JASC 7314
Service difficulty reports · 1,734
Reports filed under 7314 · Engine Fuel Pump, 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 = '7314' 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 = '7314' 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 ASMF20180625007Pump · leakingDURING A RIGHT ENGINE VIBRATION TEST. DETECTED A FUEL LEAK THAT WAS OUT OF LIMITS. MAINTENANCE REPLACED THE RIGHT FUEL PUMP IAW AMM 73-11-01, TESTED GOOD.SDR 2018FA0000179Pump · failedDURING A DUAL LESSON AT 2500MSL THE AIRCRAFT EXPERIENCED A POWER INTERRUPTION. FOLLOWING THE CHECKLIST, THE ELECTRICAL FUEL PUMP WAS TURNED ON WHICH RESTORED NORMAL POWER IMMEDIATELY. THE FLIGHT RETURNED TO KLOT WITHOUT FURTHER INCIDENT. UPON INSPECTION OF THESDR JRAA2018041200001Pump · brokenNR 1 ENGINE FAILED DURING TAKEOFF, GOT 3 BACK FIRING BEFORE ENGINE SHUTDOWN, QRH COMPLETED. REMOVED FUEL PUMP AND DISCOVERED IT HAD A BROKEN SHAFT. INSTALLED NEW FUEL PER MM 72-00-61 AND OPS CHECKED IT PER AMM 71-09-100.SDR ASAA2018040124113Pump · leakingNR 2 ENGINE DEVELOPED A FUEL LEAK. ACFT GROUNDED. REMOVED THE NR 2 ENGINE HMU IAW TC N8473000. REMOVED THE NR 2 ENGINE FUEL PUMP IAW AMM 73-11-11. REMOVED THE NR 2 ENG MAIN OIL HEAT EXCHANGER IAW AMM 79-21-02. REMOVED NR 2 ENGINE SERVO FUEL HEATER IAW AMMSDR ASAA2018020423485Pump · leakingFUEL LEAK FROM THE NR 2 ENGINE. ACFT GROUNDED. ACCOMPLISHED TEST 3A AT IDLE POWER, LEAK CHECKED IAW AMM 71-00-00-700-801-F00. FOUND LEAK FROM FUEL PUMP PAD DRAIN. LEAK IS AT 38 DROPS PER MINUTE. REMOVED AND REPLACED THE NR 2 ENGINE FUEL PUMP IAW AMM 73-1SDR SWAA2018012419306Pump · low pressureDURING CLIMB, THE NR 2 ENGINE DID NOT ADVANCE TO FULL CLIMB THRUST FROM REDUCED THRUST FOR 45 SECONDS. R & R NR 2 ENGINE FUEL PUMP IAW AMM.SDR ASAA2018011423169Pump · leakingON ENGINE START RAMP REPORTED FUEL RUNNING OUT OF THE BOTTOM OF NR 2 ENGINE, A FIRE BALL OUT THE BACK AND FUEL BEING INGESTED IN TO THE INTAKE WITH EVIDENCE OF RESIDUAL FUEL ON THE BOTTOM PORTION OF THE INLET. PILOTS REPORTED NORMAL ENGINE INDICATIONS. GROUNDESDR ASAA2017120522806Pump · leakingWHILE ACCOMPLISHING TSR 701083 FOUND FUEL LEAKING FROM NR 2 ENGINE FUEL PUMP DRAIN PAD. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG FUEL PUMP REF AMM 73-11-11-000-801-F00 & AMM 73-11-11-400-801-F00. REMOVED AND REPLACED NR 2 ENG FUEL PUMP SEAL REF AMM 72-60-SDR ASAA2017120122754Seal · leakingFOUND OIL LEAKING FROM #2 ENGINE. GROUNDED - YES. REMOVED THE FUEL PUMP PACKAGE AND REPLACED SEALOL SEAL PER B737-800 MM 72-60-00. REINSTALLED THE FUEL PUMP PACKAGE PER AMM 73-11-01. IDLE LEAK LK CK GOOD, EEC AND