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 USAA2010060991095Compressor · damagedFLT 2020 - DCA-BOS - EMERGENCY LANDING - LEVEL FLIGHT N1 AT 65 PERCENT ENGINE COMPRESSOR STALL. REDUCED THRUST, EASED NR 2 THRUST LEVER FORWARD. MODERATE TO SEVERE VIBRATION. RETURNED BELOW 46 PERCENT N1. VIBRATION DISAPPEARED. ENGINE ANTI-ICE=ON, WING ASDR HALA2010060300239Compressor · stalledOPEN - AIR TURN BACK - AT APPROX 3'000 FT. LT ENGINE SHUTDOWN. COMPRESSOR STALL ALERT WAS FIRST VISIBLE ALERT DISPLAYED. REPAIR IN WORK.SDR HALA2010052200231Shroud · damagedETOPS SIGNIFNICANT SYS - ON WALKAROUND FOUND ABRADABLE SHROUD DAMAGE ON NR 1 ENG AT 6 O'CLOCK POS DAMAGE AFT OF FAN BLADES APPROX 24" X 1". REPAIRED IAW M105 FILE NR 594099.SDR CA100611001Compressor Wheel · seizedACFT LANDED AND START WAS ATTEMPTED WITH HIGH T4, START ABORTED, SECOND START WAS ATTEMPED WITH SAME RESULT ACFT REMAINED OVERNIGHT. DURING START ATTEMP THE FOLLOWING MORNING THE AXIAL COMPRESSOR WHEEL WAS FOUND SEIZED. ENGINE WAS REMOVED AND SENT FOR INVESTISDR 2010FA0000697Plenum · wrong partPLENUM CHAMBER FOUND INSTALLED IS INCORRECT FOR THIS ENGINE MODEL IAW MFG ILLUSTRATED PART CATALOG 72-00-91, REV 16.SDR ASMF201005001Shroud · groovedDURING THE MX INSP, AFTER THE LAST FLIGHT OF THE DAY, IT WAS DETECTED IN THE LT ENGINE, THE FAN BLADES WITH PLASTIC BAG REMAIN. MX PERFORMED A FOD INSP IAW MM TASK 71-00-00-800-802-F00, DETECTING A GROOVE 1.125 INCHES WIDE ON 360 DEGREES OF ABRADABLE SHROUD. TSDR UALA2010051401640Blades · missingWHILE INSPECTING 14TH STAGE BLADES THRU AP7. NOTICED 13TH STAGE BLADES HAS 2 BLADES WITH MISSING MATERIAL AT T/E AND TIP. APPEARS TO BE OVER THE .250 MAX IN IN BOTH DIRECTIONS. CF IS FOR NR 2 ENG S-N 726525. CONTACTED SAMC ENG CONTROLLER & ENGINEER AND BOTH ASDR HEEA128373Frame · crackedFOUND CRACKED FRONT FRAME AT 6 O'CLOCK POSITION INSIDE INLET AREA. OIL LEAKAGE SEEMED TO BE CARRIED THROUGH TO THE PARTICLE SEPARATOR BLOWER AND DEPOSITED ON THE TAILBOOM, RATHER THAN INTO THE COMPRESSOR. SENT ENGINE FOR REPAIR.SDR UALA2010051001586Blade · nickedNR 1 ENGINE 3 BLADES HAVE SEVERAL NICKS. REPAIRED BLADE AREAS MARKED WITH WHITE DOTS, WILL NEED EDDY CURRENT CHECK. ACCOMPLISHED BLADE HFEC NDT PER MM. INDICATIONS NORMAL. BLADE REPAIRS WITHIN LIMITS.SDR P5CA2010050601635Compressor · damagedMEMO MESSAGE "VVVVVV" DISPLAYED AT 1515Z AT FL 360, ENGINE 3 N2 VIBRATION AT 5.0. ALL OTHER PARAMETERS WERE NORMAL AND MONITORED. AT APPROXIMATELY 12,000 FT, NR 3 ENGINE FAILED. QRH PROCEDURES ACCOMPLISHED. INSPECTION OF TAILPIPE REVEALED NO METAL. BOROSCSDR UALA2010050401507Compressor · stalled(ENG 1 COMPRESSOR STALL), CHECK INLET, EXHAUST AND MASTER CHIP DECTECTOR, REPORT FINDINGS TO SAMC, OPBLM EMC ARSHAD. LCL FBO ACCOMPLISHED VISUAL INSP OF ENG 1 INLET & EXHAUST, NO DEFECTS NOTED, CHECKED MASTER CHIP DETECTOR, NO DEFECTS NOTED. PFR SHOWS FLT PHASDR UALA2010042901445Compressor · stalledENG COMPRESSOR STALL IN FLIGHT. ENG POSITION UNKNOWN. ENG RECOVERED AND CONTINUED OPERATING. IMMED PRECEDING STALL, ENG POWER WAS ACCELERATING AT CRUISE OR CLIMB POWER. SELF CLEARING COMP STALL. ACP STALL CHECKS ON BOTH ENGS. CREW DEBRIEF- AT 3000FT AFTER TSDR ASMF20100405Compressor · damagedDURING A BORESCOPE INSP OF THE HPC AND HPT MODULES OF RT ENGINE WERE DETECTED 41 BLADES OF HPC 8TH STAGE AND 23 BLADES OF 9TH STAGE WITH TEARS, NICKS, BENDS AND MISSING MATERIAL FROM THE LEADING TO THE T/E. OPENSDR UALA2010042601392Blade · damagedRIGHT ENG HAS ONE DAMAGED FAN BLADE. REPAIRED NR 2 ENG FAN BLADE IAW MM. EDDY CURRENT INSP ACP'D. NO DEFECTS FOUND. RPR WITHIN LIMITS FOR CONTINUING SERVICE.SDR HALA2010042300190Guide Vane · damagedETOPS SIGNIFICANT SYS - NR 1 ENG FAN EXIT GUIDE VANE PLATFORM DAMAGED AT ABOUT 9:30 POS (NOTE VANE ROOT AREA NOT AFFECTED). REPAIRED PLATFORM IAW AMM72-33-02 OK FOR SVC.SDR USAA2010042390817Blades · brokenFLT 1511, AIRCRAFT EXPERIENCED NR 1 ENGINE ROLLBACK WITH 9.9 N1 VIBRATION WHILE EN ROUTE. CREW DECLARED AN EMERGENCY AND THE FLIGHT WAS DIVERTED TO BNA. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. VENDOR REPORT IDENTIFIED 3RD STAGE LPT BLADE SET WITH SDR 2010FA0000390Diffuser · damagedCUSTOMER CALLED TO REPORT AN IFSD OF HIS ENGINE DURING AN ACFT FERRY FLIGHT. THE ACFT WAS GOING TO TROUBLESHOOT AN OIL SMELL IN THE CABIN COMPLAINT. ENGINE 216118 HAS 1223 HOURS REPORTED AT THIS TIME. A FIRE WARNING ANNUNCIATED AS THE AIRCRAFT WAS PASSING FSDR UALA2010041901299Seal · damagedNR 1 ENG, NR 17 BLADE ROOT, RUBBER FAIRING SEAL DISBONDING. REPLACED FAIRING AND SEAL ASSY.SDR C8GA201000007Fan Blade · damagedDURING TAKEOFF, ACFT ENCOUNTERED A BIRD STRIKE, TAKEOFF WAS ABORTED. POST FLIGHT INSP WAS PERFORMED NOTING THAT THE NR 1 ENGINE HAD DAMAGED FAN BLADES. R & R (5) EA SETS OF FAN BLADES. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR UALA2010041401259Case · fodLOOSE METAL PIECE WEDGED AGAINST A BRACE ON THE EXHAUST SIDE OF THE LT ENGINE AT 11:30 POS PART WAS FACE OF COMPRESSOR INTERMEDIATE CASE FAIRING. REMOVED METAL. REPLACED COMPRESSOR INTERMEDIATE CASE FAIRING IAW MM.SDR ASMF201004001Blades · damagedDURING A BORESCOPE INSP OF THE HPC 1, 4 AND 9 STAGES BLADES OF THE RT ENGINE WAS DETECTED. 