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 2003F00298Blade · damagedIN FLIGHT NR 3 ENGINE COMPRESSOR STALLED TWICE AND HAD HIGH EGT INDICATION. ENGINE NR 3 WAS SHUTDOWN IN FLIGHT AND FLIGHT CONTINUED TO KMIA WITHOUT FURTHER INCIDENT. MIA MAINTENANCE INSPECTED ENGINE NR 3 AND FOUND THE C-9 THROUGH C-13 BLADES DAMAGED. ENGNE SDR 2003UALA00281Rub Strip · debondedDIVERTED DUE TO NR 1 ENGINE COMPRESSOR STALL. COMPRESSOR STALL CAUSED BY HIGH PRESSURE COMPRESSOR (HPC) 6TH STAGE (C6) BLADE DAMAGE WHICH WAS IN TURN CAUSED BY HPC C6 RUBSTRIP COATING DISBONDING. SERVICE BULLETIN 72-0369 IS IN PLACE TO UPGRADE COATING TO AVOSDR CHI2003F00002Compressor Wheel · crackedTWO CRACKS WERE FOUND IN THE 1ST STAGE COMPRESSOR DISC (PN210133105) DURNG AN INSPECTION. THE CRACKS ARE LOCATED IN TWO OF THE COMPRESSOR BLADE RETENTION SLOTS. THIS IS THE SECOND TIME CRACKS HAVE BEEN FOUND EMANATING FROM THE BLADE RETENTION SLOTS OF THIS PSDR AWXA200300270Vane · damagedWHEN PREPARING FOR TAKEOFF AT DFW EN ROUTE FOR PHX WHEN THROTTLES ADVANCED RECEIVED COMPRESSOR VANE FAULT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE RATIO BLEED CONTROL IAW T/C R5M75002, AND LUBRICATED THE 13TH STAGE BLEED VALVE IAW BMM 75-31-0, PG. 602. SDR GTIA030139Blade · damagedNR 1 ENGINE 1 EA C1 BLADE HAS .2500 IN/ SQ CHIP OUT 2 INCHES FROM PLATFORM OF BLADE, 1 EA C1 BLADE HAS .3750 FLAT ON L/E 2 INCHES FROM PLATFORM OF BLADE. REMOVED AND REPLACED 4 EA BLADES FROM NR 1 ENGINE IAW MM.SDR 6370103Compressor Wheel · crackedDISCOVERED DURING SCHEDULED MAINTENANCE. RT ENGINE FAN DISK FOUND CRACKED WHILE PERFORMING SCHEDULED NON DISTRUCTIVE TESTING IAW AD AND MFG SB. FAN DISK PN BRR20791, SN CTDK 7185 ENGINE TYPE BR700-710A1-10, SN 11386. REMOVED LP FAN MODULE 31, PN M31-113, SNSDR MEX2003063Blade · damagedFLT 911 - MTY-MEX - DURING MAINTENANCE INSPECTION, DETECTED A FAN BLADE OF ENGINE NR 1 WITH DAMAGE. THE INSPECTOR VERIFIED THE BLADE AND WAS OUT OF LIMITS. THE TECHNICIAN BLENDED THE BLADE IAW MM 72-00-00, ALL CORRECT. (M)SDR IXXA0300024OCompressor · stalledAFTER DEPARTURE FROM GSO DURING CLIMB OUT TO TOL. WHEN POWER REDUCED FROM CLIMB TO CRUISE, CREW NOTED NR 1 ENGINE COMPRESSOR STALL. PRECAUTIONARY ACTION WAS TAKEN AND ENGINE SHUTDOWN FOR REMAINDER OF FLIGHT. CREW MADE AN UNEVENTFUL LANDING IN TOL.SDR DLM88030224Compressor · stalledRT ENG WITH NORMAL PWR T/O AT ROTATION HAD A COMPRESSOR STALL. THE ENG ROLLED BACK AND EGT 500 DEGS RISING. REPLACED ENGINE.SDR CA030307002Engine · vibration(CAN) PILOT REPORTED AIRFRAME VIBRATION WHEN POWER RETARDED DURING DESCENT (FROM 94 TO 88 PERCENT). ITT FLUCTUATING AS LOW AS 200 DEGREES. ENGINE N1 & N2 FLUCTUATES .5 TO 1.5 PERCENT DURING CRUISE WITH LOW BUZZING.UPON INSPECTION OF INLET, FOUND FOD DAMAGE ON SDR 048548Gas Generator · failedCREW WAS ON TAKE OFF