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 CA140114002Pump · failed(CAN) ENGINE FAILED TO LIGHT OFF DURING START SEQUENCE. TROUBLESHOOTING FOUND ENGINE DRIVE FUEL PUMP TO BE AT FAULT. REPLACEMENT OF FUEL PUMP CORRECTED THE ISSUE.SDR SIMA20131220007Pump · failedAFTER TAKEOFF HAD ENG 1 LOW PRESS INDICATION. THE RELAY COULD BE HEARD BEHIND CAPTAIN SEAT GOING ON & OFF CONSTANTLY. PROBLEM WAS FOUND WHEN USING PUMP 1B ON NR 1 ENG. AIRCRAFT WAS REMOVED FROM SERVICE. R&R FUEL PUMP 1B IAW EMB 145 AMM 28-21-01. OPC AND LSDR CA131230001Pump · damaged(CAN) ENGINE COULD NOT ACHIEVE LIGHT OFF DURING THE START SEQUENCE. TROUBLESHOOTING FOUND RT ENGINE DRIVEN FUEL PUMP PRODUCTING ZERO FUEL PRESSURE. REMOVAL OF FUEL PUMP SHOWED THE AFTER BEARING OF THE FUEL PUMP DAMAGED. REPLACEMENT OF ENGINE FUEL PUMP CARSDR CALA2013121393648Pump · failedENG FAILED 2 MINUTES AFTER START, NO OTHER INDICATIONS. ENG AUTO SHUTDOWN SEE PL 7436002 FOR REPLACEMENT OF NR 2 ENG LOW - HIGH PRESS FUEL PUMP. NR 2 ENG OPERATIONS & LEAK CHECKED GOOD.SDR 2013FA0000693Pump · leakingUPON FIRST START SINCE ENGINE OVERHAUL, FUEL BEGAN LEAKING FROM THE FUEL PUMP OVERBOARD DRAIN. FUEL PUMP WAS A NEW, PN AF-15473. REPLACED THAT FUEL PUMP WITH ANOTHER NEW FUEL PUMP, PN AF-15473. THIS SECOND NEW FUEL PUMP BEGAN LEAKING AFTER APPROXIMATELY 8 HSDR CA131031001Pump · leaking(CAN) DURING HELICOPTER 50 HR INSPECTION, THE ENGINE DRIVEN FUEL PUMP WAS FOUND TO BE LEAKING OIL FROM THE WEEP HOLE. FUEL PUMP REPLACED.SDR ASMF2013110800009Pump · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED. MAINTENANCE DETECTED THE FUEL PUMP DAMAGED ON RT ENGINE, SO FUEL PUMP WAS REPLACED IAW AMM 73-11-01 AND TESTED IAW AMM 71-00-00, ALL CORRECT.SDR CALA2013101592076Pump · leakingNR 1 ENG IS LEAKING FUEL OUT OF LOWER SIDE OF FUEL PUMP CASE TRANSFER TUBE JOINT. REMOVED FUEL PUMP & FUEL CONTROL, DISCONNECTED MAIN FUEL LINE.SDR SWAA2013101821263Pump · failedIN FLIGHT SHUT DOWN, DIVERSION NR 2 ENGINE ROLLED BACK & SHUT DOWN IN FLIGHT. R & R NR 2 ENGINE MEC FUEL PUMP ASSEMBLY IAW MT.SDR SWAA2013102121289Pump · faultyREPORTED SMELL OF JET A IN CABIN FROM ROW 13 AFT. R & R NR 1 ENGINE MAIN FUEL PUMP ASSEMBLY & HMU ASSEMBLY IAW MT.SDR GULA2014F00057Pump · failedLEFT ENGINE DRIVEN FUEL PUMP FAILED DURING GROUND TRIM RUN UP. UNABLE TO ADJUST FUEL FLOW FOR STABLE FLOW. FUEL FLOW WAS FLUCTUATING AT MID RANGE AND MAX POWER SETTINGS. FAILED ON MAX POWER DROPPING DOWN TO BELOW MID POWER SETTING.SDR ASMF201310009Pump · leakingDURING RT ENGINE TEST, MAINTENANCE DETECTED FUEL LEAK OF 80 DROPS PER MINUTE IN THE FUEL PUMP PAD DRAIN DURING IDLE POWER OPERATION; SO THE RT ENGINE FUEL PUMP WAS REPLACED IAW AMM 73-11-01, TESTED CORRECT.SDR CALA2013092791505Pump · faultyREF LOG 1, PER FIM 76-11 FAULT TREE 807. REPLACE NR 1 ENG FUEL PUMP ASSEMBLY IAW AMM. REMOVED NR 1 ENG FUEL PUMP & FMU IAW AMM. OFF UNIT MR73150-111, NEW PUMP ON ORDER OSTF Z7157.SDR JJBA20130914008Pump · inoperativeDURING CLIMB, NR 2 ENGINE POWER LEVER NOT RESPONSIVE. R & R NR 2 ENGINE MFC AND FUEL PUMP AND RIGGED.SDR CA130919005Pump · low pressure(CAN) PILOT REPORTED A ROUGH RUNNING ENGINE DURING FLIGHT. DURING THE COURSE OF