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 ZI3R2015013000001Fuel Nozzle · burnedRECEIVED AN ENGINE SET OF GENX NOZZLES. UPON RECEIVING INSPECTION IT WAS NOTED THAT THE NOZZLE HAD BURN OUT ON THE SUPPORT.SDR ASAA2015012510419Fuel Nozzle · malfunctionedFOUND "ECONOMIC" FAULT-UPPER EGT SECTORS READING HIGH NR 73-31372, NR 2 ENGINE. FOUND ON T/C 78273000. ACFT GROUNDED. REPLACED NR 2 ENGINE FUEL NOZZLES IAW POWER PL-73 CMPT-07267-2, NOZZLES 1-6 AND 16-20.SDR ASAA2015010910208Fuel Nozzle · malfunctionedFOUND FAULT NR 73-31372, NR 2 ENGINE ECONOMIC UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. PERFORMED NR 2 ENGINE TOP 11 FUEL NOZZLE REPLACEMENT IAW EA PWR PL-73 CMPT-07267-2.SDR QMLA2014121114137Fuel Nozzle · malfunctionedDURING STARTUP, THE ACFT WAS BROUGHT TO IDLE IN PREPARATION FOR DEPARTURE. THE MEDICAL CREW SAW SMOKE EXITING THE EXHAUST. THE PILOT TURNED TO LOOK AT THE AFT END OF ACFT & LOOKED BACK AT GAUGES TO NOTICE THAT THE ENG INSTRUMENTS HAD AGREED WITH HIS VISUAL CSDR CA141121005Elbow · corroded(CAN) FOUND RUST AND DEBRIS FROM SERVO TO FUEL PRESSURE GAUGE. ALL FITTINGS FROM COCKPIT TO SERVO WERE BADLY CORRODED AND FULL OF DEBRIS DUE TO RUST. ALL FITTINGS AND LINES HAD TO BE REPLACED.SDR UE5R2014110700001Fuel Nozzle · crackedCRACK IN THREADED PORTION OF FUEL NOZZLE BODY FOUND AFTER LEAK TEST FAILURE AFTER NOZZLE INSTALLATION INTO FUEL NOZZLE ADAPTER ASSEMBLY. CRACK IN THREADS IS ONLY VISIBLE BY USING A 5X MAGNIFICATION.SDR ZI3R2014111300001Fuel Nozzle · burned outRECEIVED AN ENGINE SET OF NOZZLES. ON RECEIVING INSPECTION IT WAS NOTED THAT TWO NOZZLES HAD BURNED OUT ON THE SUPPORT.SDR ASAA2014102009444Fuel Nozzle · faultedFOUND FAULT CODE 73-31372 ECONOMIC FAULT-UPPER EGT SECTOR READING HIGH ON NR 2 ENGINE. ACFT GROUNDED, ACCOMPLISHED FIM 73-11 T801, INITIAL EVALUATION. DURING ENGINE RUN, FOUND PROBE T49.5 S1 WITH DOUBLE THE TEMPERATURE OF T 49.5 S4. R & R T49.5 S1 PROBE. SDR 2014FA0000627Injector · cloggedIN CONJUNCTION WITH LT & RT FUEL INJECTOR MANIFOLDS, ARE CAUSING EXCESSIVE EXHAUST FUMES IN THE COCKPIT. PART TIME ONLY REACHED 215.6 HOURS BEFORE BECOMING CLOGGED INTERNALLY CAUSING THE EXCESSIVE EXHAUST FUMES. PREVIOUS ISSUES HAVE ALSO NOT REACHED ITS 400SDR CA141010015Injector · fod(CAN) DURING TAKE-OFF ROLL THE LT ENGINE FAILED TO DEVELOPE FULL POWER AT FULL THROTTLE SETTING. THE TAKE-OFF WAS REJECTED AND THE AIRCRAFT SNAGGED. UPON INSPECTION, SMALL UNKNOWN FOREIGN DEBRIS WAS FOUND IN CYLINDERS 1,3 & 5 FUEL INJECTOR NOZZLES. FUEL CONTROSDR EPUA201408232014Injector · dirtyENGINE LOST POWER ON TAKEOFF. MADE A POPPING LIKE SOUND & SURGED, RECOVERED & THEN REPEATED. ACFT