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 CA130528007Drive Shaft · cracked(CAN) FOUND A CRACK ON AN LPC DRIVE SHAFT REAR SPLINE END FACE. (SHAFT SERAL NUMBER 1680NNB) TAY 16009 IS HERE FOR A 2ND MID LIFE. THE CRACK INDICATION WAS CONFIRMED BY A SECOND FPI CHECK. THIS SHAFT ALSO HAS FRETTAGE ON THE FRONT SPLINESSDR UALA2013052903735Vane · burnedNR 1 ENGINE HPT FIRST STAGE VANES HAS ONE VANE BURNED THRU ON OD PLATFORM THAT EXTENDS INTO THE PLATFORM FILLET RADIUS LOCATED BEHIND LOWER IGNITER PLUG. ACCOMPLISHED NR 1 ENGINE BOROSCOPE INSPECTION OF HPT NGV. IAW DISPOSITION ECRA 7200-03291 MEASURES LESS SDR R61A201305260493Blade · damagedDURING CLIMB, CREW REPORTED A BIRD INGESTION INTO ENGINE NR 1. CREW DID NOT DECLARE AN EMERGENCY BUT DIVERTED TO PIT DUE TO HIGH LP VIBES. ACFT LANDED WITHOUT INCIDENT. MX FOUND 2 FAN BLADES DAMAGED, BUT CHANGED 4 TO KEEP ENGINE IN BALANCE IAW AMM. OPS CHECSDR UALA2013052403616Blade · damagedNR 1 ENGINE FOUR LPC BLADES DAMAGED ON L/E, BLADES NOT NUMBERED. BLENDED IAW MM72-31-02. CARRIED FORWARD RAISED FOR HFEC INSP TO BLADES (X4) TO BE ACP IAW NTM UAL PART 6 72-31-401 WITHIN 6 CYCLES.SDR EVCA2013080900001Compressor · failedWHILE IN THE TRAFFIC PATTERN, EXPERIENCED ENGINE FAILURE WHILE DEMONSTRATING A NORMAL TAKEOFF. BEGAN TO ACCELERATE FWD AND PASSED THROUGH 40 KNTS AND BEGAN TO CLIMB, THERE WAS A LOUD BANG AND A LEFT YAW OF ACFT, ACFT IS APPROX 20 FT AND 50 KNOTS. TRIMED HESDR UALA2013052803681Blade · nickedNR 1 ENGINE HAS ONE 1ST STAGE FAN BLADE WITH A L/E NICK LOCATED 5" FROM TIP IN AREA "A" & IS 0.060" DEEP. ACP BLEND TO LE OF BLADE IAW MM, BLEND WHITE DOTTED & CARRY FORWARD RAISED FOR HFEC INSP TO BE ACP WITHIN 6 CYCLES IAW NTM UAL PART 672-31-401. ACCOMPLISSDR UALA2013052403623Blade · dentedNR 2 ENGINE FIRST STAGE FAN BLADE NR 36 HAS TWO DENTS ON L/E. ON LOCATED TWO INCHES FROM TIP AND MEASURES 0.20 INCH DEEP AND ONE LOCATED SIX INCHES FROM MIDSPAN SHROUD AND IS 0.060 INCH DEEP. ACCOMPLISHED BLEND TO L/E OF BLADE NR 36 IAW MM.SDR UALA2013052403612Blade · nickedNR 2 ENGINE FAN BLADE NR 19 HAS NICK 4 INCHES FROM BLADE TIP. PERFORMED PRELIMINARY BLADE BLEND. ACCOMPLISHED HFEC AS REQUIRED REF MM AND NDT MANUAL PART 672-31-401. STILL REQUIRES ADDITION .020" BLENDING REF MM 72-31-02 AT BLADE NR 19. BLENDED BLADE ADDITSDR UALA2013052403611Blade · nickedNR 2 ENGINE FAN BLADE, NR 38 HAS A NICK IN THE L/E ONE INCH FROM TIP. PERFORMED PRELIMINARY BLADE BLEND ON BLADE NR 38.SDR UALA2013052303571Blade · damagedNR 2 ENG BLADE, NR 29 L/E DAMAGED. DAMAGE IS L/E IN AREA "F", REPAIRED IAW MM 72-31-02.SDR AALA20130522003Compressor · stalledCREW REPORTED COMPRESSOR STALLED ON RT ENGINE. EMERGENCY DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENGINE AT ON 05/22/2013. SYS GROUND CHECK NORMAL OPS. (OPEN)SDR UALA2013052103511Fairing · missingRT ENGINE LOOKING AFT FROM ENGINE 5 O'CLOCK POSITION COMPRESSOR INTERMEDIATE CASE