JASC 7310
Service difficulty reports · 1,981
Reports filed under 7310 · Engine Fuel Distribution, 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 = '7310' 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 = '7310' 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 F3LA2015051101132Fuel Line · leakingNUMBER 2 ENG FUEL LEAK FROM MAIN FUEL SUPPLY LINE. R & R MAIN FUEL SUPPLY LINE IAW AMM 73-11-11 PAGE BLOCK 401. LEAK CHECKED GOOD. TORQUE WRENCH F9TAB3949C CALIBRATION DATE 10 15, LOG PAGE 896973.SDR DALA2015043003078Filter · leakingCREW REPORTED A FUEL DISAGREE-PROG 2 MESSAGE AFTER 4 HRS OF FLIGHT WITH A 3500LB DIFFERENCE BETWEEN TOTALIZER AND CALCULATED. THE CHECKLIST WAS USED TO VERIFY THAT THERE WAS NOT A FUEL LEAK. TOTALIZER WAS 3500 LB LESS THAN CALCULATED. MAINTENANCE TROUBLESHOSDR ASMF201506004Fuel Filter · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG OIL FILTER BY PASS LIGHT TURNED ON & THE LT ENG CONTROL LIGHT TURNED ON. PERFORMED BITE TO EEC IAW AMM 73-21-00, SHOWING RT ENG FAILURE CODE 73-31072 & LT ENG FAILURE CODE 73-31321, THE ACFT WAS SSDR EPUA20150428003Fuel Line · chafedDURING A FLEET CAMPAIGN DIRECTIVE INSPECTION, DUE TO A PREVIOUS FAILURE IN WHICH THE ENG LOST POWER & LEAKED FUEL, THE LT ENG WAS FOUND TO HAVE A CHAFED ENG FUEL TUBE, PN 3040637. DUE TO THE LEVEL OF CHAFING THE FUEL TUBE NEEDED TO BE REPLACED. THE FUEL TUBESDR EPUA2015042815002Fuel Line · chafedDURING A FLEET CAMPAIGN DIRECTIVE, DUE TO A PREVIOUS FAILURE IN WHICH THE AN ENG LOST POWER & LEAKED FUEL, THE LT ENG WAS FOUND TO HAVE A CHAFED ENG FUEL TUBE, PN 3040637. DUE TO THE LEVEL OF CHAFING THE FUEL NEEDED TO BE REPLACED. THE FUEL LINE WAS FOUND TOSDR EPUA20150429001Fuel Line · chafedNUMBER 1 ENG FUEL LINE, PN 3040637, WAS INSPECTED & FOUND TO HAVE CHAFING THAT EXCEEDED THE LIMITS FOR CONTINUED SERVICE. WE HAVE ELECTED TO INSPECT ALL OF OUR ACFT FOR THIS DEFECT & HAVE DISCOVERED OTHERS REQUIRING PART REPLACEMENT. SB 13250R1, OPTIONAL, ADSDR EPUA20150428001Tube · leakingPILOT ABORTED TAKE OFF DUE TO LOW AND FALLING TORQUE ON LEFT ENGINE. MAINTENANCE INSPECTED LEFT ENGINE AND DETERMINED THAT THE FUEL PRESSURE DELIVERY TUBE (PN: 3040637) HAD DEVELOPED A LEAK. CHAFFING HAD OCCURRED BETWEEN THE FUEL DELIVERY TUBE AND THE STARTESDR 2015FA0000304Warning Light · illuminated(B9573) LOW FUEL FLOW WHILE TAKING OFF.SDR 2015FA0000303Warning Light · illuminated(B9583) LOW FUEL FLOW ON THE GROUND.SDR QMLA2015040215024Filter Element · bypassingON