JASC 7810
Service difficulty reports · 1,904
Reports filed under 7810 · Engine Collector/Tailpipe/Nozzle, 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 = '7810' 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 = '7810' 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 HEEA0016619Exhaust Stack · crackedEXHAUAST STACK CRACKED.SDR 2002FA0000788Flange · brokenPILOT EXPERIENCED LOW MP AT 22K. SLOWLY BLED DOWN AT CRUISE. PILOT SAID AT NORMAL 25 INCHES, IT BLED DOWN TO 22 INCHES WITH FUEL THROTTLE. UPON CHECK MECHANIC NOTED EX STAINS ON R/CYL BANK AND DISCOVERED FLANGE COMPLETELY SEPARATED AT TURBO FLANGE AREA EXHASDR 99ZZZX3035Stack · crackedCRACK NEXT TO WELD ON AFT SIDE.SDR 99ZZZX1266Ejector Duct · crackedEJECTOR DUCT CRACKED. REMOVED AND REPLACED.SDR HEEA0016491Ejector · damagedSEAL ON EJECTOR ASSY TORN AND SEVERAL MISSING RIVETS.SDR 99ZZZX3040Stack · crackedEXHAUST STACK CRACKED AT AFT CENTER WELD.SDR HEEA0016303Ejector · crackedEJECTOR HAS PROGRESSIVE CRACKS.SDR HEEA0016302Ejector · crackedEJECTOR HAS EXCESSIVE CRACKING.SDR 99ZZZX3032Stack · crackedCRACK ON AFT SIDE NEAR CENTER AT FLANGE BASE.SDR HEEA0016205Duct · crackedDUCT CRACKED.SDR AU981513Tailpipe · fire(AUS) NR 3 ENGINE TAILPIPE FIRE.SDR 99ZZZX658Nozzle · damagedPRE-FLIGHT INSPECTION FOUND 5.50 INCH BY 4 INCH PIECE OF EXHAUST NOZZLE MISSING FROM AFT END OF NOZZLE. EXHAUST DUCT WAS DAMAGED AS PART DEPARTED AIRCRAFT. BOTH PARTS REPLACED.SDR HEEA0016155Duct · crackedEXHAUST DUCT CRACKED.SDR 98ZZZX4593Header · mismanufacturedHWS RECEIVED FROM CUSTOMER A NEW TURBOCHARGER EXHAUST HEADER WYE WHICH WAS PURCHASED FROM A CESSNA DISTRIBUTOR RECENTLY FOR INSPECTION. THE CUSTOMER WAS CONCERNED ABOUT THEIR PART BECAUSE ATTEMPTING TO INSTALL CORRESPONDING PARTS IN THEIR RESPECTIVE POSITIONSSDR 98ZZZX4592Header · mismanufacturedHWS RECEIVED FROM CUSTOMER A NEW TURBOCHARGER EXHAUST HEADER WYE WHICH WAS PURCHASED FROM A CESSNA DISTRIBUTOR RECENTLY FOR INSPECTION. THE CUSTOMER WAS CONCERNED ABOUT THEIR PART BECAUSE ATTEMPTING TO INSTALL CORRESPONDING PARTS IN THEIR RESPECTIVE POSITIONSSDR AU981612Exhaust Stack · misinstalled(AUS) PILOT REPORTED UNUSUAL NOISE COMING FROM THE RT ENGINE AND SUSPECTED A STICKY VALVE. AFTER ENGINE RUNS, THE COWLS WERE REMOVED FROM THE RT ENGINE TO CARRY OUT A COMPRESSION CHECK. IT WAS THEN NOTICED THAT THE NR 3 EXHAUST STACK WAS NOT FITTED TO THE NRSDR 98ZZZX4265Exhaust Pipe · wornPART HAD EITHER WORN OR WAS IMPROPERLY REWORKED CAUSING THE FLAIR