FAIRING RT SIDE PANEL SECTION MISSING. REPAIRED PER AMM 72-34-05. REPLACED MISSING FAIRING.SDR UALA2013051303316Blade · nickedNR 2 ENGINE FAN BLADE NR 10 HAS NICK ON L/E. DAMAGE IS 10 INCHES FROM ROOT TO A DEPTH OF 1MM. DAMAGE BLENDED OUT IAW MM.SDR FDEA201305090952Compressor · stalledAFTER TAKEOFF LT ENGINE BEGAN SURGING AND HAD A NOTICABLE THUMP LIKE A COMPRESSOR STALL. ALT 2000' AGL. POWER AT CLIMB, RETARDED THROTTLE RETURNED TO DEPARTURE. PERFORMED BORESCOPE OF NR 1 ENGINE LP, IP, HP, COMPRESSOR AND LP, IP, HP, TURBINE IAW AMM 72-0SDR UALA2013051303293Blade · damagedNR 2 ENGINE 1EA FAN BLADE FAILS TAP TEST MARKED. REPLACED NR 2 ENGINE 1EA BLADE.SDR CA130509008Scroll · cracked(CAN) CRACK IN SCROLL FOUND BY AME AFTER COMPRESSOR ASSY WAS REMOVED FOR LOOSE PERCUSSION WELDED ATTACHMENT STUDS. COMPRESSOR ASSY BEING SHIPPED FOR REPAIR. SCROLL, SN FU40784. SCROLL TSN TO FOLLOW.SDR ZD4R20130530610Retaining Ring · dislodgedA CHIP LIGHT ILLUMINATED, CLEANED CHIP PLUGS AND RETURNED ENGINE BACK TO SERVICE. APPROX 11 HOURS LATER, CHIP LIGHT ILLUMINATED AND METAL WAS MORE SIGNIFICANT THAN BEFORE. DECIDED TO PULL THE ENGINE AND SEND IT IN FOR REPAIR. THE ENGINE WAS DISMANTLED AND IT SDR SWAA2013050815841Compressor · stalledAIR TURNBACK - AFTER TAKEOFF NR 2 ENGINE COMPRESSOR STALL. REMOVED AND REPLACED NR 2 ENGINE PER TC AND MM.SDR UALA2013050703164Blade · damagedNR 1 ENGINE FAILED VIBRATION TEST. FIRST STAGE FAN BLADES REMOVED PER MM. BLADE DAMAGE. BLADE AND DAMAGE IS OUT OF LIMITS PER 72-31-11-200-010-B. PER AMM MAX BLEND LIMIT IS .040, AREA BLENDED MEASURES .0625 DEEP. REPLACED NR 14 BLADE PER MM 72-13-11-400SDR SWAA2013050115387Compressor · stalledINFLIGHT SHUTDOWN/AIR RETURN/DECLARED EMERGENCY. NR 2 ENGINE COMPRESSOR STALL DURING CLIMBOUT. REMOVED AND REPLACED NR 2 ENGINE PER TC.SDR HALA2013042800047Blade · bentNR 1 ENGINE HAS BENT BLADE, 7.5 INCHES FROM FILLET ON NR 9 FAN BLADE. PERFORMED AMM 72-31-41-200-801-A, FOUND WITHIN LIMITS IAW AMM.SDR XV6A2013042700004Engine · bird ingestionBIRD STRIKE NR 1 ENGINE, VIBRATION AT 3.8 FOR 1 MINUTE REDUCE TO BELOW 3.0 FOR THE REST OF FLIGHT. OTHER INDICATIONS NORMAL. ENGINE INSPECTED AND FOUND DAMAGE TO 8 EACH FAN BLADES. NO OTHER DEFECTS NOTED PER AMM 71-00-47 AND GMM 9-13. REMOVED AND REPLACED SDR UALA2013043003015Blade · nickedNR 1 ENGINE FIRST STAGE FAN BLADE NICKED ON LEADING EDGE APPROX 12 INCHES FROM OUTBOARD END WITH A DEPTH OF .010. ACCOMPLISHED FIRST BLEND ON BLADE IAW AMM 72-31-02. ACCOMPLISHED HFEC AS REQUIRED REF NDT MANUAL PART 6 72-31-401. NO CRACKS FOUND.SDR SWAA2013042415148Case · crackedNR 1 ENGINE CRACKED IN FAIN CASE A1 FLANGE, O/B BOLT SECURING FIRE DETECTION LOOP AT THE 12:30 POSITION. REPAIRED.SDR JBZA20130429001Compressor · fodACFT WAS DEPARTED. DURING LIFT OFF, NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL ASSOCIATED WITH UNUSUAL NOISES. LANDED WITHOUT INCIDENT. GROUND OBSERVERS REPORTED