APPROACH FOR LANDING, DURING FLIGHT RECEIVED A MOMENTARY, FUEL FILTER BYPASS, WARNING LIGHT ILLUMINATION. REDUCED POWER & THE LIGHT EXTINGUISHED. AS POWER WAS INTRODUCED AGAIN DURING LANDING THE WARNING LIGHT MOMENTARILY ILLUMINATED AGAIN. LANDED & SHUTDSDR CA150331006Fuel Sys · leaking(CAN) CREW RECORDED A FUEL DISCREPANCY FROM FLIGHT PLAN OF 200-300K. ON TAXI IN DISCREPANCY INCREASED TO 1.5K. WHEN ENGINE WAS CHECKED AFTER SHUTDOWN IT WAS FOUND TO BE LEAKING. MTCE CONFIRMS NR 1 ENGINE LEAKING SIGNIFICANTLY. AIRPORT FIRE DEPARTMENT RESPONDESDR USAA2015033100001Fuel Filter · cloggedNUMBER 2 ENG FUEL FILTER CLOGGED AFTER TAKEOFF CLIMB FOR 10 MINUTES. REPLACED NR 2 ENG FUEL FILTER IAW TASK CARD 26T40073001.SDR CA150325023Fuel Nozzle · leaking(CAN) DURING THE FIRST FLIGHT AFTER FUEL NOZZLES WERE CHANGED, A CLEAR SUBSTANCE WAS FOUND TO BE LEAKING FROM NR 2 ENGINE COWL, THAT APPEARED TO WORSEN. CREW THEN ELECTED TO RETURN TO BASE. ACFT LANDED UNEVENTFULLY, ALL FUEL NOZZLES, RINGS FOR THE TRANSFER TSDR AALA20150226019Fuel Filter · faultyDURING TAKEOFF NR 1 ENG FUEL FILTER INLET PRESS LOW LIGHT ILLUMINATED. TAKEOFF ABORTED AT 40 KNOTS. R & R NR 1 ENG FUEL FILTER. PERFORMED LEAK CHECK IAW AMM 73-12-01-201. SYS CHECKED NORMAL.SDR FDEA201502210565Manifold · rupturedAT APPROX 1000 FEET ON STABLE FLAPS 35 DEGREES APPROACH, THE NR 3 ENG FLAMED OUT. IAW CREW, N2 INDICATION ROLLED BACK & AFTER TOUCHED DOWN, NR 3 ENGINE WAS SHUTDOWN. LT FUEL MANIFOLD FOUND RUPTURED, R & R.SDR KNNA2015031000042Fuel Line · leakingNR 2 ENGINE FUEL LINE FOUND TO BE LEAKING. APPEARED TO BE AT THE JUNCTION BETWEEN THE BRAIDED PORTION AND THE HARD LINE. THE DAMAGED LINE WAS RETURNED TO THE ENGINE LESSOR FOR INSPECTION. THE METAL BRAIDS WERE FOUND TO BE INTACT BUT THE INTERIOR WAS FRACTUREDSDR ASAA2015021210640Shroud · damagedDURING MAINTENANCE, FOUND NR 2 ENGINE, FUEL MANIFOLD PROTECTING SHROUDS AT 6 & 5 O'CLOCK POSITIONS DAMAGED, CRACKED. ACFT GROUNDED. R & R 2 RUBBER, SYNTHETIC MATERIAL, FUEL MANIFOLD SHROUDS. INSTALLED SAFETY CABLE IAW AMM 70-20-01. GOOD FOR SERVICE.SDR ASAA2015020710576Warning Light · illuminatedENROUTE AT CRUISE, NR 2 ENGINE VALVE CLOSED LIGHT ILLUMINATED AND STAYED ON BRIGHT. ALL ENGINE PARAMETERS AND FUEL FLOWS WERE NORMAL. NR 1 ENG FF 2.65, NR 2 ENG FF 2.63. ENGINE PERFORM NORMALLY AND NO OTHER INDICATIONS ABNORMAL. DISPATCH AND MX CONTROL NOTISDR SIMA20150203003O-Ring · damagedWHILE BEING VECTORED FROM APPROACH, WE NOTICED THE NR 1 FUEL QTY ON EICAS QUICKLY