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 UIEA2011053000268Sleeve · damagedDURING WALK AROUND CHECK, MX FOUND A HOLE 0.5" WIDE ON THE OUTER SLEEVE OF THE LONG FIXED CORE EXHAUST NOZZLE (LFCEN) ON THE NR 2 ENGINE. THE HOLE IS 6.0" FROM THE EXHAUST SLEEVE T/E AT THE 11:00 O' CLOCK POSITION. (DISPOSITION WAS MADE TO REMOVE ANY BURRS USDR S9BA20110004Doubler · corrodedRT EXHAUST TRAIL DOUBLER CORRODED WS 131 AND WS 90.6 IS THE CENTER OF THE CORROSION. REPAIRED IAW EO-CFBBW-5-31-11, SRM 57-30, AND RD-57-213.SDR UIEA2011050900256Sleeve · crackedDURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 9 O'CLOCK POSITION ON THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 3" LONG AND IS APPROX .5" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF TSDR A6WA201140286Skin · chafedINNER SKIN ON LT TAIL PIPE FAIRING CHAFED IN 2 AREAS MARKED. REPAIRED CHAFED AREAS ON LT TAIL PIPE IAW CMM 78-11-00 AND REO 601R-78-10-1173.SDR UIEA2011040400239Sleeve · crackedDURING MX WALKAROUND, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR 2 ENG. THE CIRCUMFERENTIAL CRACK IS APPROX 15" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. SRM 54-41-30 THE LENGTH OF THE CRACKSDR JR2R2011031800095Support Bracket · crackedDURING INSTALL 2EA NUT PLATE SUPPORT BRACKETS CRACKED ON LT EXHAUST NOZZLE. REMOVED AND REPLACED NUT PLATE BRACKETS IAW SHORTS CMM 20-42-06.SDR A6WA201140224Fairing · chafedLT JETPIPE FAIRING CHAFED FROM PYLON. REPAIRED LT JETPIPE IAW REO 601R-78-11-3960.SDR QMLA2011030711032Panel · delaminatedTHE MECHANIC INSPECTED AND FOUND SOME DELAMINATION ON THE LT REAR ENGINE COWLING PANEL AFT OF THE EXHAUST OUTLET IN EXCESS OF THE LIMITS SPECIFIED IN THE AEC SRM 51-10-11, 2-1, PARA 3. THE MECHANIC HAS SENT THE COWLING TO OUR REPAIR STATION FOR THEIR EVALUASDR CA111222011Diffuser · used(CAN) UPON LANDING AND PERFORMING A POST FLIGHT VISUAL INSPECTION THE AME FOUND THE BOTTOM STRUT ON THE EXHAUST DIFFUSER CRACKED WITH A SECTION OF MATERIAL MISSING. THE EXHAUST DIFFUSER SERVES AS THE REAR BEARING SUPPORT. AS A RESULT OF THIS DEFECT THE POWERSDR UIEA2011030600144Sleeve · crackedDURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR 2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 8" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OFSDR CA110314018Exhaust Pipe · cracked(CAN) EXHAUST PIPE WELD CRACKED AT HEAT EXCHANGER NR 4 CYLINDER.SDR 2011F00055Exhaust Pipe · separatedDURING CRUISE AT 4000' THE PILOT EXPERIENCED A PARTIAL DROP IN MP ON THE RIGHT ENGINE. A DIVERSION TO KPBI WAS PERFORMED AND THE AIRCRAFT LANDED WITHOUT FURTHER INDECENT. A POST FLIGHT VISUAL INSPECTION REVEALED THAT THE LEFT REAR EXHAUST PIPE HAD SEPARATED FRSDR P4YA2011022400001Case · crackedON POST FLIGHT INSPECTION FOUND THE NR 1 ENGINE