ACTUATORS TEST GOOD. ALTERNATE DEACTIVATION PROSDR 2017FA0000613Pump · wornTHE MAIN FUEL PUMP CUSTOMER REPORTED AN UNSERVICEABLE IMPELLOR SHAFT WHICH CAUSED AN IN-FLIGHT SHUTDOWN. DISASSEMBLY OF THE PUMP REVEALED THAT THE MAIN DRIVE SHAFT SPLINE WAS EXCESSIVELY WORN AND CONTAINED A DEEP CIRCUMFERENTIAL GROOVE CAUSED BY ROTATIONAL WSDR SWAA2017110817669Pump · faultyAIR TURNBACK/DECLARED EMERGENCY, NR 1 ENGINE WOULD NOT INCREASE TO FULL POWER. R&R FUEL PUMP PER MT.SDR FDEA201710082880Pump · malfunctionedDURING TAKEOFF ROLL AT 120 KIAS, ENG FAIL LIGHT ON GLARESHIELD ILLUMINATED. REJECTED TAKE-OFF AND COMPLIED WITH QRH. AS PER CREW VERBAL DEBRIEF, THEY DID NOT FEEL A ROLL DURING TIME OF EVENT AND HEARD AN ENGINE POWER BACK. REQUIRES TROUBLESHOOTING. REPLACED THSDR ASAA2017100222096Pump · leakingNR 1 ENGINE FUEL LEAKING FROM FUEL PUMP PAD DRAIN. ACFT GROUNDED. REMOVED THE FUEL PUMP, IAW AMM 73-11-01-000-801-F00. INSTALLED A NEW FUEL PUMP IAW AMM 73-11-01-000-801-F00. OPS AND LEAK CHECKED GOOD IAW AMM TEST TABLE 71-00-00-800-811-F00.SDR ASAA2017092522051Pump · leakingNR 1 ENGINE FUEL LEAK. GROUNDED - YES. RAN NR 1 ENGINE, FOUND FUEL LEAKING FROM FUEL PUMP PAD DRAIN AND TO BE OUT OF LIMITS IAW AMM 71-71-00-200-801-F00 FIG 605 LEAK LIMIT TABLE. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP, REF AMM 73-11-11. OPS & LEAK CHECKED SDR CALA2017090403047Pump · faultyLEFT ENG VALVE LIGHT ILLUM DURING ENG START NO FUEL FLOW. REPLACED FUEL PUMP REF AMM 73-11-01. ACCOMPLISHED ACCELERATION TIME TEST REF JRH 2-5-64. TIME TEST PASSED. FUEL FLOW WAS NORMAL AT IDLE (1.09), FLT IDLE (1.49) AND 95% TO (1.39 EPR FUEL FLOW AT 13.6K). SDR ASAA2017083021773Pump · leakingDURING START OF THE NR 2 ENGINE. FUEL FOUND LEAKING. GROUND CREW REPORTED FUEL LEAK DURING AND AFTER START. ACFT GROUNDED. PERFORMED ENGINE VENTS AND DRAIN INSPECTION ON THE NR 2 ENGINE. RAN THE NR 2 ENGINE TWO TIMES AT IDLE POWER. FUEL LEAKING DURING STARTSDR UIEA2017082701553Warning Light · illuminatedRT CENTER FUEL PUMP PRESSURE LIGHT AT ENGINE START.SDR CALA2017082102796Pump · faultyON DESCENT AT APROXIMATELY 10K, FLT CREW FELT A SLIGHT SHUDDER AND NOTED THAT THE RT ENGINE EGT WAS ROLLING BACK WITH ASSOCIATED LOW OIL PRESSURE LIGHT ILLUMINATING AND INDICATOR SHOWED 5 PSI. FOM USED AND SECURED ENGINE BY PULLING FIRE HANDLE. EMERGENCY DECLSDR AALA201708079013Pump · leakingTHERE HAVE BEEN SEVERAL CREW REPORTS OF AN OIL OR FUEL LEAK FROM THE RIGHT ENGINE. FOUND LEAK COMING FROM FUEL PUMP PAD DRAIN. REPLACED ENGINE FUEL PUMP.SDR SIMA20170804002Pump · failedDURING TAKEOFF ROLL, AT ABOUT 90 KNOTS, 5 PERCENT N1 LOSS