WHEN TO 830 LBS & AMBER VENSES 1200 LBS ON NR 2. WE THOUGHT IT TO BE AN INDICATION PROBLEM AT FIRST BUT DECIDED TO DECLARE AN EMER & LANDED WITH NO PROBLEM. CFR CONFIRM MASSIVESDR DALA2015020200840Transmitter · leakingON GROUND, WITH EXTERNAL AIR CONNECTED, STRONG ODOR OF FUEL AND EXHAUST FUMES FROM MID TO AFT OF ACFT. ODOR WAS PRESENT THROUGH MID CLIMB. MAINTENANCE FOUND FUEL FLOW TRANSMITTER LEAKING ON NR 1 ENGINE. R & R UPPER FLANGE O-RING IAW AMM. LEAK CHECK AND PACSDR UIEA2015012800050Filter · damagedNUMBER 1 ENG MAIN FUEL FILTER HOUSING & FILTER HEAD THREADS ARE DAMAGED. R & R IAW AMM 73-11-08. LEAK CHECK ACCOMPLISHED ON TASK CARD 8007 ITEM 14.SDR ASMF201501025O-Ring · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, A FUEL & HYD LEAKS WERE DETECTED. THE PLATFORM WAS CLEANED. PERFORMED REVISION, DETECTING FUEL LEAK IN THE TRANSIENT BLEED VLV DRAIN PORT. THE RT ENG WAS MOTORING AFTER IT WAS STARTED & ENG OPERATIONSDR SWIA2014121940422Line · failedDURING CLIMBOUT, NR 2 ENGINE ROLLED BACK TO IDLE. RETURNED TO FIELD. R & R RT ENGINE P3 LINE TO FUEL CONTROL TUBE ASSEMBLY WITH A SERVICEABLE UNIT IAW AMM. OPS CHECKED GOOD.SDR UIEA2014112300605Fuel Filter · defectiveLEFT ENG FUEL FILTER STATUS MSG. ACCOMPLISHED FIM 73-11 FT 803, NO CONTAMINATION. REPLACED FUEL FILTER IAW AMM 73-11-02 401. COMPLIED WITH POWER PLANT TEST 71-00-00 501 TEST 2, NO LEAKS.SDR CA150120012Fuel Divider · failed(CAN) THE AIRCRAFT WAS STARTED AND TAXIED TO THE RUNWAY, BOTH STARTS HAD NO ABNORMAL INDICATIONS. AT THE RUNWAY THRESHOLD WHILE HOLDING THE BRAKES, THE PILOT APPLIED APPROXIMATELY 80 PERCENT TAKEOFF POWER AND BEFORE THE BRAKES WERE RELEASED, NR 2 ENGINE LOST PSDR CA141202027Engine · power loss(CAN) THE CREW STARTED THEIR SHIFT WITH A WALK AROUND AND AN ENGINE RUN UP. THE AIRCRAFT WAS STARTED AND TAXIED TO THE RUNWAY, BOTH STARTS HAD NO ABNORMAL INDICATIONS. APPLIED APPROXIMATELY 80% OF TAKEOFF POWER OBSERVING THE ENGINE INSTRUMENTS, AND BEFORE TSDR CA141120012Unknown · leaking(CAN) ON TAXI OUT, FUEL WAS OBSERVED LEAKING FROM NR 2 ENGINE. SHUTDOWN NR 2 ENGINE. AIRCRAFT WAS STOPPED AND TOWER WAS ADVISED. CFR MET STATIONARY AIRCRAFT AND DEEMED IT OKAY TO RETURN TO GATE FOR MTC INSPECTION. IFS REPORTED FUEL ODOUR IN THE CABIN. NO NEGSDR UIEA2014111800597Fuel Filter · faultedRIGHT ENG FUEL FILTER EICAS MSG. R & R RT ENG FUEL FILTER IAW AMM 73-11-02. LEAK CHECKED GOOD.SDR 2014FA0000659Fuel Line · brokenDURING CRUISE FLIGHT, RT ENGINE NR 6 CYLINDER EGT AND CHT