LANDED SAFELY. SUMPED WING TANKS, HEADER TANKS & FUEL STRAINER. THE ENG FUEL INJECTORS WERE CLEANED & THE ENTIRE SYS WAS SUMPED AGAIN. POST MAINT FLIGHT CHECSDR L2QR201406250001Fuel Nozzle · unsecureDURING HOT SECTION INSPECTION IT WAS DISCOVERED THAT FOUR FUEL NOZZLE ASSEMBLY KEY WASHERS NOT PROPERLY BENT TO SECURE NOZZLE. TABS WERE BENT OVER THE FUEL NOZZLE ADAPTER INSTEAD OF THE FUEL NOZZLE ASSEMBLY.SDR CA140701002Fuel Nozzle · contaminated(CAN) THE PILOT REPORTED A HUNG START WHERE THE ENGINE WOULD NOT ACCELERATED TO IDLE. THIS HAD AN EFFECT ON OPERATIONS, SUSPECTED FLIGHT CANCELLATION. TROUBLESHOOTING FOUND METALLIC DEBRIS IN THE FUEL NOZZLE LINES. COMPLETE FUEL SYSTEM IS BEING REPLACED.SDR CHIR2014040400236Nozzle · misoverhauledT3 NOZZLE WAS RECEIVED OVERHAULED, INSTALLED IN ENGINE AND RAN IN TEST CELL. DURING TEST CELL A COAST DOWN NOISE WAS NOTED. DURING DISASSEMBLY, PIECES OF THE NOZZLE FELL OUT, FURTHER INSPECTION FOUND THAT THE LAB SEAL RIVETS IMPACTED THE NR 3 WHEEL AND GROUNSDR IU5R2014032800001Fuel Nozzle · crackedDURING INVESTIGATION ON FUEL NOZZLES IAW CMM 73-13-41. ENGINEERING REVIEW PRIOR REPAIR CONDITIONS OF CIRCUMFERENTIAL CRACKS, CC ON THE OUTER AIR SWIRLER, OAS, SIDE OF EB WELD JOINT TO THE END CAP BAFFLE, ECB, IT WAS APPARENT BY OAS ADJACENT MATERIAL CONDITIONSDR CA140314017Fuel Nozzle · malfunctioned(CAN) ENGINE VERY SLOW TO ACCELERATE THROUGH 40-50 PERCENT N1 DURING START PROCEDURE. ENGINE START SYS TROUBLESHOT AND FOUND FUEL NOZZLE TO BE CAUSE OF ISSUE. NOZZLE REMOVED AND RETURNED TO REPAIR FACILITY FOR REPAIR.SDR 2014FA0000144Injector · dirtyPILOT REPORTED ROUGH RUNNING ENGINE AND MADE PRECAUTIONARY LANDING. PILOT WAS ABLE TO INFORM MAINTENANCE OF THE CYLINDERS THAT WERE HAVING ISSUES FROM THE ENGINE MONITOR INDICATION. MAINTENANCE FOUND SMALL AMOUNTS OF DIRT IN THE INJECTORS OF THE AFFECTED CYLSDR CALA2013121893770Fuel Nozzle · defectiveDUE TO ENG IGNITER R2 SLOW LIGHT OFF, REPLACE SIX EACH FUEL INJECTOR NOZZLES ON RT SIDE OF ENG 7 - 12. REPLACED NR 2 ENG FUEL NOZZLES 10 - 12, NOZZLES 7 - 9. REPLACED IAW SEQUENCE # 9546008.SDR CA131218003Fuel Nozzle · dirty(CAN) THE OPERATOR REPORTED A FLAME OUT DURING ROUTINE TAXI FOR TAKEOFF. THE ACFT RETURNED TO HANGAR AND THE MAINTENANCE CREW WAS ABLE TO REPLICATE THE EVENT DURING GROUND RUNS. WHEN REDUCING POWER FROM APPROXIMATELY 70 PERCENT DOWN TO IDLE. A BORESCOPE INSPSDR CA131120010Servo · malfunctioned(CAN) RT ENGINE WOULD NOT PRODUCE MORE THAN 2000 RPM DURING RUN-UP. FUEL INJECTION SERVO REPLACED.SDR CA131007009Nozzle · malfunctioned(CAN) THE PILOT WAS ON TAKEOFF ROLL AT ABOUT 88 KNOTS WHEN HE WITNESSED A PUFF OF