JASC 7810
Service difficulty reports · 1,900
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 CALA2013103092515Cone · crackedNR 2 ENG EXHAUST CONE HAS 4.5" CRACK IN ZONE 1 AT 4 O'CLOCK POSITION. STOP DRILLED CRACK IAW AMM 78-11-12-200-011-C.SDR A6WA201310214326Heat Shield · crackedRT JET PIPE HEAT SHIELD CRACKED BETWEEN SECOND AND THIRD STIFFENERS. REPAIRED IAW CMM 78-11-00.SDR A6WA201310214285Fairing · crackedLEFT JETPIPE FAIRING EXTERIOR CRACKED BY LOWER ACCESS PANEL. REPAIRED CRACKED SKIN ADJACENT TO LOWER ACCESS PANEL IAW CMM 78-11-00, REPAIR SRS 062.SDR A6WA201310184284Fairing · crackedRT ENGINE TAIL PIPE FAIRING IS CRACKED AT DRAIN LINE MOUNT. PERFORMED FILLER & DOUBLER REPAIR IAW STS EA 15-20-13-441.SDR A6WA201310144257Tailpipe · crackedRIGHT ENGINE TAIL PIPE FROM FWD STIFFENER IS CRACKED AT INBD 4 O`CLOCK. REPAIRED RT ENGINE TAIL PIPE STIFFENER IAW CMM 78-11-00.SDR CA131008007Panel · missing(CAN) DURING GROUND HANDLING THE RAMP CREW NOTICED A PANEL MISSING FROM THE LT ENGINE TAILCONE. IT IS NOT KNOWN WHEN OR WHERE THE PANEL DEPARTED THE ACFT HOWEVER THE DAMAGE INDICATES THAT IT DEPARTED IN FLIGHT. THE ENGINE TAILCONE ASSY WAS REPLACED. PANEL, PSDR CA131003005Nozzle · separated(CAN) DURING THE CLIMB, THE CREW HAD A LT ENGINE EMERGENCY FIRE WARNING AFTER ROTATION. THEY FOLLOWED EMERGENCY PROCEDURES AND AFTER SECURING THE ENGINE AND FIRING THE FIRST BOTTLE, THE FIRE WARNING WAS EXTINGUISHED. THEY DECLARED AN EMERGENCY AND LANDED WISDR AC2A9NA09252013Grommet · failedNEW STYLE EXHAUST SYS FAILURE AT ATTACHMENT POINTS WHERE RUBBER GROMMETS INSULATOR CONNECT TAIL PIPE. AFTER GROMMETS FAIL, THE MOVEMENT AND EXHAUST VIBRATION LEAD TO EXCESSIVE FIREWALL CRACKING.SDR A6WA2013100200230Seal · tornLT JET PIPE FAIRING UPPER LOWER SEALS ARE TORN. R & R UPPER & LOWER SEALS IAW CMM 78-11-00, SRS 070.SDR 2013FA0000672Adapter · crackedMECHANIC WAS PERFORMING MX ON THE AIRFRAME AND NOTICED EXHAUST STAINING ON THE OUTSIDE OF THE COWLING. ON OPENING THE COWLING THE MECHANIC DISCOVERED THE EXHAUST HAS BEEN PRESSURIZED AT EVERY ANNUAL SINCE INSTALLATION. THE CRACK WAS NOT EVIDENT AT THE LAST ASDR CA130912002Tailpipe · cracked(CAN) FOUND RT TOP TURBOCHARGER TAIL PIPE CRACKED.SDR A6WA2013100200231Seal · tornRT JET PIPE FAIRING L/E SEAL UPPER AND LOWER ARE TORN. REMOVED AND INSTALLED NEW UPPER & LOWER SEALS IAW CMM 78-11-00, SRS 070.SDR CA130905006Cable · broken(CAN) DURING 150 HR INSPECTION, EXHAUST RETENTION CABLE FOUND BROKEN. 78.8 HRS TTSN.SDR A6WA201309044158Fairing · gougedLT JET PIPE FAIRING HAS GOUGE PUNCTURE HOLE ON L/E STIFFENER. REMOVED DAMAGED STIFFENER AND INSTALLED NEW, IAW CMM 20-23-00,20-42-06, 20-40-11, 20-42-20.SDR A6WA201309034157Shield · crackedRT ENGINE JET PIPE FIRE DETECTOR LOOP SHIELD IS CRACKED. REPLACED WITH SERVICEABLE FIRE DETECTOR LOOP SHIELD.SDR A6WA201309034156Bracket · crackedRT ENGINE JET PIPE FIRE LOOP SHIELD FWD SUPPORT MOUNT BRACKET IS CRACKED. REPLACED WITH NEW SERVICEABLE BRACKET.SDR M2LA201309160001Clamp · brokenPILOT HAD DEPARTED AND SHORTLY