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 20010125CW001Compressor · failedJUST AFTER T/O COPILOT REPORTED SPARKS COMING FROM RIGHT ENGINE, INBOARD AND OUTBOARD EXHAUST STACKS. POWER WAS REDUCED AND AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. INSPECTION THROUGH HIGH AND LOW BLEED VALVE OPENINGS REVEALED MASSIVE COMPRESSOR FAILURSDR MALA000746Engine · stalledDURING INITIAL CLIMBOUT NR 1 ENGINE INDICATED ENGINE VIBRATION OF 1.5 MOMENTARY INDICATION, AT ABOUT 12,000 WE HAD TWO OCCURANCES OF COMPRESSOR STALL AND ENGINE QUIT. DURING DESCENT N1 READ 12 PERCENT, N2 0 PERCENT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENSDR 2001F00086Bolt · looseRECEIVED A PRELIMINARY ENGINE CONDITION REPORT CONCERNING A ENGINE THAT WAS GOING THROUGH A HOT SECTION INSPECTION. IT WAS NOTED IN THE REPORT, THE 4, 5, AND 6 COMPRESSOR TIE ROD BOLTS WERE LOOSE. THERE WAS DAMAGE NOTED TO THE DIFFUSER PIPES, CT SHROUD SEGMESDR AU001261Case · cracked(AUS) NR 2 ENGINE LOWER COMPRESSOR CASE HALF HAD DEBONDING OF THEPLASTIC BAND SECTION BETWEEN NR 3 AND NR 4 STAGES. EXCESSIVE SPOOL RUB EVIDENT ON THE PLASTIC SECTIONS CAUSING EXCESSIVE CRACKING. CIRCUMFERENTIAL CRACKING WAS FOUND ACROSS THE ENTIRE SECTION OF SDR DL72S002252Compressor · stalledCOMPRESSOR STALL ON T/O ROLL NR 2 ENG. ABORT AT 30 KTS RETURN TO GATE. INSP INLET AND EXAUST. RAN ENG PER PFHB. ALL CK NORMAL, 13 KNT CROSS WIND GUSTING TO 19 KNTS.SDR DL76S002234Engine · fodNR 1 ENGINE SUSTAINED DAMAGE TO 7 FANS BLADES DURING TAKEOFF FROM PBI. DEPARTMENT OF AIRPORTS FOUND 2 PARTIAL REMAINS OF TURKEY VULTURES NEAR END OF RUNWAY. ENGINE WAS NOT SHUT DOWN IN FLIGHT. ENGINE WILL REQUIRE REPLACEMENT BEFORE FURTHER FLIGHT.SDR CA001110039Blade · damaged(CAN) AFTER TAKEOFF OUT OF MANCHESTER NH (MHT) GOT N1 VIB ICON. FOLLOWED BY SMOKE IN CABIN. CREW SHUT DOWN THE ENGINE AND RETURNED TO BLOCKS. PRELIMINARY REPORT OF EXTENSIVE FAN BLADE DAMAGE. ROAD CREW BEING ARRANGED TO GO TO MHT FOR POSSIBLE ENGINE CHANGE. AVSDR C2XAOOIA404Engine · fodEFD-DURING POST FLIGHT INSPECTION, CREW REPORTED THAT THE NUMBER ONE ENGINE HAD FOD DAMAGE. MX REMOVED/REPLACED THE AFFECTED ENGINE, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.SDR CA001110034Compressor · damaged(CAN) CREW REPORTED NR 1 ENGINE VIBRATION AFTER TAKEOFF FOLLOWED BY AN UNCOMMANDED ENGINE STOPPAGE. MAINTENANCE REPORTED THAT A BORESCOPE INSPECTION REVEALED EXTENSIVE COMPRESSOR DAMAGE. 