SMOKE FROM THE EXHAUST STACKS, THE PMU STATUS LIGHT ILLUMINATED, AND THE ENGINE TEMPERATURE INCREASED WHILE COMPRESSOR SPEED AND TORQUE DECREASED BEFORE THE THROTTLE WAS PULLED BSDR 2013FA0000494Nozzle · brokenPILOT NOTED A +5 DEGREE ON POWER CHECK AND AT TIMES DID NOT FEEL THAT THE ENGINE WAS PRODUCING FULL POWER. UPON REMOVING THE ENGINE INLET COWLING A 1.7500" PIECE OF TUBING WITH A 90 DEGREE BEND WAS FOUND INSIDE THE INLET SCREEN AREA ON THE SCREEN FLOOR. THESDR REXA2013081601469Fuel Nozzle · leakingF/A REPORT A STRONG ODOR IN CABIN. ODOR BEGAN WHEN PACKS STARTED. STRONG "OILY" ODOR. ODOR IMPROVED AFTER A TIME, BUT REMAINED IN THE CABIN. ODOR SEEMED STRONGER IN SOME AREAS. PRIMARILY AROUND ROWS 5 AND 6. WHEN PACKS WERE OFF, ODOR WENT AWAY. FOUND LEAKSDR CA130724001Packing · cracked(CAN) ON 100 HR INSPECTION FUEL STAINING WAS NOTICED BETWEEN NR 4 AND NR 5 FUEL NOZZLE. UPON FURTHER INSPECTION THE PACKING ON THE FUEL TRANSFER TUBE WAS FOUND CRACKED ON INNER DIAMETER. PACKAGING OF THE PACKING`S STATED THEY HAVE AN UNLIMITED SHELF LIFE.SDR CA130711002Fuel Nozzle · failed(CAN) AIRCRAFT WAS HANGING AT 50 PERCENT N1 AT START. FUEL NOZZLE REPLACED.SDR CA130513005Fuel Nozzle · leaking(CAN) DURING TURN AROUND INSPECTIONS THE MECHANIC NOTED FUEL LEAKING FROM THE NR 1 ENGINE COWLING. INSPECTION REVEALED A LEAK FROM THE 1 FUEL NOZZLE, APPROXIMATELY 15 HOURS POST NOZZLE CHANGE. THE MECHANIC ATTEMPTED TO RE-TORQUED THE FITTING AND THEN SWAP THESDR UALA2013040502277Nozzle · faultedNR 1 ENGINE FUEL NOZZLES DISPLAYED 'ENG IGNITOR L1' SLOW LIGHT OFF. REPLACED FUEL NOZZLES FROM STEP 4C TO END. OPS AND LEAK CHECKED GOOD IAW AMM 71-00-00 -800-801-N00 TESTS 3 AND 6.SDR CKE2013F00001Bushing · looseFUEL INJECTOR BUSHINGS DID NOT STAY IN PLACE WHEN FUEL INJECTORS WERE REMOVED. INJECTORS WERE REMOVED FOR CLEANING. THIS ENGINE HAS 11TSMOH AND 4 OUT OF THE 6 BUSHINGS LOOSENED WITH THE INJECTOR. PROBABLE CAUSE IS THAT THE LOCTITE 620 DOES NOT HOLD THE BUSHSDR CKE2013F00000Bushing · looseFUEL INJECTOR BUSHINGS DID NOT STAY IN PLACE WHEN FUEL INJECTORS WERE REMOVED. INJECTORS WERE REMOVED FOR CLEANING. THIS ENGINE HAS 185 TSMOH AND 5 OUT OF THE 6 BUSHINGS LOOSENED WITH THE INJECTOR. PROBABLE CAUSE IS THAT THE LOCTITE 620 DOES NOT HOLD THE BUSDR IVLA20130109001Injector · brokenON 01/01/2013 DURING TAKEOFF PILOT NOTICED ENGINE RUNNING ROUGH, RETURNED TO AIRPORT FOR LANDING. (NO EMERGENCY DECLARED) ON 01/02/2013 A MECHANIC INSPECTED THE AIRCRAFT AND SUSPECTED FOULED SPARK PLUGS, AFTER CLEANING SPARK PLUGS THE MECHANIC TEST RAN THE AISDR UALA2012122407380Injector · dryRAN ENGINE FOR FUEL DISTRIBUTION VALVE OPS CHECK. NEED TO