AFTER TAKEOFF EXPERIENCED SMOKE IN THE CABIN. LANDED. INSTALLED NEW EXHAUST TAILPIPE ASSEMBLY V-BAND CLAMP.SDR M2LA2013F00169Clamp · brokenSHORTLY AFTER TAKEOFF, EXPERIENCED SMOKE IN THE CABIN. LANDED. INSTALLED NEW EXHAUST TAILPIPE ASSEMBLY V-BAND CLAMP, WHICH HAD BROKEN.SDR CALA2013081690496Exhaust Duct · damagedENG 1 HAS 2 MISSING RIVETS ON UPPER OTBD TAILCONE.SDR CA130819011Nozzle · loose(CAN) IT WAS REPORTED THAT THE NR 1 ENGINE HAD A FIRE WARNING AND THE PILOT SHUTDOWN AND SECURED THE ENGINE, AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. THE ON GROUND TROUBLESHOOTING FOUND A LOOSE/DETACHED EXHAUST NOZZLE CLAMP.SDR CA130814003Collector · cracked(CAN) DURING CLIMB OUT AFTER TAKEOFF, THE PILOT HEARD A LOUDER THAN NORMAL ENGINE NOISE. ALL ENGINE PARAMETERS WERE NORMAL, SO THE PILOT FLEW TO THE MAINTENANCE FACILITY. UPON FURTHER INSPECTION, THE RT EXHAUST COLLECTOR WAS FOUND TO BE CRACKED AT THE ELBOW.SDR FDEA201308081810Nozzle · gougedEXHAUST NOZZLE OUTER SKIN GOUGED APPROXIMATELY 8.5 INCHES LONG VERTICALLY. REPAIRED IAW EA6-7810-167489.SDR A6WA2013081641136Frame · crackedRIGHT JETPIPE FAIRING NR 1 FRAME CRACKED AT 3:00 POSITION AT TOOLING HOLE. REPAIRED IAW CMM 78-11-00, REPAIR SRS 043.SDR A6WA2013073141115Seal · gougedRT JET PIPE FAIRING UPPER SEAL WORN AND STIFFENER GOUGED WITH HOLE PUNCTURE. R & R SEAL AND STIFFENER IAW CMM 78-11-00, SRS 0910,78-11-00, SRS 070, 20-40-11, 20-42-06, 20-23-00, 20-25-06.SDR JJBA20130718015Shroud · crackedNR 2 EXHAUST OUTLET SHROUD, HAS CRACKING ON OTBD SKIN SECTION. REMOVED FINGERNAIL FOR REPAIR IAW AMM 54-78-11. REINSTALLED EXHAUST OUTLET IAW AMM 54-78-11.SDR 2013FA0000418Exhaust Header · damagedNR 1 EXHAUST HEADER SUPPORT BOLT CHAFING INTO NR 1 HEADER.SDR 2013FA0000417Exhaust Header · damagedNR 1 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED. BOLT CHAFED AND REPLACED.SDR CA130717004Exhaust Duct · cracked(CAN) DURING A 200HR INSPECTION, EXHAUST STAINING WAS NOTICED ON THE LT FORWARD CYLINDER. THE L/H FORWARD EXHAUST STACK WAS FOUND TO HAVE ONE OF THE MOUNTING FLANGES CRACKED OFF WHERE IT IS WELDED TO THE EXHAUST STACK. THE EXHAUST STACK WAS REPLACED AND THE AISDR A6WA2013073141116Stiffener · crackedRT JETPIPE 1ST STIFFENER CRACKED AT 9 O`CLOCK POSITION. REPAIRED IAW AMM 78-11-00, REPAIR SRS 042.SDR A6WA201307241089Fairing · crackedRIGHT EXHAUST NOZZLE FAIRING IS CRACKED BY PANEL 446BR. REPAIRED EXHAUST NOZZLE FAIRING IAW REO 601R-78-11-4006, REV C.SDR UALA2013071104824Tailpipe · fireON ARRIVAL, NR 2 ENGINE SHUTDOWN, GROUND REPORTED FIRE BURNING IN TAILPIPE LASTING 2-3 MINUTES. NO EXTINGUISHING AGENTS WERE USED ON ENGINE. REPAIRED TAIL PIPE OIL.SDR 2013FA0000400Exhaust Header · damagedNR 1 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED AND WORN INTO HEADER. BOLT CHAFED AND REPLACED.SDR 2013FA0000399Exhaust Header · damagedNR 1 AND NR 6 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED AND WORN INTO HEADER. BOLTS CHAFED AND REPLACED.SDR 2013FA0000398Exhaust Header · chafedNR 1 HOLE ENLONGATED