TO GO DEEPER INTO THE PIPE SECTION THAN WAS ORIGINALLY INTENDED. AS A RESULT, FORWARD SECTION SLID TOO FAR INTO THE FLAIR CAUSING THE EXHAUST PIPE SECITON FORWARD OF THIS TO SEPARATE.SDR 98ZZZX4801Exhaust Riser · crackedEXHAUST RISER FOUND CRACKED ON 25-HOUR INSPECTION. SUBMITTER SUSPECTED CAUSE TO BE EXHAUST SYSTEM TOO RIGID TO ALLOW FOR HEAT EXPANSION.SDR 98ZZZX4795Exhaust Riser · crackedEXHAUST RISER FOUND CRACKED ON NR 3 CYLINDER ON 50-HOUR OIL CHANGE. SUBMITTER SUSPECTS CAUSE TO BE EXHAUST SYSTEM TOO RIGID TO ALLOW FOR HEAT EXPANSION.SDR CA981007008Exhaust Stack · broken(CAN) COWLING REMOVED FOR STARTER CHANGE. INSPECTION FOUND THE EXHAUST STACK ON NR 2 CYLINDER BROKEN. THE OUTBOARD STUD AND THE HELICOIL WERE PULLED FROM THE CYLINDER. NUMBERS ON CYLINDERS AND ACCESSORIES DO NOT MATCH LOG BOOK NUMBERS.SDR 98ZZZX3652Exhaust Stack · crackedPILOT FOUND CRACKS DURING POST-FLIGHT INSPECTION. REMOVED AND REPLACED.SDR 98ZZZX3651Exhaust Stack · crackedPILOT FOUND CRACKS DURING POST-FLIGHT INSPECTION. REMOVED AND REPLACED EXHAUST STACK.SDR 98ZZZX3650Exhaust Stack · crackedPILOT INSPECTED EXHAUST AFTER FLIGHT AND FOUND IT TO BE CRACKED. REMOVED AND REPLACED.SDR 98ZZZX3649Exhaust Stack · crackedPILOT FOUND CRACKS DURING POST-FLIGHT INSPECTION. REMOVED AND REPLACED EXHAUST STACK.SDR 98ZZZX3648Exhaust Stack · crackedPILOT DISCOVERED CRACKS DURING POST-FLIGHT INSPECTION. REMOVED AND REPLACED EXHAUST STACK.SDR 98ZZZX3647Exhaust Stack · crackedPILOT FOUND CRACK AT WELD. REMOVED AND REPLACED.SDR CA980916065Gasket · failed(CAN) DURING INSPECTION, THE EXHAUST GASKETS WERE FOUND BURNED IN THE CENTER AREA. THE SUBMITTER REPORTS THAT PREVIOUSLY GASKETS WERE MADE FROM ASBESTOS MATERIAL, WHICH WAS NOT SUSCEPTIBLE TO BURNING.SDR AU981118Exhaust Stack · cracked(AUS) RIGHT ENGINE REAR EXHAUST SEGMENT CRACKED FOR 75 PERCENT OF THE CIRCUMFERENCE OF THE FLANGE. PART TC: 1,971.SDR HEEA0015867Ejector · crackedLEFT EJECTOR ASSEMBLY'S WELDS ARE CRACKED AND HAS LOOSE RIVETS.SDR HEEA0015801Exhaust Stack · crackedCRACKED ALONG WELD LINE ON SMALL RADIUS.SDR HEEA0015704Duct · crackedEXHAUST DUCT CRACKED.SDR HEEA0015703Exhaust Stack · crackedEXHAUST STACK CRACKED.SDR CA980908002Exhaust Pipe · broken(CAN) DURING PRACTICE LANDINGS, A LOUD ENGINE NOISE WAS HEARD, FOLLOWED BY A LOSS OF POWER, WHEN CLIMB POWER WAS APPLIED. AIRCRAFT RETURNED TO BASE. POST-FLIGHT INSPECTION FOUND THE NR 3 CYLINDER EXHAUST PIPE HAD BROKEN. THE PLASTIC COOLANT RESERVOIR HAD MESDR