JASC 7313
Service difficulty reports · 530
Reports filed under 7313 · Fuel Injector 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 = '7313' 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 = '7313' 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 CA951116026"O" Ring Packing · leaking(CAN)IN CRUISE THE #1 ENGINE TORQUE DECREASED TO 67 PERCENT. DURING DESCENT, THE #1 ENGINE FIRE LIGHT ILLUMINATED. THE ENGINE WAS SECURED AND THE FIRE BOTTLE WAS DISCHARGED. AN UNEVENTFUL SINGLE ENGINE LAN DING WAS MADE AT DESTINATION. POST FLIGHT INSPECTION FSDR SIMA952951O-Ring · leakingDFW - FLT 3864 - IN CRUISE FLIGHT THE NR 2 ENGINE POWER DROPPED OFF TO 40 PERCENT AND STABILIZED. FEATHERED PROP AND CONTINUED TO DFW WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED FUEL LEAK FROM NR 12 FUEL NOZZLE TRANSFER TUBE O-RING. REPLACED ASDR CA951026018Packing · split(CAN)IN CRUISE THE NR 2 ENGINE TORQUE DECREASED TO 40 PERCENT. THE POWER LEVER WAS RETARDED AND THE EEC WAS RESET. THE ENG TORQUE DECREASED TO ZERO FOLLOWED BY AN ENG AUTOFEATHER, BUT THE ENG CONTINUED TO RUN. ON APP THE FIRE WARNING LIGHT ILLUMINATED AND ESDR 96ZZZX1494Nozzle Set · defectiveNOZZLE SET DEFECTIVE. SIL PW200-002. REMOVED DUE TO CARBON ACCUMULATION THAT COULD CAUSE ENGINE START DIFFICULTY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX1493Nozzle Set · defectiveNOZZLE SET DEFECTIVE. SIL PW200-002. REMOVED DUE TO CARBON ACCUMULATION THAT COULD CAUSE ENGINE START DIFFICULTY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX1492Nozzle Set · defectiveNOZZLE SET DEFECTIVE. SIL PW200-002. REMOVED DUE TO CARBON ACCUMULATION THAT COULD CAUSE ENGINE START DIFFICULTY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX1491Nozzle Set · defectiveHYBRID FUEL NOZZLE SET DEFECTIVE. SIL PW200-002. REMOVED DUE TO CARBON ACCUMULATION THAT COULD CAUSE ENGINE START DIFFICULTY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 95ZZZX6197Nozzle · defectivePILOT COMPLAINED OF POWER/N2 FLUCTUATING WITH COLLECTIVE INPUT. SUBSEQUENT INSPECTION REVEALED THE FUEL NOZZLE WAS AT FAULT. REMOVED AND REPLACED NOZZLE AND PROBLEM WAS CURED. NOZZLE SENT IN FOR REWORK.SDR SIMA952911O-Ring · failedFWA - FLT NR 4003 - EN ROUTE TO CMH, LEFT ENGINE TORQUE DROPPED 30 PERCENT THEN BEGAN TO DECLINE STEADILY. CREW ELECTED TO DIVERT TO FWA AND PROCEEDED WITH IN FLIGHT SHUTDOWN PROCEDURES WHEN TORQUE REACHED 30 PERCENT. UNEVENTFUL LANDING WAS MADE IN FWA. MAISDR CA951026017Fuel Tube · leaking(CAN)IN CRUISE THE #1 ENGINE PARAMETERS BEGAN TO DECREASE, AND THE PILOT DIVERTED THE AIRCRAFT TO AN ALTERNATE. THE ENGINE WAS SHUTDOWN ON APPROACH AND AN UNEVENTFUL LANDING WAS CARRIED OUT. POST FLIGHT IN SPECTION FOUND A FUEL TRANSFER TUBE LEAKING ON #5 FUELSDR 96ZZZX979Nozzle · defectiveFUEL NOZZLE 'ERRATIC SPRAY PATTERN'.SDR 95ZZZX6039Nozzle · defectiveRT ENGINE FLAMED OUT AT 42,000 FEET. DISASSEMBLED ENGINE, SENT FIRST STAGE NOZZLE OUT FOR RE-WORK, REASSEMBLED ENGINE. TEST FLIGHT OK.SDR 95ZZZX5254Shroud · misinstalledTHE LEFT ENGINE WAS VERY SLOW TO START. INVESTIGATION REVEALED THE FUEL NOZZLE SHROUD WAS INSTALLED 180 DEGREES FROM CORRECT POSITION WHICH BLOCKED FUEL FLOW THROUGH THE NOZZLE CAUSING SLOW STARTS. THE FUEL NOZZLES HAD BEEN REPLACED 291.1 HOURS PREVIOUSLY. SDR CA960212027Nozzle · carbon buildup(CAN)DURING FLIGHT, AT ABOUT 150' AGL, THE ENGINE