DROPPED TO ZERO DEGREES AT THE SAME TIME AN ENGINE VIBRATION STARTED. RT ENGINE WAS THEN SHUTDOWN AS A PRECAUTIONARY MEASURE. LANDED AT AIRPORT WITHOUT INCIDENT. INSPECTED RT ENGINE AND FOUND NR 6 CYSDR HALA2014102900178Fuel Sys · malfunctionedEXCESSIVE FUEL FLOW ON NR 1 ENGINE DURING CLIMBOUT + 3-4000 LBS AN HOUR. THEN NORMAL DURING CRUISE/LEVEL OFF NR 1 FUEL USED 1200 LB > THAN NR 2 ENG (CONT) 3 + 20 HRS AFTER DEPARTURE NR 1 ENG FUEL FLOW CYCLING BETWEEN 5- 9000 LBS AN HOUR DURING CRUISE FUEL USESDR AALA20141021002Coupling · leakingLEFT ENG FUEL LEAK FROM MAIN FUEL SUPPLY HOSE DISCONNECT COUPLING. REPLACED LT ENG MAIN FUEL SUPPLY HOSE ASSEMBLY.SDR FDEA201410163174Check Valve · failedAFTER LANDING, AT IDLE NR 2 ENGINE SHUTDOWN. REMOVED LOW PRESSURE BLEED AIR CHECK VALVE FOR INSPECTION IAW MM 36-11-01-6, FOUND ONE FLAPPER HINGE STIFF AND LOWER BEARING CAP LOOSE. REPLACED NR 2 ENGINE LOW PRESSURE CHECK VALVE.SDR UIEA2014101300490Fuel Filter · faultedSTATUS MSG DISPLAY RT ENG FUEL FILTER. R & R RT ENG FUEL FILTER IAW MM 73-11-02 601. OPERATIONS CHECKED NORMAL.SDR ASAA2014100609313Servo · leakingLEAK CHECK AFTER HMU CHANGE FOUND FUEL HEATER SERVO LEAKING FROM AROUND CAP, EVIDENCE SHOWS IT HAS BEEN LEAKING FOR AWHILE. CLASSIFIED AS CONTINUOUS. ACFT GROUNDED. REMOVED SERVO HEATER IAW MM 73-11-07-000-801-F00. INSTALLED SERVO FUEL HEATER IAW MM 73-11-0SDR BIAA20141005001Packing · cutWHILE ON TAKEOFF ROLL, PILOT NOTICED A STRONG ODOR OF FUEL AND WITNESS A LOSS IN POWER OF THE ENGINE.SDR 9WGA201409270001Fuel Filter · dirtyNR 2 ENGINE FUEL FILTER OFF LIGHT DURING TAKE OFF ROLL. REMOVED, CLEANED AND REINSTALLED FUEL FILTER. PERFORMED ENGINE RUNS. SYSTEM OPERATIONALLY CHECKED NORMAL.SDR QMLA2014092714117Valve · leakingDEPARTED FOR SCENE FLIGHT MEETING EMS ON HOSPITAL PAD. THIS IS AN 18 MINUTE FLIGHT, ABOUT 15 MINUTES INTO THE FLIGHT THE CREW MEMBER IN THE BACK STARTED SMELLING OIL & FUEL TYPE FUMES. THE PILOT COULD AS WELL AS THE OTHER CREW MEMBER IN THE FRONT. ABOUT 1 -SDR ASAA2014092309211Pump · leakingAFTER ENGINE INSTALLATION, OPS & LEAK CHECK, NR 1 ENGINE FUEL PUMP PAD LEAKAGE. CLASSIFIED AS A RUNNING LEAK. ACFT GROUNDED. REMOVED FUEL PUMP PACKAGE IAW T/C 73-11-01-000-801-F00, ACCOMPLISHED STEPS 2 THRU 2H (15). FINISHED STEP 2.H, 16, 17, 18. FUEL PUMSDR RU3A20140916032Fuel Line · crackedAFTER ARRIVAL A FUEL LEAK ON THE NR 1 ENG WAS NOTED. A CRACK IN THE PRIMARY FUEL LINE FROM THE FCU TO THE SOV WAS DISCOVERED.SDR UIEA2014090400421Fuel Filter · defectiveLEFT ENG FUEL FILTER EICAS MSG. R & R LT ENG FUEL FILTER IAW AMM 73-11-02, LEAK CHECKED OK.SDR CA140908009Fmu · leaking(CAN) ACFT WAS GROUNDED DUE TO HEAVY FUEL LEAK NOTICED FROM THE NR 1 DRAIN. NO EXTERNAL FUEL LEAK WAS NOTICED FROM FMU, HEATER OR TRANSFER TUBES. THE FMU WAS REPLACED AT CUSTOMER FACILITY.SDR SWAA2014082131063O-Ring · faultyAPPROACHING AIRPORT NOTICED AN IMBALANCE OF 900LBS LT TANK LOW. R & R O RING IAW MM.SDR CA140826009Fuel Sys · bypassing(CAN) WHILE TAXIING, PILOT NOTICED FUEL FILTER IMPENDING BYPASS INDICATION. CREW ELECTED TO RETURN TO RAMP. TROUBLESHOOTING.SDR CA140804013Bracket · damaged(CAN) MFG IDENTIFIED AN ISSUE WHERE THE FUEL TUBE BRACKET, ST3493-06, WAS INSTALLED ON A ENGINE WITH RUBBER MISSING ON 50 PERCENT OF THE BRACKET. THIS BRACKET IS APPLICABLE TO ENGINE MODELS. AN ENGINEERING ASSESSMENT IDENTIFIED THAT OVER TIME THERE IS A CHANCSDR UIEA2014071900333Filter · faultyRIGHT ENG FUEL FILTER STATUS MSG. REPLACED RT ENG FUEL FILTER IAW AMM 73-11-02, NO LEAKS NOTED.SDR S9BA2014072100007Line · leakingSTRONG ODOR OF OIL & FUEL IN CABIN. LANDED, INSPECTED ALL FUEL LINES AND OIL COMPONENTS THE LT ENGINE FOR ANY POSSIBLE LEAKAGES THAT MAY CAUSE THE ODOR IN THE CABIN. FOUND AGB TO HMU LINE LEAKING AFTER INITIAL ENGINE RUN. TIGHTEN LINE IAW MM 730000, STEP 9ASDR QXEA2014062800547Actuator Valve · failedDURING CLIMBOUT 14000 FT TO FL 220, NR 1 AND 2 FUEL TEMP ON ED TURNED RED, RAN EAC. TURNED AUX PUMPS ON BRINGS TEMP DOWN BUT WENT RIGHT BACK UP WHEN AUX PUMPS TURNED OFF BOTH FUEL TEMPS RED ON GROUND WITH AUX PUMPS RUNNING BOTH TEMPS DID NOT EXCEED 74 DEGRSDR CALA2014063091378Bypass Valve · leakingFLUID DRAINING FROM NR 1 ENG. DETERMINED LEAK COMING FROM FUEL OIL COOLER BYPASS VLV AT RATE OF 8 DROPS AT IDLE & 10 DROPS STATIC. ACCOMPLISHED 5 MIN IDLE RUN NO DRIPS RUNNING OR STATIC.SDR QMLA2014061914075Valve · faultyDEPARTED BASE FOR A SCENE FLIGHT AT 16:06. LANDED ON SCENE AT 16:35. AFTER AN EXTENDED RUN TIME ON THE GND SHUT DOWN THE ENG TO SAVE MY FUEL FOR THE MISSION. AFTER LOADING THE PATIENT IN THE ACFT THE ENG FAILED TO RESTART. IT REACHED 210 RPM & ACTED AS IF SDR ASAA2014061808273Heater · leakingWHILE WORKING TC QA07 PNC, NR 2 ENG FUEL FILTER DIFFERENTIAL PRESSURE SWITCH REPLACEMENT, FOUND FUEL HEATER SERVO LEAKING FROM UPPER SEAM. GROUNDED. REPLACED SERVO FUEL HEATER IAW AMM 73-11-07. SERVO FUEL HEATER INSTALLATION TEST AND LEAK CHECK GOOD REF 71-0
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