HEEA0015505Duct · crackedEXHAUST DUCT CRACKED CAUSED BY WORKING RIVETS ON BLOWER HOUSING.SDR 98ZZZX3935Exhaust Stack · crackedUPON PERFORMING OTHER MAINTENANCE, A CRACK WAS DISCOVERED IN THE EXHAUST STACK/RISER ASSY UNDER THE CLAMP POSITIONED APPROXIMATELY 12 INCHES FROM END OF EXHAUST. SUBMITTER SUSPECTS HEAT, VIBRATION, AND FATIGUE CAUSED ROLE IN PART FAILURE. SUGGEST AREA BE INSSDR 98ZZZX3420Clamp · looseEXHAUST CLAMP CAME LOOSE IN-FLIGHT ALLOWING EXHAUST STACK TO COME LOOSE FROM THE TURBOCHARGER EXIT PORT ON THE LEFT ENGINE. HOT EXHAUST GASSES BLISTERED THE PAINT ON THE AFT CENTER OF THE COWLING. ENGINE WAS SECURED/FEATHERED AND UNEVENTFUL LANDING ACCOMPLISSDR P5CA9801218Exhaust Sleeve · delaminatedNR 4 ENGINE EXHAUST SLEEVE INNER SKIN DELAMINATED AT 6 O'CLOCK POSITION. REMOVED AND REPLACED NR 4 ENG EXHAUST SLEEVE ASSY IAW MM 78-11-02.SDR P5CA9801211Exhaust Sleeve · crackedCRACKED NR 4 ENGINE EXHAUST SLEEVE AT 1:00 AND 6: POSITIONS. REPAIRED CRACK PER BOEING SRM 54-30-3.SDR HEEA0015486Ejector · crackedEJECTOR ASSY CRACKED.SDR HEEA0015485Ejector · crackedEJECTOR ASSEMBLY CRACKED.SDR HEEA0015445Ejector · crackedEJECTOR ASSEMBLY CRACKED AND BRACKET BROKEN.SDR HEEA0015342Duct · crackedFLANGE CRACKED ON DUCT ASSEMBLY.SDR HEEA0015306Ejector · crackedEJECTOR OUTER SHROUD CRACKED AND FLANGE CRACKED ON EJECTOR ASSEMBLY..SDR P5CA9801197Exhaust Sleeve · looseNR 3 ENGINE EXHAUST SLEEVE A 1 O'CLOCK POSITION LOOSE FASTENERS. REPAIRED PER SRM 51-30-02.SDR HEEA0015220Stack · crackedEXHAUST STACK CRACKED.SDR 98ZZZX2983Inlet · crackedAD 89-24-03 CALLED FOR 100-HOUR INPSECTION OF TURBOCHARGER. THIS AIRCRAFT HAS NEW P/N PART AND WAS CRACKED 2 INCHES AT THE Y-TURBO INLET.SDR 98ZZZX2680Muffler · crackedFOUND THE HEATER MUFFLER CRACKED AROUND THE FLANGE AREA ALONG THE WELD. THIS MAKES SECOND ONE SEEN WITH LESS THAN 200 HOURS TT. CRACK WAS APPROXIMATELY 6 INCHES. SUBMITTER STATED ONLY AFFECTS THE 172R MODELS.SDR CA980818017Collector · cracked(CAN) ENGINE OIL CONSUMPTION WAS 1 LITRE PER HOUR AND SMOKE WAS COMING FROM THE EXHAUST STACK. INSPECTION FOUND THE 1ST STAGE NOZZLE AND EXHAUST COLLECTOR TO BE CRACKED BEYOND LIMITS. PART TC: 925.SDR P5CA9801135Rivets · shearedNR 3 ENGINE EXHAUST PLUG MOUNT BRACKET SHEARED RIVETS. REPLACED SHEARED RIVETS PER SRM 51-30-02.SDR 98ZZZX2618Shield · looseTHE EXHAUST SHIELD HAD COME LOOSE ON BOTH LT AND RT ENGINES. BOTH SHIELDS HAD CAUSED ENOUGH DAMAGE TO WARRANT REMOVAL OF BOTH ENGINE MOUNTS FOR REPAIR.
Back to JASC 7810