FOR ABOUT 2 SECONDS. FOLLOWED BY 5 PERCENT N1 INCREASE, ALL OTHER PARAMETERS REMAINED NORMAL REMOVED AND REPLACED THE NR 1 ENGINE FUEL PUMP IAW EMM 73-00-00, SPECIAL PROCEEDURE 002. PERFORMED OPS ASDR MUIA20170802001Pump · unknownCREW REPORTED ABNORMAL ENGINE INDICATIONS. REPLACED ENGINE DRIVEN FUEL PUMP AND FCU.SDR AALA201708239025Pump · faultyDESCENDING INTO TPA AT 11,000 FEET, ENGINE SPOOLED FROM FLIGHT IDLE, AIRCRAFT YAWED, AND NR 2 ENGINE SHUTDOWN. CAPTAIN AND FIRST OFFICER COMPLETED ECAM. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE HIGH PRESSURE FUESDR 2017FA0000641Pump · high pressureTHE MECHANICAL LW-15473 FUEL PUMP WAS BEING REPLACED DUE TO AGE. UPON REVIEW OF LYCOMING SL L255A, IT APPEARED THAT THE 62B26931 WAS A DIRECT REPLACEMENT. UPON INSTALLATION THE AIRCRAFT WAS PULLED OUT FOR A RUN UP. USING THE SAME START TECHNIQUE WE HAVE BEESDR CALA2017071702256Pump · faultyLEFT ENGINE FAILED TO ACCELERATE DURING TAKE OFF. AUTOTHROTTLES WERE ENGAGED. REMOVED AND REPLACED THE FUEL PUMP IAW MM 73-11-01, REMOVED AND REPLACED THE FUEL METERING UNIT IAW MM 73-21-01. PERFORMED TEST 2A LEAK TEST, WET MOTOR TEST, TEST 3 IDLE POWER, TESDR YAXA2017071101Pump · leakingENGINE WOULD NOT SHUT DOWN WITH MIXTURE CONTROL AT IDLE CUTOFF. FOUND ENGINE DRIVEN FUEL PUMP LEAKING FROM RELIEF VALVE INTO DECK PRESSURE REFERENCE LINE INTO INTAKE. ENGINE DRIVEN FUEL PUMP REPLACED WITH NEW.SDR ASAA2017070421266Pump · leakingNR 1 ENGINE FUEL PUMP DRAIN AT GEARBOX LEAKING 40 DROPS PER MINUTE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE FUEL PUMP IAW AMM 73-11-01.SDR AALA20170627013Pump · faultedREJECTED TAKE OFF AT 76 KNOTS, NR 2 ENGINE DID NOT ACHIEVE FULL POWER. N2 IDICATION TURNED RED, AMBER CAUTION LIGHT FLICKERED ON/OFF. NO ECAM MESSAGES DISPLAYED. MAINTENANCE REPLACED RIGHT ENGINE FUEL PUMP PER AMM 73-21-41. ACCOMPLISHED MCM 71-95-02 FOR RIGHT SDR AALA201706299020Fmu · faultedAIRCRAFT WAS GROUNDED. REJECTED TAKE OFF AT 76 KNOTS, #2 ENGINE DID NOT ACHIEVE FULL TOGA POWER. N2 IDICATION TURNED RED, AMBER CAUTION LIGHT FLICKERED ON/OFF. NO ECAM MESSAGES DISPLAYED. MAINTENANCE REPLACED RIGHT ENGINE FMU PER AMM 73-94-12. ACCOMPLISHED MCMSDR CALA2017060501674Pump · faultyLEFT ENG PRODUCING REDUCED THRUST PROGRESSIVE LOSS WITH ALT GAIN. EMERGENCY DECLARED. REMOVED AND REPLACED LOW PRESSURE FUEL PUMP ON #1 ENG PER AMM 73-11-01. LEAK CHECK GOOD. OPS CHECK PER POWER PLANT TEST 71-00-00-700-804-R03.SDR SWAA2017060514120Pump · faultyNR 2 ENGINE WOULD NOT DEVELOP CLIMB THRUST OUT OF 10,000 FEET, RETURNED TO DEPARTURE. R & R THE NR 2 ENGINE FUEL PUMP IAW MT.SDR 2017FA0000350Pump · leakingPILOT REPORTED A FUEL LEAK FROM THE ENGINE DRIVEN FUEL PUMP AFTER FLIGHT. INSPECTED PUMP, REMOVED DRAIN LINE FROM BOTTOM OF PUMP, VERIFIED LEAK. PERFORMED GROUND RUN FOR OPERATIONAL LEAK CHECK, COULD NOT DUPLICATE. CONTACTED TECH SUPPORT, AND WAS ADVISED TOSDR ASAA2017032920339Pump · leakingDUE TO HISTORY AND TO PREVENT FUTURE DELAYS T/S NR 1 ENGINE FOR FUEL LEAK DURING ENGINE START. GROUNDED - YES. FOUND LEAK SOURCE TO BE NR 1 ENGINE FUEL PUMP DRAIN. REMOVED NR 1 ENGINE FUEL PUMP PACKAGE, REF TASK CARD N8473000. INSTALLED MAIN OIL/FUEL HEAT EXCHSDR 2017FA0000120Pump · defectiveENGINE DRIVEN PUMP FAILED TO MAINTAIN PROPER FUEL PRESSURE.SDR 2017FA0000084Pump · failedMECHANICAL ENGINE DRIVEN FUEL PUMP FAILED IMMEDIATELY AFTER ENGINE WAS OVERHAULED. WE HAVE FOUND INTERNAL COMPONENTS OF THIS ITEM FAIL WITHIN A FEW HOURS OF SERVICE.SDR ASAA2017022419931Pump · leakingNR 1 ENGINE LEAKING FUEL FROM THE FUEL PUMP PAD DRAIN LINE WITH THE NR 1 ENGINE RUNNING. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE FUEL PUMP IAW AMM 73-11-01. OPS & LEAK CHECKED GOOD IAW AMM POWERPLANT TEST TABLE 71-00-00-800-811-F00.SDR CALA2017012000144Pump · faultyR N1 3 PCT LESS THAN L N1 AT TAKEOFF PWR. ALL OTHER INDICATIONS IN NORMAL RANGE. OK INFLT PER INBOUND CREW, SHOULD READ LEFT ENGINE WAS 3% LOWER N1 THAN RIGHT ENGINE. REPLACED NR 1 ENG FUEL PUMP DUE TO FAILED PRESSURE TEST PER AMM 73-11-01-705-001-H00. PER AMMSDR 2017FA0000144Pump · inoperativePRE-FLIGHT RUN-UP DISCOVERED LACK OF TAKE OFF POWER AND ENGINE VIBRATION. THE AIRCRAFT FLIGHT WAS ABORTED AND THE AIRCRAFT RETURNED TO THE HANGER. THE ENGINE WAS TROUBLESHOT AND THE ENGINE DRIVEN FUEL PUMP WAS DISCOVERED TO HAVE MULTIPLE DEFECTS IN ITS LOWERSDR ASOA201701015001Pump · erraticPILOT REPORTED LEFT ENG BETWEEN 16,000 AND FL220 ENGINE WILL ROLLBACK FROM 87.2 TO 85.9. THE ENGINE WILL ROLL UP AND DOWN TILL FL220 THEN IT STABILIZES. MX REMOVED AND REPLACED FUEL PUMP ASSY ON LEFT ENGINE WITH OPERATIONAL AND LEAK CHECKS GOOD. A/C WAS APPROVSDR AALA20161220009Pump · faultyDURING INITIAL THRUST APPLICATION FOR TAKEOFF, RIGHT ENGINE WOULD NOT ACCELERATE PASS 35 PERCENT. ABORTED TAKEOFF AT LOW SPEED. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED HYDROMECHANICAL UNIT AND FUEL PUMP ASSEMBLY IAW AMM 73-94-12. HIGH POWER RUN CHECKEDSDR 2016FA0000601Pump · failedOVERHAULED ENGINE DRIVEN FUEL PUMP FAILED AFTER 23.2 HOUR TIS. FUEL PUMP FAILED TO MAINTAIN FUEL PRESSURE AT IDLE RPM. MAJOR PROBLEM INDUSTRY WIDE.SDR 2016FA0000600Pump · failedOVERHAULED ENGINE DRIVEN FUEL PUMP FAILED AFTER 23.2 HOUR TIS. FUEL PUMP FAILED