2000-11-14TC:SDR CA001206011Blade · broken(CAN) DURING DISASSEMBLY OF ENGINE TO COMPLY WITH GEARBOX INSPECTION AND HOT SECTION INSPECTION METAL FRAGMENTS WHERE FOUND IN THE COMBUSTOR,. INSPECTION OF THE COMPRESSOR REVEALED 3 BROKEN BLADES ON NR 2 IMPELLER S/N 2-03501-353 CAUSING MAJOR DAMAGE DOWN STRSDR CA001107009Compressor · damaged(CAN) CREW REPORTED NR 1 ENGINE VIBRATION AFTER TAKEOFF FOLLOWED BY UNCOMMANDED ENGINE STOPPAGE.BOROSCOPE INSPECTION REVEALED EXTENSIVE COMPRESSOR DAMAGE.SDR 2000UALA00634Compressor · stalledCOMPRESSOR STALL ON NR 1 ENGINE AT CLIMBOUT. *S/D* BORESCOPED 6TH AND 7TH STAGES. NO LIMITING CONDITIONS FOUND.SDR CA001107002Blade · damaged(CAN) DURING CRUISE NR 3 ENGINE VIBRATION INCREASED TO 5.0 UNITS AND FELT INSIDE THE AIRCRAFT. NR 3 ENGINE SHUT DOWN AS PER EMERGENCY PROCEDURES.FAN BLADES SUSPECTED.SDR R7MR33075Seal · leakingLEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR R7MR33074Seal · leakingLEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR CA001027002Compressor Wheel · fod(CAN) ON APPROACH, FOUR MILES OUT, INTO REGINA, SASK, THE CREW NOTICED A SUDDEN POWER SURGE ON THE RIGHT HAND ENGINE. THE RIGHT ENGINE WAS SURGING FROM 83% TO 65% CONTINUOUSLY WITH A TEMPERATURE FLUCTUATION. THE CREW REDUCED POWER AND CONTINUED THE APPROACH, LSDR R8RR010147Gas Generator · cokedAFTER LANDING AND SHUT DOWN, THE MECHANIC CHECKED THE COMPRESSOR FOR FREEDOM OF ROTATION. THE COMPRESSOR WAS SEIZED. SUSPECT FUEL INJECTION WHEEL COKING. (X)SDR SWAA002028Blade · damagedAIR TURNBACK, DURING ROTATION RECEIVED NUMEROUS BIRD STRIKES TO AIRCRAFT. ON RETURN TO ALB, NR 1 ENG VIBRATION GAUGE READ 3.0, APPROACHED 4.0 AT FL 240,THRUST LEVER REDUCED TO KEEP VIBRATION LEVEL TO BELOW 4.0. SMELL IN CABIN. PERFORMED BIRD STRIKE INSP PERSDR TWAA0015606Compressor · fodCREW ABORTED TAKEOFF AT 65 KTS DUE TO RT ENGINE STALL WITH VIBRATION ON RT FUEL CONTROL LEVER. ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO THE GATE. COMPRESSOR HAD FAILED WITH ENGINE CASE PENETRATION, INCLUDING ONE INSTANCE OF UNCONTAINED FAILURE AT 12 O''CLSDR 20010123CW004Bearing · failedRT ENGINE FAILURE IN FLIGHT. ENGINE FAILED DUE TO NR1 BEARING FAILURE.SDR 20010112SG028Engine · deterioratedFLT 2570 - BIL - LEFT ENGINE TORQUE DROPPED 15 PERCENT DURING TAEOFF ROLL. MAINTENANCE VERIFIED LOW TORQUE DURING ENGINE RUNS. HOT SECTION DETERIORATION IS SUSPECTED. HSI HAD 3184.7 HOURS, DUE IN 415.3. ENGINE WAS CHANGED. (M)SDR 20001019SH029Case · crackedDURING PROPELLER CHANGE ON LEFT ENGINE, A SERIES OF CRACKS WERE FOUND ON THE INBOARD EXHAUST FLANGE. THE FLANGE IS A PART OF THE POWER SECTION, SO FIELD REPAIR WAS NOT POSSIBLE. THE AFFECTED POWER SECTION WAS REPLACED WITH A SERVICEABLE POWER SECTION. A POSSDR 20001024SH004Seal · crackedSEAL EXHIBTS TWO SHORT CRACKS, 0.150 INCH LENGTH EACH, IN THE