LOOSE MATERIAL REMOVED. TO BE REPAIRED IN 25T PER AMM. FAN EXIT CASE LINER MISSING COATING. REAPPLY COATING BY PTT 59501. REPAIRED APPLIED SDR ALGA030211276ALScroll · crackedON DAILY SERVICE CHECK, MX FOUND ENGINE COMPRESSOR SCROLL CRACKED. R & R ENGINE ASSY.SDR HALA2011030100121Blade · nickedUNDRESS NICK NOTED ON NR 1 ENGINE FAN BLADE. FOUND NR 1 ENGINE FOD ON NR 28 BLADE,REMOVED AND REPLACED BLADE 9 AND 28 PER AMM 72-31-404-021-400. ACCOMPLISHED VIBRATION CHECK PER AMM 71-00-00, OPS CHECK OK. OK FOR SERVICE.SDR ZZDA2011248Compressor · stalledLEFT ENGINE COMPRESSOR STALL (LEFT ENGINE WENT BOOM, PLANE YAWED, N2 WENT TO 56 PERCENT, LOTS OF VIBRATION). SHUT DOWN ENGINE. REMOVED AND REPLACED NR 1 ENGINE IAW 71-00.SDR ASAA1159074Blade · damagedWHILE PERFORMING T/C 78472002 ON NR 1 ENGINE FOUND NR 17 BLADE PLATFORM WITH TORN RUBBER STRIP. REPLACED NR 17 PLATFORM P/N OFF 340 001 816 0 & INSTALLED PLATFORM P/N 340 001 816 0 PER T/C 78472002. PERFORMED FAN BLADE SURVEY PER T/C 78472002 STEP 55 CHECKS SDR CA110224002Fan Blade · dentedDURING THE MORNING PRE-FLIGHT INSP WALK AROUND, FLIGHT CREW NOTICED SOME DAMAGES TO THE LT ENGINE FAN BLADES. MX WAS NOTIFIED AND A TEAM DISPATCHED ON AN AOG TRIP. MX INSP REVEALED DENT ON MULTIPLE FAN BLADE L/E AND ON THE INTAKE ACOUSTIC PANEL. ENGINE FAN SDR SAJFCALS100007Arm · failedB-18208// AIRCRAFT, IN ROUTE, FLT CREW REPORTED THAT DURING CLIMB, FL130 NR 1 ENG SURGE EPR & N1 SPOOLED DOWN & FLT CREW FOLLOW QRH NR 1 ENG SHUTDOWN. A/C RETURNED. NR 1 ENG WAS REMOVED FROM SERVICE. MX FOUND THE SIXTH STAGE VSV ARM FAILED WHICH CAUSED SEVSDR F3LA2011022100606Stop · seizedACFT LOG PAGE 590497: AIR TURN BACK AT 01302. ECAM WARNING NR 2 ENGINE COMPRESSOR VANE (AIR RETURN. REPLACED NR 2 ENGINE MASTER BALLSCREW ACTUATOR STOP. REF AMM 75-31-50 PB 401, OPS CHECK NORMAL.SDR CA110221008Scroll · cracked(CAN) CRACK IN COMPRESSOR SCROLL ON THE RT SIDE OFF OF A WELD. APPROXIMATELY 1" IN LENGTH. COMPRESSOR ASSY REMOVED FOR REPAIR.SDR UALA2011021600813Skin · missingRT ENGINE REAR STATOR MISSING WHOLE LOWER SKIN, UPPER SKIN BEGINNING TO COME OFF. INSPECT INTERMEDIATE CASE STRUT FAIRING IAW MM. INSPECTED COMPRESSOR INTERMEDIATE CASE STRUT AT 3 O'CLOCK POS. LOWER FAIRING MISSING. DAMAGE. CF IAW AMM.SDR ASMF201102003Blades · damagedDURING A BORESCOPE INSPECTION OF THE HPC 1ST STAGE BLADES OF RIGHT ENGINE WAS DETECTED FOUR BLADES OF THE HPC 1ST STAGE WITH LEADING EDGE TIP CURLED 45 DEGREES OUT OF LIMITS IAW 72-00-00, PARAGRAPH 5H (8) C (7), PAGE 625; WITH DIMENSIONS OF 1.0 INCHES LENGTH ASDR UALA2011021400772Rub Strip · damagedNR 1 ENGINE ATTRITION LINER AT 6 O'CLOCK POSITION FILLER REPAIR, BREAKING LOOSE. APPROX 3"X 2". ON WALK AROUND FOUND NR 1 ENG RUB STRIP AT APPROX 6 O'CLOCK POSITION DAMAGED. DAMAGE IS WITHIN THE RUB STRIP INNER LAYER, MEASURING 3.5 INCHES WIDEST AREA. FAN RUSDR IPXA1M64752Blade · damagedREF LP 423403 ITEM 2: INSPECT ENG NR2 IAW FIM TASK 77-32-08-00. WHEN PERF STEP 3 OF FIM 77-32-08-00 FOUND FAN BLADES 3,4,5,6,20,21,22 HAVE TIP CURLS OR AIRFOIL DISPLACEMENT, ALL OUT OF LIMIT. PARTS REQUESTED REQ E019213. R & R FAN BLADES IAW AMM 72-31-02-4 SDR ASAA1159028Shim · damagedREF T/C 78472002 NR 1 ENG FAN BLADE LUBRICATION. FOUND ALL 24 EACH FAN BLADE SHIMS MISSING MOLY COATING. INSTALLED 24 EACH P/N 340 252 307 0 ON BLADES REF T/C 78472002.SDR UALA2011020800681Guide Vane · delaminatedRT ENG 6 O'CLOCK FAN EXIT GUIDE VANE DELAMINATED. REMOVED EXIT GUIDE VANE AS PER MM. APPLIED SEALANT AND SPEED TAPE AS REQUIRED.SDR AALA20110204TUL15Fan Blade · damagedIAH - CREW REPORTED LEFT ENGINE COMPRESSOR STALL ON CLIMBOUT. AUTOPILOT KICKED OFF AND AIRCRAFT YAWED SLIGHTLY. EMERGENCY DECLARED FLIGHT RETURNED IAH LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED BOROSCOPE AND FOUND LEFT ENGINE HAD SDR FDEA201102030466Blades · damagedDURING INITIAL CLIMBOUT, FELT MODERATE VIBRATION (FELT LIKE NOSE GEAR SPINNING). AFTER INITIAL LEVEL OFF AT 9000 FT, VIBRATION LESSENED. DURING CLIMB TO 15000 FT, VIBRATION CONTINUED TO REVERSE WITH HIGH EVM READING. RAN QRH & WITH HIGH EVM & VIBRATION ASDR MASA2011020501870Fan Blade · damagedNR 2 ENG FAN BLADE DAMAGE. MX R2 ONE BLADE SET AND BLENDED OUT ALL OTHER DAMAGE. P/N DESCRIPTION OFF S/N
4114T15P02 BLADE, IHI0834W, 4114T15P02 BLADE IHI0836W.SDR CA110214018Plug · damagedDURING THE 600 HR/24 MONTHS INSPECTION ON ENGINE AND AIRFRAME, FOUND MISSING RIVETS ON COMPRESSOR WASH NOZZLE PLUG. REMOVED DEFECTIVE PARTS AND FOUND METAL FROM RIVET SHAVINGS IN COMPRESSOR WASH NOZZLE. SUSPECT METAL MAY HAVE PASSED THRU COMPRESSOR WASH NOZZLE
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