1 BLADE OF THE HPC 1ST STAGE WITH L/E TIP CURLED 90 DEGREES OUT OF LIMITS IAW 72-00-00, PARA 5H (L) (7), PAGE 625; WITH DIMENSIONS OF 3.5 INCHES LENGTH AND 1.25 INCHES WSDR CA101005003Compressor Blade · missingENGINE WAS REMOVED FROM ACFT ON APRIL 03, 2010 DUE TO PROPELLER STRIKE & SUDDEN STOPPAGE INCIDENT. DURING DISASSEMBLY OF THE COMPRESSOR STACK, THE 2ND STAGE COMPRESSOR DISK WAS NOTED WITH MISSING QTY 1 COMPRESSOR BLADE (NOT INSTALLED AT PREVIOUS BUILD) . THESDR 2010FA0000428Compressor · damaged(QEMY) DURING INCOMING INSP OF THE SUBJECT HP COMPRESSOR, 8-10 SPOOL (IPC 72-31-00-01-590), 1-OFF INDICATION HAS BEEN IDENTIFIED ON THE RAISED EBN LAND SITUATED INTERNALLY BETWEEN THE STAGE 9 AND 10 DISKS. THE INDICATION HAS BEEN DETECTED DURING THE FLUORESCESDR HALA2010040100149Blade · nickedETOPS SIGNIFICANT SYS - ON PRE-FLIGHT INSP FOUND SMALL NICK ON RT ENG BLADE NR 27. REPAIRED IAW AMM 72-31-02. NO CRACKS NOTED. OK FOR SERVICE. EDDY CURRENT INSP IAW AMM 72-31-02. NO CRACK IND.SDR HALA2010033100145Fan Blade · damagedETOPS SIGNIFICANT SYS - NR 2 ENG FAN BLADE NR 1 TIP DAMAGED. REPAIRED IAW AMM 72-31-02. EDDY CURRENT INSPECTED IAW AMM 72-31-02, NO CRACK IND.SDR AALA20100328DFW01Compressor · stalledDFW - CREW REPORTED AFTER CLIMB THE RIGHT ENGINE COMPRESSOR STALLED. CREW SHUT DOWN ENGINE (SINGLE ENGINE TIME 15 MINUTES) EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE RIGHT ENGINE AND ISOLATORSSDR ASMF201004002Blades · damagedDURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENGINE WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN THE 1ST, 2ND, 3RD AND 4TH STAGES IAW AMM 72-00-00, PARAGRAPH 5H. THE FINAL REPAIR DETAILS OR ENGISDR ASMF20100321001Blade · damagedDURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENG WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN THE 1ST, 2ND, 3RD AND 4TH STAGES IAW AMM 72-00-00, PARAGRAPH 5H. THE FINAL REPAIR DETAILS OR ENGINE SDR HALA2010032000129Blades · damagedETOPS SIGNIFICANT SYS -ON OVERNIGHT INSP FOUND NR 2 ENG COMPRESSOR INLET BLADE FOD DAMAGE ON OUTER SECTION OF BLADE. BLENDED FOD DAMAGE ON NR 2 ENG COMPRESSOR BLADE NR 24 IN L/E AREA A. DAMAGE FOUND TO BE LESS THAN
.125". INSPECTED DAMAGE AREA IAW AMM 72-SDR XE5RTAES086Compressor · damagedTHE OPERATOR REMOVED THE ENGINE FROM SERVICE DUE TO A SURGE AND REJECTED TAKEOFF. BORESCOPE INSPECTION FOUND EXTENSIVE HPC STAGE SIX BLADE DAMAGE. TAESL CONFIRMED THIS DAMAGE DURING TEARDOWN OF THE ENGINE AFTER 5616 HOURS SINCE LAST FULL REFURBISHMENT AT ANOSDR ASOA201000395Blade · lack of lubeEXESSIVE VIBRATION IN LT ENGINE DURING CLIMB OUT. ( 