SEEING SEVERAL THREE FOOT FLAMES COMING FROM NR 2 ENGINE EXHAUST ACCOMPANIED BY SOUNDS LIKE A SDR UALA2013041602604Blade · nickedNR 1 ENGINE FAN BLADE NR 33 HAS A NICK ON LEADING EDGE 1 INCH FROM TIP. REPAIRED DAMAGE REF AMM.SDR UALA2013041502594Blade · nickedNR 2 ENGINE HAS A NICK IN FAN BLADE. BLENDED ONE FIRST STAGE BLADE ON NR 2 ENGINE REF MM.SDR UALA2013041002420Blade · tornRIGHT ENGINE FAN BLADE NR 15 HAS A TEAR IN THE LEADING EDGE, NEAR THE TIP. BLENDED DAMAGE OUT OF NR 2 ENGINE. FAN BLADE NR 15. DAMAGE WAS IN AREA A, WAS REMOVED PER AMM 72- 31-02.SDR Q0MF20130409003Blade · damagedAIRCRAFT B-16822 EXPERIENCED ENG NR 1 UNABLE TO ACCELERATE ACCOMPANIED ENG SURGE ABOUT TAKEOFF, THE CREW DECIDED TO ABORT TAKEOFF. THEN "ENG 1 FAIL" AND "ENG EXCEEDENCE" EICAS MESSAGE APPEARED DURING TAXIING BACK. MECHANIC PERFORMED ENG NR 1 INSPECTION FOUNDSDR REXA2013040500727Blade · lack of lubeON FLIGHT 3814 (ATL TO IAD) ON TAKEOFF CREW NOTICED THAT THE LEFT ENG FAN VIBE IN YELLOW (1.9) HAD TO KEEP POWER BELOW 76% N1 TO KEEP VIBRATION IN GREEN RANGE. CREW ACCOMPLISHED QRH AND PERFORMED AIR RETURN TO ATL. APPLIED LUBRICATION ON THE FAN BLADE IAW CRSDR UALA2013040502287Sealant · damagedLEFT ENGINE HAS STRIP OF MATERIAL HANGING. WHEN VIEWED FROM BEHIND, IT IS 10 O'CLOCK. 10 INCH PIECE OF SILASTIC REMOVED AT 10 O'CLOCK POSITION ON NR 1 ENGINE EXIT CASE LINER OUTER SEGMENT. REPLACED APPLIED SEALANT IAW AMM.SDR UALA2013040402222Blade · damagedNR 18 FAN BLADE REPORTED AS HAVING DAMAGE AT BLADE TIP. REF BLADE IS ON NR 2 ENGINE. DAMAGE MEASURES .156 X .5 IN. IN AREA 1 OF BLADE TIP. OK TO CONTINUE FOR 25 FLT HOURS. BLENDED BLADE 18 ON ENGINE NR 2.SDR UHLA2013040200111Compressor · damagedAT FL180 E1 SURGED REPEATEDLY. ENGINE 1 CONTROL FAULT CAME ON EICAS. FOLLOWED QRH AND THRUST WAS UNSTABLE. PERFORMED INFLIGHT SHUTDOWN OF ENGINE 1 AND RETURNED TO DTW. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MTX PERFORMED BOROSCOPE OF ENG 1 IAW GE MMSDR UALA2013040202118Vane · erodedNR 2 ENGINE EXIT VANE 5:30 POSITION, LEADING EDGE STRIP, MISSING AND VANE HAS EROSION. REPAIRED IAW AMM 72-33-02 TO BE REPLACED AFT 100 HR INSPECTION.SDR UHLA2013032900098Blade · damagedON TAKEOFF, TWO BIRDS INGESTED INTO NR 2 ENGINE ON T/O, LP VIBE 2.8 AT CLIMB POWER. AFTER COMPLETION OF THE AFTER TAKEOFF CHECKLIST, DECIDED TO RETURN TO FIELD. DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED BIRD STRIKE INSPECTION, CLEANED DEBRISSDR UALA2013032802000Liner · damagedPIECE OF HONEYCOMB RUB STRIP MISSING ON NR 2 ENGINE AT 6:00 AND 6:30 POSITIONS. REPAIRED FAN CASE ATTRITION LINER AT 6:00 AND 6:30 POSITIONS PER MT 72-017 REV E.SDR SWAA2013040214401Compressor · stalledABORTED TAKEOFF/DECLARED EMERGENCY. TWO VIOLENT COMPRESSOR STALLS ON NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE IAW MT.SDR UALA2013032701942Rub Strip · missingRIGHT ENGINE HAS 1.75 INCH BY 1 INCH SECTION OF RUB STRIP MISSING