TO MAINTAIN FUEL PRESSURE AT IDLE RPM. MAJOR PROBLEM INDUSTRY WIDE.SDR ASAA2016111918747Pump · leakingNR 1 ENGINE FUEL PUMP LEAKING AT THE DRAIN LINE APPROXIMATELY 1 DROP PER SECOND. ACFT GROUNDED. REMOVED AND REPLACED THE FUEL PUMP IAW AMM 73-11-01, AMM 79-21-02-400-801-F00 STEP 3. (1), AND AMM 73-11-01-400-801-F00 STEP 3 H (1,2).SDR ASAA2016111918749Pump · leakingUPON ENGINE START NR 2 GROUND CREW NOTICED FUEL DRIPPING FROM ENGINE NR 2. GROUNDED, YES. OPENED COWLS & RAN ENGINE AT IDLE, UPON START LARGE QUANTITY OF FUEL CAME OUT CONTINUOUSLY FROM FUEL PUMP PAD DRAIN LINE. ACCOMPLISHED FUEL PUMP PACKAGE REMOVAL, REF AMM SDR ASAA2016110918634Pump · leakingDURING ENGINE RUN FOUND LEAK FOR THE FUEL PUMP PAD DRAIN IAW AMM 71-71-00-200-801-F00 FIGURE 605. ACFT GROUNDED. R & R THE PUMP IAW AMM 73-11-01-400-807 ITEM 3. A.-J. LEAK & OPS CHECKED OK.SDR WX0A2016102673196Pump · failedAT 13,000 FEET ENG NR 2 ROLLED BACK AND FAILED. FOLLOWED ECAM + EQRH ACTIONS AND ATTEMPTED RELIGHT. ENG GOT TO 38% DURING RELIGHT PROCEDURE AND WENT NO FURTHER. SECURED ENG PER EACM. ENG WINDMILLED TILL APPROX 5 MINS FROM LANDING. OVERWEIGHT LANDING AT 14SDR 2016FA0000548Washer · detachedDURING A 50 HOUR OIL CHANGE INSPECTION, THE QUICK STYLE OIL DRAIN BECAME WEDGED OPEN BY DEBRIS/FOD. THE QUICK DRAIN WAS REMOVED BY MAINTENANCE PERSONEL AND DEBRIS/FOD THAT WAS LODGED IN QUICK DRAIN WAS DETERMINED TO BE THE WASHER FROM THE FUEL PUMP UPPER ACTUSDR AALA20160924002Seal · leakingDURING CRUISE A BURNING TYPE ODOR WAS REPORTED THROUGHOUT THE FLIGHT DECK AND MAIN CABIN. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED FIM 21-00-00-810-806 AND VERIFIED OIL ODOR FROM NR 2 ENGINE BLEED AIR. FOUND OISDR JJBA20160916007Pump · inoperativeNR 1 ENGINE SURGED IN-FLIGHT CAUSING AN OVER TORQUE AND ACFT BECAME UNCONTROLLABLE. CREW THEN SHUTDOWN THE ENGINE. REMOVED MFC AND FUEL PUMP, MFC PN 3244853-19, SN-C31243V, TT-7648.77, TC-9192. UPON TAKEOFF CLIMB, BOTH ENGINES WERE OPERATING TOGETHER NORMALSDR REXA2016090301676Pump · malfunctionedLEFT ENGINE ROLLED BACK TO IDLE AT 1000 FT. N1 & ITT NORMAL FOR IDLE N2 70% ACCOMPLISHED QRH ENGINE SHUTDOWN. R & R THE ENGINE FUEL PUMP IAW AMM 73-11-01, R & R THE ENGINE MAIN FUEL CONTROLLER IAW AMM 73-21-01. OPS CHECKED GOOD IAW AMM 71-00-00SDR SWAA2016090855582Pump · disengagedDURING CLIMB THROUGH 5000 FEET, AUTOTHROTTLE DISENGAGED. NR 2 ENGINE WAS AT CLIMB N1 OF 95%. NR 1 ENGINE WAS AT 90% N1, NR 1 ENGINE WOULD NOT ADVANCE PAST 90% N1 WITH THRUST LEVER FULL, FORWARD. BOTH EECS WERE ON. R & R FUEL PUMP IAW MT.
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