FLAMED OUT AND THEN RELIT, HOWEVER THE ENGINE RPM ONLY REACH 30 PERCENT NG. THE PILOT CARRIED OUT AN AUTOROTATION. THE AIRCRAFT WAS FITTED WITH FLOAT GEAR.DURING THE FLARE AND RUN-ON LANDING, THE TAIL SKID CONTSDR 95ZZZM486Nozzle Gasket · leakingDEN - THE CREW ELECTED AN AIR TURNBACK WHEN THE LEFT ENGINE LOST POWER IN FLIGHT AND TORQUE DROPPED TO 1000 AT FULL POWER. MAINTENANCE FOUND SEVERAL FUEL NOZZLE GASKETS (MS937116) LEAKING. ALL FUEL NOZZLES AND GASKETS WERE CHANGED AND LEAKED CHECKED GOOD. ASDR SWIA95613Fuel Nozzle · failedLT ENGINE FAILURE AT ROTATION RETURNED FOR LANDING. FOUND O-RINGS FOR NR 10 FUEL NOZZLE SPLIT. INSTALLED NEW O-RINGS RAN ENGINE, FLAMED OUT, INSTALLED, SERVICED NR 10 NOZZLE AND NEW TUBE. RAN ENGINE AT 100 PECENT TORQUE FOR 5 MINUTES. OPS CKS GOOD, NO LEAKSDR 95ZZZX3747Nozzle · defectiveAIRCRAFT WOULD DROOP RPM WHEN THE COLLECTIVE WAS LIFTED. REPLACEMENT OF THE FUEL NOZZLE CORRECTED THE PROBLEM. FCU WAS CHANGED AS PRECAUTION.SDR HEEA955331Fuel Nozzle · defectiveENGINE HARD TO START. REQUIRED BATTERY CART ON 2 OR 3 STARTS. REPLACED WITH SERVICEABLE FUEL NOZZLE.SDR UF6A950607O-Ring · failedORD - FLT 5061 - NR 2 ENGINE TORQUE WOULD NOT MAKE POWER. ON APPROACH, ENGINE FLAMED OUT. MAINTENANCE REPLACED FUEL NOZZLE O-RING. OPS CHECK GOOD. (X)SDR 95ZZZX3047Washer Key · misinstalledRECEIVED FUEL NOZZLE SET FROM STOCK AND ONE KEY WASHER WAS FOUND TO BE IMPROPERLY INSTALLED. SET RETURNED TO OVERHAUL FACILITY REGIONAL AIRCRAFT SERVICES.SDR HEEA954942Nozzle · defectiveFUEL NOZZLE DEFECTIVE. EXCESSIVE DROOLING AND SPITTING. SERIAL NUMBERS REMOVED PKHC4238 & PANO0613 & PKHA8102.SDR HEEA954764Fuel Nozzle · defectiveAIRCRAFT WILL NOT START ABOVE 12% N1. REPLACED FUEL NOZZLE DUE TO IMPROPER SPRAY PATTERN.SDR RMXA9520533Nozzle Assy · crackedUPON INSPECTION OF ENGINE ASSEMBLY FOR CAUSE OF LOW POWER (-86%) THE G.P. NOZZLE WAS FOUND TO HAVE A LARGE CIRCUMFERENTIAL CRACK ON THE INNER SHROUD TO VANE ASSY. WELD (81/2" CRACK) CIRCUMFERENCE OF INNER SHROUD IS APPROXIMATELY 19". REPLACED NOZZLE.SDR 95ZZZX6943Nozzle Assy · defectiveENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. NOZZLE FOUND LEAKING PER SPECS.SDR 95ZZZX6942Nozzle Assy · defectiveENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. NOZZLE INSPECTED AND FOUND TO BE EJECTING A SOLID STREAM PER SPECS.SDR 95ZZZX6941Nozzle Assy · defectiveENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. FOUND PRIMARY SIDE OF NOZZLE PLUGGED, EXCEPT FOR SOLID THIN STREAM AT 40 DEGREE PATTERN POSITION, PER SPECS.SDR 95ZZZX6940Nozzle Assy · defectiveENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. FOUND PRIMARY SIDE OF NOZZLE PLUGGED, EXCEPT FOR SOLID THIN STREAM AT 40 DEGREE PATTERN POSITION, PER SPECS.SDR 95ZZZX6939Nozzle Assy · defectiveENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. NOZZLE FOUND TO BE SPLITTING PER SPECS.SDR 95ZZZX6938Nozzle Assy · not torquedENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. UNABLE TO TEST HIGH CROSS FLOW. HEAD NOT TORQUED PER SPECS.SDR 95ZZZZ160Fuel Pump · malfunctionedDEN - FLT NR 494 - ON APPROACH INTO DENVER, AT APPROX 12,000 MSL, THE LT ENGINE WOULD NOT SPOOL ABOVE IDLE. EPR 1.07, N1 20 PERCENT, N2 35 PERCENT, EGT 320 DEGREES, FUEL FLOW .5. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED ENG FUEL CON
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