AT 7 O'CLOCK POSITION. INSPECTED AREA FOUND TO BE WITHIN LIMITS OF AMM 72-33-01-601. AREA LESS THAN 3.0 INCHES IN DIAMETER. REPAIR IN 500HRS, OR 200 CYCLES WHICHEVER IS LESS. REPAIRED AREA.SDR UALA2013032902034Blade · nickedSEVERAL BLADES IN INLET OF NR 1 ENGINE HAVE NICKS IN THEM. BLENDED BLADES PER 72-31- 02. PERFORMED HFEC INSPECTION OF BLADES REF NDT MANUAL PT 6 72-31-401, NO CRACK INDICATIONS.SDR UALA2013032501821Guide Vane · damagedNR 2 ENG 9 O'CLOCK POSITION IGV MISSING TAPE FROM PREVIOUS REPAIR. TAPE MISSING FROM PREVIOUS APPLICATION REPAIR. TAPED IGV AT 9 O'CLOCK POS PER AMM. NO FURTHER DAMAGE NOTED.SDR UALA2013032201810Blade · damagedNR 2 ENGINE LPT FAN BLADE HAS A NICK APPROXIMATELY 4 INCHES FROM LEADING EDGE BLADE TIP. ACCOMPLISHED EDDY CURRENT IAW NDTM 72-31-401, NO CRACKS DETECTED.SDR UALA2013032201807Stator Vane · delaminatedRT ENGINE, NINE FAN STATOR VANES CHIPPED AND PROTECTIVE COVERING DELAMINATING. REPAIRED VANES WITH APPROVED TAPE PER MM.SDR UALA2013032001710Blade · bentNR 1 ENGINE FAN BLADE NR 22 HAS A BEND IN THE LEADING EDGE ABOUT 4.5 INCHES FROM TIP. REF AMM 72-31-11-0601, BLADE IS NOT WITHIN LIMITS. REPLACED NR 22 BLADE.SDR UALA2013031801625Blade · damagedNR 1 ENGINE BLADE NR 15 REQUIRES REWORK. ACCOMPLISHED BLEND IAW MM72-31-02-801 AND ACP HFEC INSPECTION PER NTM UAL PART6 72-31-401.SDR UALA2013031801631Blade · damagedNICK IN FAN BLADE FOR RIGHT ENGINE. INSPECTED BLADE. BLADE HAS A TEAR IN AREA 2, 24.75 INCH FROM ROOT, DEPTH IS 0.260. REPAIRED PER MM 72-31-02-801.SDR UALA2013031301491Blade · dentedNR 1 ENGINE, NR 1 BLADE DENTED. REMOVED DENT FROM 22.5 INCH FROM ROOT AND 15-64TH DEEP PER MM 72-31-02. ACCOMPLISHED HFEC BLADE INSPECTION PER NDT PART 6 72-32-401. NO DEFECTS NOTED.SDR UALA2013031201469Blade · dentedNR 1 ENGINE FAN BLADE NR 10 HAS A DENT ON THE LEADING EDGE 3 INCHES FROM THE TIP WITH 1-4 OF AN INCH IN DEPTH. DAMAGE REMOVED AS PER MM. CF CREATED TO HAVE EDDY CURRENT INSPECTION. LEFT ENGINE NR 10 FAN BLADE REPAIRED AS PER PTT 3802004. IT NEEDS EDDY CURRSDR UALA2013031401548Blade · dentedNR 1 ENGINE FAN BLADE 10 HAS A DENT ON THE LEADING EDGE 3 INCHES FROM THE TIP WITH 1-4 OF AN INCH IN DEPTH. DAMAGE REMOVED AS PER MM. CF CREATED TO HAVE EDDY CURRENT INSPECTION. EDDY CURRENT INSPECTION TO BE ACCOMPLISHED WITHIN SIX FLIGHT CYCLES. EDDY CURRSDR UALA2013022801215Blade · damagedBLADE FOD DAMAGE ON LEFT ENGINE NOTED ON SEVERAL BLADES 18 INCHES FROM BLADE TIP-SMALL NICKS. NICKS ARE WITHIN LIMITS PER MM. THE 18 INCHES FROM BLADE TIP IN (AREA 5) NICKS NEED TO BE BLENDED WITHIN 25 HOURS.SDR CA130307007Compressor · dirty(CAN) SMOKE TOILET CAUTION MESSAGE DURING TAKEOFF ROLL. CREW ABORTED TAKEOFF. MESSAGE CLEARED SHORTLY THEREAFTER. FOUND RT ENGINE COMPRESSOR BLADES TO BE SOILED. SUSPECT NR 3 CARBON SEAL IS LEAKING OIL INTO 10TH STAGE BLEED AIR AND CAUSING SMOKE TOILET EICA
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