REMOVE INGITOR PLUG TO VERIFY NR 13 FUEL INJECTOR VALVE IS DRY BY BOROSCOPING. REMOVED IGNITOR PLUG FOR BORO. INSPECTOR VERIFIED THAT FUEL INJECTOR WAS DRY NR 13 INJECTOR.SDR CA130116005Fuel Nozzle · malfunctioned(CAN) FOLLOWING AN ENGINE CHANGE, THE CREW PERFORMED A FLIGHT TO PERFORM CUTOFF AND RELIGHT TEST. THE ENGINE DID NOT RELIGHT AFTER 2 ATTEMPTS. A SINGLE ENGINE UNEVENTFUL LANDING WAS PERFORMED. THE ENGINE DID NOT RELIGHT DURING THE ON GROUND INVESTIGATION. TSDR TRBA20121216001Fuel Nozzle · leakingAFTER PARKING, THE GROUND CREW INFORMED THE CREW OF A LOT OF FUEL LEAKING FROM THE BOTTOM OF NR 2 ENGINE. FUEL WAS LEAKING WITH ENGINE RUNNING AT IDLE AND PUDDLE OF FUEL PRESENT UNDER ENGINE. THE ACFT WAS REMOVED FROM SERVICE. R & R FUEL NOZZLE NR 1 & NR 2 OSDR CA121126002Ejector · leaking(CAN) WITH A PARKED ACFT, AFTER ENGINE SHUTDOWN, FUEL WAS NOTED LEAKING FROM THE NACELLE. OPENING THE COWLINGS REVEALED A LEAK AT THE FUEL EJECTOR TANK, PRE SB 26285. THE TANK WILL BE REPLACED BEFORE THE ACFT IS RETURNED TO SERVICE.SDR 2012FA0000820Injector · failedAFTER INSTALLATION OF FACTORY REBUILT ENGINE. PERFORMED GROUND RUN OF ACFT, AT ALL SETTINGS THE ENGINE RAN TOO RICH, AND ADJUSTMENTS HAD NO EFFECT. ACFT WAS NOT AIRWORTHY. REMOVED FUEL SERVO FROM ENGINE, SENT OUT FOR REPAIR. REINSTALLED FUEL SERVO AFTER RESDR CA120926003Fuel Nozzle · leaking(CAN) CREW REPORTED WHILE CLIMBING THROUGH 3000 FT, THE TORQUE OF NR 2 ENGINE DROPPED TO ZERO WITH ILLUMINATION OF OIL PRESSURE CAUTION SHORTLY THEREAFTER. ENGINE WAS SHUTDOWN IAW QRH AND DIVERTED TO NEAREST AIRPORT. ACFT LANDED SAFELY WITHOUT INCIDENT. ROOTSDR BSYA2012038Injector · pluggedJUST AFTER TAKEOFF FROM YIP, PILOT NOTICED POWER ON RIGHT ENGINE TO BE LOW AND WITH LOW READINGS ON THE EGT GAUGE. PILOT RETURNED AND LANDED SAFELY AT YIP WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NR 2 AND NR 6 FUEL INJECTORS PLUGGED, MAINTENANCE CLESDR UALA2012072303957Filter · warning lightRT ENGINE FUEL FILTER, RETURNED TO FIELD, REPLACED FUEL PUMP FILTER PER MM. RAN ENGINE, LEAK CHECKED GOOD AND NO FILTER MESSAGE.SDR CA120723007Fuel Nozzle · failed(CAN) AT ARRIVAL, UPON SHUTTING DOWN ENG NR 2, THE GROUND CREW SAW FIRE AT ENGINE 2 AND REPORTED TO THE PILOT. THE PILOT SAW ALSO NACELLE OVERHEAT ALERT, FOLLOWED BY ENG NR 2 FIRE WARNING. SUBSEQUENTLY PILOT DISCHARGED FIRE BOTTLE NR 1 FOLLOWED 30 SECONDS LASDR 2012FA0000435Fuel Nozzle · contaminatedFINDING UPPER DECK LINE RUSTING INTERNALLY ON TORNADO ALLEY TURBO EQUIPPED ACFT. THE RUST CONSISTS OF BOTH LARGE AND SMALL PARTICLES THAT ARE EASILY DISLODGED. ACFT THAT HAVE THIS CONDITION EXHIBIT RUST STAINS ON AND AROUND