AND BOLT CHAFED. NR 6 HEADER SUPPORT BRACKET COMPLETELY BROKEN OUT, BOLT CHAFED.SDR 2013FA0000397Support Bracket · damagedNR 1 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED AND WORN INTO HEADER. BOLT CHAFED AND REPLACED.SDR UALA2013070304662Exhaust Duct · crackedNR 1 ENGINE EXHAUST TAILCONE HAS A CRACK APPROX 6 INCHES LONG AT THE 3 O'CLOCK POSITION FWD EDGE. FOUND A CRACK AT 9:00 POS THAT IS "Y" SHAPED WITH LEGS MEASURING 3.5 X 3.5X 2.5 INCHES FOR A TOTAL OF COMBINED LENGTH OF 9.5 INCHES. FOUND CRACK AT 3:00 POS AT SDR UALA2013070104566Tail Cone · crackedCRACK IN LT ENGINE EXHAUST TAILCONE. 5 O'CLOCK POSITION. NEXT TO PREVIOUS WELD. PERFORMED INSP OF LT ENGINE TAILCONE IAW MM. CRACK LOCATED IN ZONE 1 STOP DRILLED IAW MM. AC OK TO CONTINUE.SDR J4HC2013F00112Exhaust Stack · burnedEXHAUST SEGMENTS BURNED THROUGH, CONTRIBUTING TO HIGHER THAN NORMAL INTAKE AIR TEMP RESULTING IN REDUCTION OF POWER DETECTED AT RUN UP.SDR UALA2013062604442Cone · crackedCRACK IN TAIL CONE OF LEFT ENGINE. REPLACED THE NR 1 ENGINE EXHAUST CONE IAW AMM.SDR 2013FA0000354Transition Duct · puncturedHOLE FOUND IN THE RIGHT TURBO TRANSITION.SDR 2013FA0000353Slip Joint · leakingEXHAUST LEAK AT THE SLIP JOINT BETWEEN THE RT TURBO TRANSITION ON NR 1 CYLINDER EXHAUST RISER IGNITED NEARBY WIRING CAUSING AN ENGINE FIRE. FIRE WAS ON THE GROUND AND DISCOVERED AFTER SHUTDOWN.SDR REXA2013061601001Exhaust Pipe · chafedNR 2 EXAUST NOZZLE INBD OUTER SKIN CHAFED. REPAIRED NR 2 EXHAUST NOZZLE INBD OUTER SKIN IAW REO 690-71-13-008.SDR CA130611003Exhaust Duct · failed(CAN) ENGINE WAS SENT FOR A SCHEDULED O/H. DURING RECEIVING AND DISASSEMBLY OF THE ENGINE IT WAS NOTICED THAT THE EXHAUST DUCT HAD SUFFERED A MAJOR FAILURE OF THE INNER SECTION.SDR CA130607004Exhaust Pipe · cracked(CAN) DURING TAXI, EXCESSIVE MOVEMENT WAS NOTED ON THE LT JET PIPE ASSY. MAINTENANCE INSPECTED AND FOUND A CIRCUMFERENTIAL CRACK TOWARDS THE FORWARD END OF THE JET PIPE ASSY. JET PIPE REPLACED WITH SERVICEABLE UNIT.SDR CA130606007Exhaust Duct · cracked(CAN) EXHAUST DUCT INNER SECTION CRACKED, THREAD AT TURBINE EXIT, AT BEARING NR 3, THIS CAUSE THE TO DAMAGE THE T/E OF TURBINE BLADE.SDR CA130605011Exhaust Duct · cracked(CAN) WHILE PERFORMING AN ANNUAL INSPECTION, THE RT EXHAUST COLLECTOR, PN 0750238-47AWL, TSN:96.7 HRS, WAS FOUND CRACKED. THE EXHAUST COLLECTOR WAS REPLACED WITH A NEW COLLECTOR, PN 0750238-47AWL TO RECTIFY THE DEFECT.SDR A6WA201306181018Fairing · crackedRIGHT TAIL PIPE FAIRING HAS TWO SMALL CRACKS FROM THE 4TH DRAIN HOLE FROM AFT. REMOVED 2 SMALL CRACKS BY INCREASING SIZE OF DRAIN HOLE BY 0.040, NO EO WAS AFFECTED.SDR JJBA20130515001Shroud · crackedA CRACK WAS FOUND IN THE NR 1 EXHAUST FINGERNAIL PANEL 419CT. THE SHROUD WAS REPAIRED IAW A REPAIR DWG.SDR CA130531009Riser · cracked(CAN) FOUND RISER CRACKED WERE IT ENTERS MUFFLER, 3" CRACK.SDR UALA2013050803234Tail Cone · crackedNR 1 ENGINE TAIL CONE HAS AN ELEVEN INCH CRACK REPORTED BY RAMP. REPLACED TAIL CONE PER AMM.
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