1.8 ) AT CLIMB POWER . VIBRATION COULD BE FELT IN COCKPIT (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) REMOVED AND REINSTALLED NR 1 ENG. FAN BLADES IAW AMM 72-21-02. LUBED FAN BLADES IAW ESSDR HALA2010031600119Stator Vane · damagedETOPS SIGNIFICANT SYSTEM, DURING PRE-FLT LT ENG STATOR VANE FAN SECTION 6 O`CLOCK MISSING PART OF L/E (VANE REMOVED PER AMM, REPLACE AT NEXT ENG CHANGE). OK TO CONTINUE PER TASK72-33-02-206-000-N00.SDR ASAA1057542Ring · nickedNR 2 ENGINE FWD ANODIZED RING NICKED AT 10 O’CLOCK POSITION. INSPECTED FAN CASE AND FOUND TO BE WITHIN REPAIRABLE LIMITS PER AMM 72 24 01 200 801 F00. REPAIRED SMALL NICK PER AMM 72 24 01 200 801 F00 PARA F, OK FOR CONTINUED SERVICE.SDR SWAA101192Compressor Blade · damagedAIR TURNBACK / DECLARED EMERGENCY / ENGINE SHUTDOWN. LOUD "POPPING" NOISES FROM NR 1 ENGINE DURING ROTATION. ENGINE INDICATIONS NORMAL. PUSHED THRUST LEVERS UP & NOISES CEASED FOR 6-7 SECONDS. THEN RESUMED. INDICATIONS STILL NORMAL. DECLARED EMERGENCY, TSDR 2010F00052Blades · damagedTHIS ACFT HAD FOD DAMAGE NOTED DURING THE MX WALK-AROUND IN THE NR 2 ENGINE INLET, ENG SN 330606. THE DAMAGE CONSISTED OF 4 BENT BLADES AND 7 NICKED BLADES. NO DEFECTS NOTED TO THE HPC DURING BORESCOPE INSP. THE FAN CASE INLET HAD 6 SCRATCH/GOUGES.SDR AALA20100222CCS01Blade · damagedMAR - CREW REPORTED DURING TAKEOFF RIGHT ENGINE HAD BIRD STRIKE. ENGINE PRODUCED LOUD PITCH CHANGE FOLLOWED BY HIGH VIBRATION REDUCED POWER TO MAINTAIN VIBRATION IN NORMAL RANGE VIBRATION CONTINUED TO CLIMB UNTIL POWER SETTING JUST ABOVE IDLE. EMERGENCY DECLSDR AALA20100221TUL03Blade · damagedMAR - CAPTAIN REPORTED THAT AIRCRAFT HAD BIRD STRIKE TO RIGHT ENGINE ON ROTATION. ENGINE WAS PULLED BACK BUT NOT SHUT DOWN. EMERGENCY DECLARED RETURNED MAR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 6 AND NUMBER 7 BLADES. ALSOSDR USAA2010022290424Compressor Blade · damagedFLT 685 - PHX-EWR - IFSD/RETF - AT LIFTOFF, EXPERIENCED MULTIPLE COMPRESSOR STALLS AND EGT EXCEEDENCE ON THE NR 1 ENGINE. SHUTDOWN NR 1 ENG AND RETURNED TO PHOENIX. REMOVED AND REPLACED THE NR 1 ENGINE PER R5M71302. ***SUPPLEMENTAL*** HPC ROTOR 3 BLADE LIBESDR ALGA2191045003Mount · crackedFOUND EXCESSIVE CRACKING ON AFT FLANGE OF REAR COMPRESSOR MOUNT.SDR RYNA2010002170004Fan Blade · bentRIGHT ENGINE HAD 3 COMPRESSOR STALLS DURING CLIMB THROUGH 16,000 TO 17,000 FT. DURING TROUBLESHOOTING FOR COMPRESSOR STALL FOUND DAMAGED 1ST STAGE FAN BLADE. PERFORMED VISUAL INSP OF BLADE DAMAGE, BLADE BENT 1 ¼ (L/E TO T/E) AND 1 24/32 (TIP TO SHANK) WITH NSDR UALA2010021500551Blades · damagedNR 2 ENG HAD