THE FUEL INJECTORS FOUND WHEN THE ISDR CA120907007Nozzle · failed(CAN) PLEASE BE INFORMED THAT B429 IS EXPERIENCING NR 1 ENGINE STARTING PROBLEM, FOLLOWING WAS REPORTED BY CUSTOMER: BOTH NR 1 AND NR 2 FUEL FILTER CAUTION LIGHT WERE ON, FUEL FILTERS WERE REPLACED, NO REPORT OF DEBRIS IN THE FILTERS. AFTER FUEL FILTERS REPLSDR MTNA0502201200001Nut · missingIN FLIGHT FROM FLL TO MTH THE PILOT SMELLED A STRONG FUEL SMELL IN THE COCKPIT. THE PILOT MADE AN UNEVENTFUL LANDING IN MTH. THE PILOT REPORTED THAT 2 EA NUTS WERE MISSING FROM THE FUEL NOZZLE RETAINER, ON ONE OF THE FUEL NOZZLES ON THE LEFT SIDE OF THE ENGISDR CA120503003Fuel Nozzle · leaking(CAN) ACFT RETURNED AFTER T/O WITH LLT ENGINE INDICATING LT ENGINE EGT AND CHT TEMPERATURES AT RED LINE LIMITS. MAINTENANCE FOUND NR 5 CYLINDER FUEL INJECTOR LINE AND NOZZLE THREADS STRIPPED AND SLIGHTLY LEAKING. ALL OTHER CYLINDER FUEL INJECTOR NOZZLES FOUSDR UIEA2012042500163Seal · brokenNR 5 FUEL NOZZLE SEAL BROKEN. NR 2 ENG OTBD FUEL RAIL NR 5 NOZZLE. R & R NR 5 FUEL NOZZLE SEAL AT NR2 ENG O/B FUEL RAIL IAW BAMM 767 73-11-05 THRU STEP 5D(5). PERFORMED OPS AND LEAK CK IAW AMM 73-11-05, CHECKS GOOD.SDR CA120507002Fuel Nozzle · leaking(CAN) DURING APPROACH, THE ENGINE HAD A LOW TORQUE INDICATION. THE CREW ELECTED TO SHUTDOWN THE ENGINE BEFORE MAKING AN UNEVENTFUL SINGLE ENGINE LANDING AT DESTINATION. POST FLIGHT INSPECTION REVEALED A FUEL LEAK FROM THE NR 8 FUEL NOZZLE. A DAMAGED O-RING WSDR XV6A2012041200002Guide Vane · burnedAIR TURNBACK. NR 1 ENGINE EGT STARTED TO EXCEED 900'C ON TAKEOFF ROLL. PULLED THRUST LEVER BACK DURING CLIMB TO PREVENT EXCEEDING MAX CONTINUOUS EGT. ALSO, NR 1 ENGINE VIBE INDICATOR WAS SHOWING 4 AND 5 DURING CLIMB. PERFORMED BORESCOPE OF LPT STAGE 1 NOZZSDR ALGA2012032303Diaphragm · backed outNR 1 NOZZLE DIAPHRAM BACKED OFF. INSTALLED NEW AT .835", CURRENT DIMENSION .802. FOUND TO BE CAUSE FOR LOW POWER.SDR UALA2012022001012Fuel Nozzle · malfunctionedNR 1 ENGINE FUEL NOZZLES MALFUNCTIONED.SDR ZI3R025M012720121Swirler · missingZI3R RECEIVED 3 EA, BR710 FUEL NOZZLES FROM MFG. ONE (1) OF THE THREE (3) NOZZLES HAD A MISSING COMPONENT; THE INNER AIR SWIRLER. THE MISSING COMPONENT WAS DISCOVERED DURING AN CUSTOMER REQUIRED X-RAY INSPECTION PERFORMED BY OEM, AND THE MISSING PART WAS VERSDR DXTA2012011004843Fuel Nozzle · cloggedAFTER TAKEOFF AT HIGH POWER SETTING AND RELATIVELY LOW AIRSPEED ON CLIMBOUT, A STRONG ODOR OF FUMES CAME INTO COCKPIT AND CABIN FOR ABOUT 10 MINS. THE APU WAS NOT RUNNING AND ALL ENGINE PARAMETERS WERE NORMAL. ODOR SEEMED TO DISSIPATE DURING CRUISE BUT RETURN
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