ROLL WHEN POWER WAS APPLIED TO THE NR 2 ENGINE. THE CREW HEARD A LOUD BANG FROM THE RIGHT SIDE OF THE AIRCRAFT. THEY ABORTED THE TAKE OFF AND TAXIED BACK DOWN TO THE GATE. THEY PROCEEDED TO PERFORM A CHECKLIST BY VISUALLY INSPECTING ENGINESDR CA030318007Stator Vane · fractured(CAN) PILOT REPORTED A LOUD BANG AND TORQUE DROPPING OFF ON LANDING. THE SUBJECT ENGINE WAS REMOVED FROM SERVICE AND SENT FOR INVESTIGATION AND REPAIR. INVESTIGATION RESULTED IN THE FINDING OF ONE MISSING FIRST STAGE STATOR VANE (I.E. 1 OF 44) FROM THE 1ST SSDR AWXA200300226Compressor · stalledDURING TAKEOFF AT BOI EN ROUTE FOR PHX HEARD LOUD POP ON LT SIDE OF AIRCRAFT, SUSPECTED COMPRESSOR STALL AND REJECTED TAKEOFF AT 90 KTS. BOISE MAINTENANCE PERFORMED INSPECTION OF THE NR 1 ENGINE IAW BMM 71-00-00 PG. 248 & 249, ENGINE RUN AT ALL PARAMETERS WAS SDR CA030306005Engine · failed(CAN) ENGINE WAS REMOVED FROM WING AFTER WHAT WAS SUSPECTED TO BE A NR 3 BEARING FAILURE AND OIL CONTAMINATION (METAL IN OIL). ENGINE WAS SENT TO ATI TO INVESTIGATE BOTH THE BEARING FAILURE AND THE OIL CONTAMINATION, TO REPLACE THE CT DISK & PT DISKS AND TO SDR DL76L030197Blade · dentedDURING T/O AT 110 KNTS BIRD INGESTION INTO NR 2 ENGINE WITH ENGINE SURGE DETECTED. ENGINE INDICATIONS NORMAL. REPORTED BY CREW 1 HR INTO FLT, NR 1 ENG GEN FAILED. A/C DIVERTED TO LGW. FOUND BIRD DEBRIS IN ENG 1, FAN BLADE DAMAGED OUT OF LIMITS. BOROSCOPE SDR XNOA01107Engine · stalledON ROTATION NR 2 ENGINE COMPRESSOR STALLED 3 TIMES. REDUCED POWER, ENGINE STABILIZED. FURTHER ADVANCEMENT OF NR 2 THROTTLE SHOWED ALL PARAMETERS NORMAL. PERFORMED VISUAL INSPECTION AND GROUND OPERATIONAL RUN. ALL ENGINE PARAMETERS WITHIN LIMITS. NO DEFECTSDR CA030226001Compressor · stalled(CAN) REJECTED TAKE OFF AFTER COMPRESSOR STALL ON THE LT ENGINE AND RISE IN TEMP AT 155 KNOTS, ALL 8 TIRES WENT FLAT (FUSES BLOWED OUT).SDR TBM700Blade · failedEXPERIENCED A TOTAL POWER FAILURE WHILE DESCENDING FROM FL250 TO FL240. PILOT MADE A SUCCESSFUL DEAD STICK LANDING. INSPECTION OF THE ENG REVEALED A CATASTROPHIC FAILURE OF A COMPRESSOR TURBINE BLADE WHICH RESULTED IN A COMPLETE ENGINE STOPPAGE AND LOCKING UPSDR 2003UALA00191Vane · brokenNR 2 ENGINE EXPERIENCED COMPRESSOR STALL. READINGS DROPPED AFTER A/C REACHED ALTITUDE. THE 7TH STAGE COMPRESSOR BLADE FAILED AT THE ROOT AND DAMAGED THE HPC, CAUSING THE ENGINE TO SURGE. T HE BLADE FAILURE WAS CAUSED BY THE VANE ARM ON THE 6TH STAGE VSV BEINGSDR GTIA030081Inlet Guide Vane · crackedMCO - FOUND LEFT NR 2 ENGINE 10 O'CLOCK POSITION FACING FRONT OF ENGINE CRACK ON IVG NEAR BASE APPROXIMATELY 2 INCHES IN LENGTH UNABLE TO STOP DRILL. REMOVED AND REPLACED THE NR 2 ENGINE IGV. (M)SDR USAABA03003Blade · damagedPHL - FLT 196 - DURING INITIAL CLIMB-OUT, CREW NOTED MODERATE VIBRATION FROM THE RIGHT ENGINE. CREW REDUCED THE THRUST TO IDLE. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOND A NINE BLADES DAMAGED BY FOD (ICE INGESTION). (M)SDR QXEA0300293Blade · brokenENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND FOUR BLADES BROKEN. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. ITSDR MALA030155Engine · stalledDURING TAKEOFF OF FLIGHT 2781, RT ENGINE COMPRESSION STALLS AT V1 ON TAKEOFF ROTATION. INFLIGHT SHUTDOWN ENGINE. AIR RETURN TO YQT. MAINTENANCE PERFOMRED COLD AND HOT SECTION BOROSCOPE, NO DAMAGE FOUND, LEAK CHECK OF A AXIS GOOD. PERFORMED GPA RUNS FOUND TSDR QXEA0300252Blade · brokenPDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE BROKEN OFF. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. NVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN CSDR QXEA0300251Blade · missingPDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE MISSING AND FOUR BLADES HAVE TRAILING EDGE DAMAGE. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BYSDR QXEA0300250Blade · missingPDX - NR1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND FOUR MISSING BLADES AND SIX BLADES HAVE TRAILING EDGE DAMAGE. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION SDR 2003F00213Compressor Wheel · out of balanceDURING CLIMB, OUT OF KDTW, THE LEFT ENGINE AMBER 'VIBRATION EXCEEDANCE' CAS MESSAGE WAS RECEIVED. POWER ON THE LT ENGINE WAS REDUCED, IAW THE AFM, AND THE MESSAGE EXTINGUISHED. THERE FORE, THE TRIP CONTINUED TO DESTINATION AND AACI MX PROVIDER AT KDTW WAS COSDR CA030213003Case · punctured(CAN) PIN SIZE HOLE LOCATED ON NR 2 PT6T-3 POWER SECTION GAS GENERATOR CASE AT APPROXIMATELY 7 O'CLOCK POSITION 3 3/4 INCHES AFT OF FIRST CIRCUMFIRENTIAL SEAM WELD (BY P3 AIR BOSS SUPPLYING AIR TO TORQUEMETER CLUTCH SEAL) WHILE PERFORMING VISUAL INSPECTION OF SDR QXEA0300246Blade · missingNR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND FOUR BLADES MISSING FROM HP TURBINE. REPLACED ENGINE. AIRCRAFT OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HSDR QXEA0300247Blade · missingNR 2 ENGINE FAILED SCHEDULED BORESCOPE. FOUND ONE BLADE MISSING FROM HP TURBINE. REPLACED ENGINE. AIRCRAFT OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER(GE) HAS BEEN COMPLESDR 2003FA0000150Compressor · fodHIGH PRESSURE COMPESSOR FOD.SDR QXEA0300245Blade · brokenNR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND THREE BROKEN BLADES, ANOTHER WITH MATERIAL MISSING AND SEVERAL OTHERS WITH SMALL NICKS IN TIPS. REPLACED ENGINE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION ATSDR QXEA0300244Blade · brokenNR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO BLADES BROKEN, ANOTHER WITH POSSIBLE CRACK. REPLACED ENGINE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE.SDR SWAA030321Manifold · rupturedAIR TURNBACK, DURING DEPARTURE NR 2 ENG OVERHEAT LIGHT ILLUMINATED. FOUND 13TH STAGE LT MANIFOLD RUPTURED. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR QXEA0300248Blade · missingNR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUSDR EGR2004F00000Compressor · crackedCOMPRESSOR PULLEY SHAFT CRACK AT WOODRUFF KEY.SDR QXEA0300230Blade · missingNR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO BLADES MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETESDR C1HA200394005Compressor · stalledDURING TAXI, ENGINE NR 2 EXPERIENCED A COMPRESSOR STALL/ PERFORMED COM 2.72.13. INSPECTED NR 2 ENGINE INLET & EXHAUST PER P&W MM 72-00-00 NO DEFECTS NOTED. OPERATED ENGINE TO 1.85 EPR. ALL PARAMETERS NORMAL.SDR HDNA084070Case · crackedONE 4TH STAGE COMPRESSOR STATOR VANE BROKE OFF SEVERELY DAMAGING THE 4TH & 5TH STAGE COMPRESSOR BLADES WITH SUBSEQUENT COMPRESSOR STALLING AND LOW ENGINE POWER.SDR QXEA0300217Blade · crackedPDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO HPT 1 BLADES BROKEN, TWO BLADES CRACKED AND SOME WITH COLLATERAL DAMAGE. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE.SDR QXEA0300132Blade · crackedPDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE. LP COMPRESSOR ROTOR 1 BLADE CRACKED. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE SENT TO PRATT AND WHITNEY FOR EVALUATION.SDR MALA030125Engine · stalledDURING FLIGHT, RT ENGINE COMPRSSOR STALLED & OVERTEMPED. AIR RETURN TO INL. CREW REPORTED, GOING THRU 500 FT WHILE DIALING DOWN CTOT, RT ENGINE SUFFERED COMPRESSOR STALL. DUE TO COMPRESSOR STALL, ENGINE TEMP EXCEEDED 970 DEGREES FOR 31 SECONDS BEFORE STALL SDR CA030205002Compressor · stalled(CAN) DURING FLIGHT YYZ/LHR, ACFT DIVERTED TO YUL, DUE TO LT. ENGINE COMPRESSOR STALL. ENGINE SHUT DOWN. RESTARTED BUT HIGH VIBRATION, AND RISING EGT. SO ENGINE SHUT DOWN AGAIN.ACFT REMOVED FROM SERVICE TO CARRY OUT BOROSCOPE AND INVESTIGATION.SDR HEEA084207Plenum · crackedPLENUM IS CRACKED.SDR SWAA030131Blade · crackedDURING POST FLIGHT, FOUND NR 2 ENG FAN BLADES NR 2 CRACKED AND NR 4 TIP CURLED. REMOVED AND REPLACED NR 2 ENG FAN BLADES NR 2, NR 4, NR 21 AND NR 23 PER MM.SDR SWAA030094Engine · leakingODOR IN CABIN DURING RT A/C PACK SYS IN USE. TERMINATED FLT AT TPA FOR INSPECTION OF NR 2 ENG AND FOUND OIL LEAK AT 6 O'CLOCK POSITION IN COMPRESSOR SECTION. REMOVED AND REPLACED NR 2 ENG PER MM.SDR HEEA083783Liner · crackedLINER CRACKED IN DOUBLE LIP AREA. REPLACED WITH SERVICEABLE PART.SDR HEEA083781Liner · crackedCRACKS AROUND THE INSIDE EDGE OF LINER AT END THAT MOUNTS TO SHIELD. REPLACED WITH SERVICEABLE PART.SDR HEEA083780Liner · damagedCOMPRESSOR LINER DELAYED STARTS. REPLACED WITH SERVICEABLE PART.SDR HEEA083773Engine · damagedENGINE HAS A HOLE IN LEFT HAND COMPRESSOR ARM PIT. REPLACED WITH SERVICEABLE ENGINE.
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