FORWARD ARM OUTSIDE DIAMETER AT THE STAGE 1 BLADE INTERFACE. THIS PART HAD ACCUMULATED 954 CSN. (X)SDR DL72S001878Compressor · stalledAFTER T/O, THE NR 3 ENGINE COMPRESSOR STALLED FOLLOWED BY AN ELECTRICAL SMELL IN CABIN. INSPECTED AND RAN ENGINE, NO TROUBLE FOUND.SDR CA001016008Stator · cracked(CAN) DURING A SCHEDULED C-2 FAN CHANGE ON WING THE 2ND STAGE STATOR WAS FOUND COMPLETELY CRACKED THROUGH A ONE BLADE LOCATION, INBOARD OF THE MID SPAN SHROUD. THE ENGINE ASSEMBLY WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR EISA20000151Catcher · stalledCOMPRESSOR STALL NR 2 ENGINE AIR TURNBACK TO (AUS). DRAINED MOISTURE TRAP IAW 73-33. RAN ENGINE, OPS CHECK GOOD PER M/M 71-00.SDR CA001030002Compressor · failed(CAN) SHORTLY AFTER TAKEOFF, THE CABIN FILLED WITH FUMES AND LIGHT SMOKE. THE AIRCRAFT RETURNED TO THE POINT OF DEPARTURE. ENGINE WAS SPLIT AT THE C-FLANGE. NO OBVIOUS DAMAGE OR ABNORMALITIES WERE FOUND. A NEW NR 2 BEARING COVER AND GASKET WERE INSTALLED.SDR CA001020009Drum · cracked(CAN) INTERMEDIATE PRESSURE COMPRESSOR ROTOR DRUM P/N UL16758 S/N 36651 EX ESN 30534 & MODULE 02 DM3560 WAS SNAGGED AT INIT INSP DURING OVERHAUL OF THIS MODULE AT RRC DUE TO CRACKING FOUND IN D OVE TAIL OF BLADE SLOTS OF STAGE 6 & STAGE 3. CRACKS CAN BE DETECTSDR SCNA00099Compressor · stalledDURING TAKEOFF ROLL, ENGINE NUMBER TWO COMPRESSOR STALL DURING THE TAKEOFF ROLL AT LAS (10 KNT) CROSS WIND. SLIGHT EPR FLUCUATION, SLIGHT NOISE, AIRFRAME PULSATED, SOFT STALL. INSPECTED INLET AND EXAUST NR 2 ENGINE, NO DEFECTS NOTED ALL PARAMETERS CHECK NORMSDR AU000651Seal · leaking(AUS) ENGINE NR 1 BEARING SEAL LEAKING.SDR CA000905017Fan Blade · bird strike(CAN) ON ROTATION AT TAKEOFF CREW REPORTED THEY HEARD A BANG & FELT THE AIRCRAFT YAW TO THE RIGHT. THE CREWFLEW AROUND TO REDUCE THE FUEL LOAD AND RETURNED TO THE STATION (YEG). A BIRD STRIKE INSPECTION WAS CARRIED OUT AND SLIGHT DAMAGE WAS FOUND ON THE C1 FANSDR 20001215SH011Seal · leakingNR 1 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR 2000UALA00508Compressor · stalledNR 2 ENGINE COMPRESSOR STALL. *S/D* NR 2 ENGINE WAS REPLACED.SDR R7MR33010Bearing · damagedEXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR R7MR32996Seal · warpedEXCESSIVE WARPAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR CA001019024Engine · surges(CAN) AT FLT390, 25NM FROM DOWNWIND OF A THUNDERSTORM, IN LIGHT CLOUD, LEFT HAND ENGINE EXPERIENCED A SURGE, CHECK LIST CARRIED OUT, THROTTLE RETURNED TO CRUISE POWER AND EXPERIENCED A SECOND SURGE. DESCENT TO FL350, ALL PARAMETERS NORMAL. CREW ELECTED TO DIVESDR CA000919016Fan Blade · damaged(CAN) - FAN BLADES (33) REPLACED (REF: DEFECT NR 00492). - A/C RETURNED TO SERVICE.SDR 20000830SH001Disk · crackedC/W NDT INSPECTION AND FOUND FORWARD RIM CRACKED IN 7 EACH PLACES AND 1 EACH DOVE TAIL CRACKED. (X)SDR CA020103016Coupling · cracked(CAN) CIRCUMFERENCE CRACKS ON PILOT O.D AREA. DISCREPANCY FOUND DURING COMPRESSOR REPAIR. DUE TO CUSTOMER REPORT METAL CONTAMINATION.SDR AU000751Bearing · failed(AUS) NR 1 BEARING FAULTY. N1 ROTOR SEIZED.SDR 20000810SH004Gear Shaft · failedTHE ENGINE SUFFERED A FAILURE OF THE COMPRESSOR BEARING ROTATING GROUP MAINSHAFT, AND HIGH SPEED PINION ASSEMBLY. (X)SDR 2000UALA00472Blade · fracturedEN ROUTE NRT-BKK, FLIGHT REPORTED NR 1 ENGINE COMPRESSOR STALL WITH MAXIMUM EGT OF 714. ENGINE WAS SHUT DOWN. AIRCRAFT DIVERTED TO TPE. *S/D* HIGH PRESSURE TURBINE FIRST STAGE BLADE FRACTURED IN THE AIRFOIL JUST ABOVE THE PLATFORM. FRACTURE WAS CAUSED BYSDR 2000UALA00462Blade · bird strikeABORTED TAKEOFF AT 120 KNOTS DUE TO A BIRD STRIKE IN THE NR 2 ENGINE. *S/D* REPLACED FAN BLADES.SDR 20010111SG010Blade · failedDURING LANDING ROLL-OUT, DURING REPOSITION, CREW NOTICED ENGINE VIBRATION. SHUT DOWN ENGINE DURING TAXI. TEAR DOWN DETERMINED 1ST STAGE LPT BLADE FAILURE. (M)SDR SWIA971906Fan Blade · dirtyRIGHT ENGINE N1 VIBRATION 2.7 MLS AT 89 PECENT AT FL 180. RETURNED TO SLC. REMOVED AND CLEANED RIGHT ENGINE FAN BLADES. OPS CHECKS GOOD.SDR CA000810013Block · worn(CAN) ECAM NR 1 ENGINE STALL WARNING DURING ENGINE SPOOL UP FOR TAKE-OFF ROLL, ABORTED TAKEOFF AND RETURNED TO GATE.CENTRALIZING BOLT HEADS AT THE NR 3, 5 & 6 POSITION VGV/IGV FOUND HARD RUBBING INTO THE RUBBING BLOCKS THAT GROVED AND OCCASIONALLY JAMMED THE VSDR TWAA0012003Fan Blade · fodTHE RT ENGINE HAD STRONG COMPRESSOR STALLS AFTER TAKEOFF. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO STL. FOUND FOREIGN OBJECT DAMAGE TO THE FAN CASE AND FAN BLADES. THE FOREIGN OBJECT WAS NOT IDENTIFIED. REPLACED TWO SETS OF BLADES, (P/N A03779-4SDR 20001017SH046Blade · separatedENGINE FAILED JUST AFTER TAKEOFF DUE TO BLADE SEPARATION ON CT DISC. ENGINE TEAR DOWN PERFORMED AT A CERTIFIED REPAIR STATION. (X)SDR SWAA001390Compressor · contaminatedBURNED OIL ODOR NOTICED DURING TAKEOFF, CLIMB AND DESCENT. REMOVED AND REPLACED BOTH ACM''''S C/W NR 1 ENG BORESCOPE INSP AND FOUND EVIDENCE OF OIL RESIDUE AT COMPRESSOR SECTION BLADES. REMOVED AND REPLACED NR 1 ENG PER MM.SDR ZIAA00006Stator Vane · damagedYIP - NR 3 ENGINE FIRE WARNING ILLUMINATED ON CLIMB-OUT. SHUT DOWN ENGINE. REMOVED AND REPLACED SWIRL STAIGHTNER IAW L-188 MM 71-1-0. OPS CHECK GOOD ON ENGINE RUN. (M)
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