BIRD STRIKE. IAW CREW, VIBS WENT TO 1.1 UNITS AT STRIKE THEN WAS NORMAL REST OF FLT. NR 2 ENG HAS APPROX 8 FAN BLADES DAMAGED WITH EVIDENCE OF SOME BIRD MATERIAL GOING THROUGH CORE. 1 ADDITIONAL BLADE IS DAMAGED NEAR MIDSPAN. BLADES DAMAGED ARE SDR CA100211005Adapter · cracked(CAN) ACFT WAS IN CRUISE AT 800 FT WHEN THE PILOT HEARD A HUMMING NOISE FOR ABOUT 2 SECONDS. AFTER THE 2 SECONDS THE ENGINE SHUTDOWN. PILOT AUTO ROTATED AND LANDED HELICOPTER. ENG HAD FLAMES COMING OUT OF THE EXHAUST STACKS UPON LANDING BUT QUICKLY DISSIPATEDSDR UALA2010021100526Compressor · stalledCREW REPORTS RT ENG HAD A COMPRESSOR STALL AT 130KTS DURING TAKEOFF. (ONE BANG). PARAMETERS DECREASED SLIGHTLY THEN RETURNED TO NORMAL. NO EXCEEDANCES OCCURED, ENGINE IS OPERATING NORMALLY. CREW ALSO STATES THEY HAD A 30 DEGREE CROSSWIND AND LIGHT SNOW AT THESDR MASA2010020900135Fan Blade · lack of lubeRIGHT ENGINE VIB AT 1.8. C/W FAN BLADE LUBE.SDR CA100209011Retaining Ring · cracked(CAN) ENG PRODUCED A CHIP LIGHT DURING OPERATION AND METALLIC DEBRIS OF SIGNIFICANT SIZE WAS FOUND ON THE LOWER GEARBOX CHIP PLUG DURING LINE MX INVESTIGATION. ENG WAS SUBSEQUENTLY REMOVED FROM SERVICE. ON DISMANTLE TO INVESTIGATE CONDITION OF THE FOLLOWING SDR MASA2010020700116Fan Blade · lack of lubeON CLIMBOUT IN MEMPHIS LEFT ENGINE VIBRATION WAS HIGH 1.6MILS BUT IN THE GREEN BAND AT CRUISE WHEN POWER REDUCED VIB WENT TO 1.8. CREW WAS ABLE TO KEEP THE VIB IN THE GREEN DURING THE FLIGHT. THE FLIGHT ATTENDANTS CALLED TO ASK ABOUT THE VIBRATION AND THE LOSDR 2010FA0000174Blades · damagedPILOT EXPERIENCED COMPRESSOR STALL DURING FLIGHT WITH LOUD NOISE AND YAW OF ACFT. PILOT EXPERIENCED LOSS OF ENGINE POWER AND PROCEEDED TO LAND ACFT. UPON INSP MX FOUND 1 EA 1ST STAGE COMPRESSOR BLADE BROKEN OFF AT ROOT AND LAYING IN PLENUM CHAMBER IN FRONT OSDR AALA20100203SAN01Compressor · stalledSAN - CREW REPORTED RIGHT ENGINE COMPRESSOR STALLED TWICE DURING CLIMBOUT. EMERGENCY DECLARED RETURNED SAN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT SAN ON 02/04/2010. SYSTEM GROUND CHECK NORMAL OPERATION.SDR HALA2010020300050Compressor · damagedDURING EXTERNAL AIR START, ABORTED START ATTEMPT DUE TO HIGH EGT (680 DEGREES). R & R LT EEC IAW AMM 73-21-01, CONDITION SAME. ACCOMPLSHED BOROSCOPE INSP IAW AMM 72-50-00. FOUND HPC STAGES 9 & 20 AND STATOR DAMAGED DUE TO FOD. R & R NR 1 ENGINE. OPS AND LEASDR SWIA201023577Blade · damagedIN CRUISE VIBRATION ON NR 2 ENGINE AT FULL SCALE AFTER FEELING AND HEARING A THUMP. (FLT 4719) REPLACED TWO PAIR OF FAN BLADES.
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