POWER TURBINE EXHAUST CASING CRACKED BEYOND LIMITS. ENGINE SN 285-063RC IN PROCESS OF BEING REMOVED AND REPLACED.SDR A6WA201140096Bracket · crackedRT EXHAUST FAIRING HAS BROKEN FIRE LOOP ATTACHMENT BRACKET. R & R 2 EA FIRE LOOP ATTACHMENT BRACKETS IAW SRM 51-42-06 AND SRM 51-40-11.SDR A6WA201140084Fairing · chafedLT ENGINE EXHAUST NOZZLE FAIRING HAS CHAFE AT INBD SIDE WHERE PYLON FAIRING RUBS. REPAIRED CHAFED DAMAGED AREA AT INBD SIDE LT ENG EXHAUST NOZZLE FAIRING IAW REO 601R-78-11-3958.SDR 2011FA0000091Exhaust Duct · crackedTHE RT EXHAUST SYS DEVELOPED GUSSET CRACKS AROUND 250 HRS TT. THE MFG SAID THE CRACKS WERE "NON SAFETY CONCERNS" AND DID NOT ADDRESS THEM AT THE TIME. AT 432 HRS TT THE EXHAUST CRACKED IN 2 DIFFERENT WELD JOINTS ON THE COLLECTORS LEADING FROM 2 CYLINDERS. RSDR CA110112008Exhaust Riser · crackedEXHAUST RISER NR 1 FOUND CRACKED AT CYLINDER FLANGE DURING INSPECTION. PART REPLACED.SDR CA110114005Exhaust Duct · failedACFT MADE EMERGENCY/UNSCHEDULED DESCENT FOLLOWING LOSS OF MANIFOLD PRESSURE AND LOSS OF CABIN HEAT. THE RT TRANSITION FAILED AND SEPARATED AT THE TURBOCHARGER FLANGE. THE ENTIRE PART IS REGARDED AS FAILED. HAD THE PILOT NOT MADE THE DESCENT, IT IS POSSIBLE THASDR UIEA2010121900195Sleeve · crackedDURING MX WALKAROUND OF N408MC MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 16" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LSDR CA110114004Duct · crackedPART WAS SENT IN WITH CRACK 85 PERCENT AROUND THE BODY. CRACK ORIGINATES FROM BALANCE TUBE ATTACHMENT TAB. SPOKE WITH MECHANIC BEFORE HE REMOVED THE PART AND HAD HIM CHECK FOR THIS ORIGIN OF THE CRACK. HAD ADVISED HIM OF SB10-1 AND HAD HIM REVIEW IT PRIOR TO SDR UIEA2010121700193Sleeve · crackedDURING MX WALKAROUND OF N517MC, MX FOUND 1 EA CRACK ON THE NR2 ENGINE EXHAUST NOZZLE OUTER SLEEVE, LOCATED AT APPROX 7 O'CLOCK POSITION. THE CIRCUMFERENTIAL CRACK IS APPROX 2.5 IN LONG. IAW AMM 78-11-01 THE LENGTH OF THE CRACK IS OUT OF LIMITS. (DISPOSITION SDR UIEA2010121600194Sleeve · crackedDURING MX WALKAROUND, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 12" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF THE SDR UIEA2010110900176Sleeve · crackedDURING MX WALKAROUND OF MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, APPROX THE 2 O'CLOCK POSITION ON THE NR2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 2.25" LONG AND IS NEAR THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS WITHIN LSDR UIEA2010110700174Sleeve · crackedDURING MX WALKAROUND OF MX FOUND 3EA CRACKS ON THE EXHAUST NOZZLE OUTER SLEEVE, THE FIRST CRACK STARTING AT APPROX THE 12 O'CLOCK POSITION AND ENDING AT THE 2 O'CLOCK POSITION ON THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 19" LONG AND IS APPROX 13" FSDR CA101105005Nozzle · damaged(CAN) THE END OF JET TUBE NOZZLE CONTACTED THE M/R BLADE DURING GROUND RUN WITH THE ENGINE COWL OPEN IN THE FIRST/LOWEST POSITION. KIT NR 0617-71-03 INSTALLED IAW SB 0617-71-00 .03 0 TO REPLACE ECL SAND FILTER. WITH THE COWLING OPEN, IN THE FIRST POSITION, TSDR 2010FA0001152Baffle · chafedTHE FRONT 2 PRODUCTS CENTER AND LT BAFFLES WERE FOUND CHAFED THROUGH THE INNER NOSE BOWL AND CAUSED A HOLE APPROX 7 INCHES LONG AND .2500 INCH WIDE. THE BAFFLES ENDED UP TOO LONG OVER TIME AS THE ENGINE MOUNTS STARTED TO SAG. HAVE HEARD OF SEVERAL OTHER REPOSDR 2010FA0001151Baffle · chafedTHE FRONT 2 PRODUCTS CENTER AND LT BAFFLES WERE FOUND CHAFED THROUGH THE INNER NOSE BOWL AND CAUSED A HOLE APPROX 7 INCHES LONG AND .2500 INCH WIDE. THE BAFFLES ENDED UP TOO LONG OVER TIME AS THE ENGINE MOUNTS STARTED TO SAG.SDR UALA2010101303812Cone · crackedNR 1 ENGINE EXHAUST CONE HAS A CRACK A T 9 O'CLOCK. CRACK LOCATED IN ZONE 1 AND IS 7.5 INCHES IN LENGTH. ACP EVA 80212 STOP DRILLED HOLE. CRACK CAN BE WELD REPAIRED IAW SM USING AMS5837 FILLER.SDR WWQA147HH1007102Exhaust Pipe · crackedDURING A 100/300/600 HOUR INSP FOUND THE LT TAIL PIPE EXHAUST FAIRING TO HAVE A CRACK IN THE BOTTOM SIDE OF THE FAIRING. FOUND THAT THIS WAS CAUSED FROM AN ADEL CLAMP IN THE WRONG POSITION. REPOSITIONED THE CLAMP AND REPAIRED THE CRACK IAW REPAIR EXHAUST FAIRISDR CA110125030Support · cracked(CAN) MUFFLER SHROUD SUPPORT CRACKED AWAY FROM MUFFLER.SDR A6WA201040753Bracket · crackedRT ENG JETPIPE NUTPLATE BRACKET PN 228-50181-833 UNDER PANEL 446BL IS CRACKED. REMOVED CRACKED BRACKET ASSY PN 228-50181-833. LOCATE AND INSTALLED NEW SERVICEABLE BRACKET ASSY PN 228-550181-833 UNDER PANEL 446BL, R JET PIPE.SDR UIEA2010092700166Sleeve · crackedDURING MX WALK AROUND, MX FOUND 2 EA CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, NR1 STARTING AT APPROX THE 7 O'CLOCK POSITION. THE CIRCUMFERENTIAL CRACK IS APPROX 3.0 IN LONG, THE NR2 CRACK IS LOCATED AT INBD SIDE AND AFT OF EXHAUST CONE AREA MEASURING 0.750 ISDR UIEA201000230Nozzle · crackedEO 4478A138: DURING MX WALKAROUND, MX FOUND 1EA CRACK ON THE NR2 ENGINE EXHAUST NOZZLE OUTER SLEEVE, AT APPROX THE 9 O'CLOCK POSITION. THE CIRCUMFERENTIAL CRACK IS APPROX 4.5 IN LONG. IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. DISPOSITION IS TOSDR MTNA0820100001Exhaust Duct · crackedTHE FIRE WARNING LIGHT CAME ON. THE LIGHT WENT OUT AFTER POWER WAS PULLED BACK, AFTER LANDING IN GND WITH OUT INCIDENT. THE MAINTENANCE PEOPLE FOUND A CRACKED EXHAUST DUCT. AFTER THE DUCT WAS REPLACED THE SYSTEM CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TOSDR EE4Y100355Exhaust Duct · corrodedDURING INSP ENGINE NR2 EXHAUST DUCT WITH SPOT CORROSION AT L/E SKIN.SDR A6WA201040727Shield · gougedLT ENGINE JET PIPE FAIRING (436AL) FIRE LOOP SHIELD IS GOUGED. R & R IAW CMM 78-11-00.SDR A6WA201040622Shield · gougedRT ENGINE JET PIPE FAIRING FIRE LOOP SHIELD IS COUGED. R & R IAW SRM 51-42-02.SDR 2010F00187Exhaust Stack · crackedDURING 50 HR INSP, MECHANIC DISCOVERED 360 DEGREE CRACK AROUND NR 1 EXHAUST STACK FLANGE.SDR UIEA2010082200142Nozzle · crackedDURING MX WALK AROUND, MX FOUND (1EA) CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 11 O'CLOCK POSITION. THE CIRCUMFERENTIAL CRACK IS APPROX 35.0 IN. LONG. IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. DISPOSITION IS TO STOP DRSDR 2011FA0000101Header · crackedTHE NR 3 EXHAUST HEADER WAS SENT FOR REPAIR 7/1610 BECAUSE IT WAS CRACKED.SDR V0XR201007150001Shroud · cracked(V0XR) LT EXHAUST SHROUD HAS A CRACK IN THE INBD/AFT FASTENER BRACKET. R & R LT EXHAUST SHROUD.SDR NSVA2010110Shroud · defectiveDURING TAKEOFF ROLL AT I90 KIAS RT TAILPIPE HOT MASTER WARNING ILLUMINATED. TAKEOFF ABORTED WITHOUT SIGNIFICANT BRAKING. REMOVED AND REPLACED EXHAUST PIPE SHROUD IAW AMM 72-10-00, OPS CHECKED GOOD.SDR HDNA201006212010Clamp · looseAT TAKEOFF, THE NR1 ENGINE FIRE LIGHT ILLUMINATED. THE ACFT RETURNED TO LANDING ZONE WITHOUT INCIDENT. UPON INSP, IT WAS FOUND THAT THE NR 1 ENGINE INBD EXHAUST STACK HAD COME LOOSE FROM THE TURBINE EXHAUST COLLECTOR AND HAD WEDGED ITSELF INTO THE ENGINE COWLISDR UALA2010062102158Fairing · missingACCOUSTIC INSULATION MISSING 7 O'CLOCK LT ENGINE EXHAUST. MISSING PIECE IS THE L/E OF THE ACOUSTIC PANEL FAIRING. SPEED TAPE IS BEING USED TO COVER CAVITY. THRUST REVERSER INOPERATIVE DUE TO TAPE REPAIR OF ACOUSTICAL LINER. REMOVED PANEL STARTED PICKING UP SDR A6WA201040570Bracket · crackedLT JET PIPE PANEL 436BL NUTPLATE BRACKET IS CRACKED IN HALF XN 221.0. R & R BRACKET IAW SRM 51-42-06, 51-40-11.SDR A6WA201040571Bracket · crackedLT JET PIPE PANEL 436BR NUT PLATE BRACKET IS CRACKED IN HALF XN 221.0. R & R BRACKET IAW SRM 51-42-06, 51-40-11.SDR CA100521007Bolt · brokenT-BOLT ON THE EXHAUST CLAMP BROKE ALLOWING THE CLAMP TO COME FREE, THE ALLOWING THE EXHAUST DUCT TO SEPARATE, LEADING TO THE ENGINE TO BE SHUTDOWN.SDR P5CA2010051701637Sleeve · crackedNUMBER 2 ENGINE EXHAUST SLEEVE CRACKED. ACCOMPLISHED TIME LIMITED REPAIR PER ENGINEERING ORDER 4478A129 WITH FAA 8110-3 DATED 17 MAY 2010. RE-INSPECT EVERY 3 FLIGHT CYCLES WITH A PERMANENT REPAIR WITHIN 50 CYCLES.SDR A6WA201040490Bracket · crackedLT ENGINE JET PIPE PANEL, 436BR, BUTTPLATE BRACKET CRACKED. REMOVED DAMAGED NUTPLATE BRACKET PN 228-50181-883 AND INSTALL NEW SERVICEABLE N/P 228-50181-883.SDR A6WA201040345Bracket · crackedLT ENGINE JETPIPE PANEL 436BL NUTPLATE BRACKET CRACKED. REMOVED DAMAGED N/P BRACKET PN 228-50181-833 AND INSTALLED SERVICEABLE PN 228-50181-833.
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