MAINTENANCE CHECKS IT WAS FOUND THAT THE ELECTRIC FUEL PUMP WAS NOT PUTTING OUT THE REQUIRED PRESSURE AS INDICATED BY MFG SID97-3F. A SERVICEABLE PUMP WAS INSTALLED AND ACFT RUNSSDR 2013FA0000566Pump · malfunctionedDURING ENGINE OPERATION, THE MIXTURE CONTROL STOP PIN HAD BECOME LOOSE AND VIBRTED OUT PARTIALLY, LOCKING THE MIXTURE IN THE FULL RICH POSITION. IT IS SUSPECTED THAT DUE TO HEAVY USE AS A TRAINING ACFT WITH REPEATED STOP TO STOP OPERATION OF THE MIXTURE CONTRSDR USAA2013090600001Pump · contaminatedON CLIMBOUT CREW REPORTED EICAS FUEL NR 2 LOW LEVEL REQUIRING LANDING AT NEAREST SUITABLE AIRPORT. MX FOUND PLASTIC PAPER ABSORBANT ON ENGINE FEED EJECTOR PUMP. REMOVED DEBRIS AND R & R ENGINE FEED EJECTOR PUMP.SDR ASMF201309002Pump · leakingDURING OVERNIGHT CHECK, MX PERSONNEL ATTENDED THE NRC A0732762 TO CORRECT FUEL LEAK IN RT ENGINE OF 40 DROPS IAW MINUTE THROUGH THE FUEL PUMP PAD DRAIN DURING IDLE POWER OPERATION. RT ENGINE FUEL PUMP WAS REPLACED IAW AMM 73-11-01, TESTED CORRECT.SDR CA130808003Motor · failed(CAN) PILOT NOTICED AN UNUSUAL BOOST PUMP NOISE AT START UP, SUSPECT INTERNAL GEAR FAILURE IN MOTOR.SDR CA130813001Pump · leaking(CAN) DURING 100 HR INSPECTION OF THE ACFT THE ENGINE DRIVEN FUEL PUMP WAS FOUND TO BE LEAKING OIL. FUEL PUMP REPLACED.SDR CA130807004Pump · failed(CAN) AFTER LANDING, FUEL WAS DRAINING FROM THE EPA CAN OVERFLOW TUBE. IT WAS DISCOVERED THAT THE ENGINE DRIVEN LOW PRESSURE FUEL PUMP WAS LEAKING FUEL FROM ITS DRAIN LINE AT A RAPID RATE. THE FUEL PUMP WAS REPLACED AND NO LEAKS WERE FOUND. (TC# 20130807004)SDR HYIA08032013001Pump · faultyRT ENGINE POWER LOSS AND LOSS OF FUEL FLOW IN CRUISE POWER SETTING. PUMP FOUND FAULTY.SDR JJBA20130731014Pump · malfunctionedNR 1 ENGINE FLUCTUATED. R & R ENGINE MFC/HP FUEL PUMP. OPS AND LEAK CHECKS SATISFACTORY.SDR YN8R201307310001Pump · leakingAFTER FUELING, PILOT NOTICED FUEL DRIPPING FROM GANG DRAIN BENEATH ENGINE. DISCOVERED FUEL WAS DRIPPING FROM ENGINE DRIVEN FUEL PUMP AT A RATE OF A DROP EVERY THREE SECONDS.SDR SIMA20130724005Pump · inoperativeTHE CREW REPORTED THE NR 2 ENGINE DURING ARE DECENT SURGED POWER AND IGNITIONS SWITCH BETWEEN A AND B ALL OTHER ENG IND WERE NORMAL. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 2 ENGINE FUEL PUMP METERING UNIT IAW MM 73-21-SDR CA130710010Stop Pin · backed out(CAN) THE PILOT REPORTED THAT HIS MIXTURE CONTROLS WHERE A FULL KNOB OUT FROM EACH OTHER AND FUEL FLOWS WHERE OUT FROM EACH OTHER DURING GROUND RUN. INSPECTION REVEALED THE MIXTURE STOP PIN ON THE REAR ENGINE FUEL PUMP HAD COME OUT. THE MIXTURE CONTROL COULDSDR UALA2013070804723Pump · leakingFOUND FUEL LEAKING OUT OF FUEL PUMP DISCHARGE PORT. COMPLETED FUEL PUMP & FUEL CONTROL INSTALLATION IAW MM 73-21-01. WET MOTOR AND 5 MINUTE IDLE LEAK CHECK COMPLETED.SDR UALA2013070504706Pump · leakingNR 4 ENG FUEL PUMP LEAK FOUND. REPLACED THE NR 4 ENG FUEL PUMP IAW AMM. ACCOMPLISHED THE NR 3 IDLE POWER TEST IAW AMM 71-00-00P501. TESTED GOOD.SDR UALA2013071004817Pump · failedNR 2 ENGINE FLAMED OUT ON GROUND. AFTER FLAMEOUT, RESTART ABORTED TO PRECLUDE OVERTEMP. R & R RT ENGINE FUEL PUMP IAW AMM. R & R FUEL CONTROL IAW AMM.SDR 4RPA201307010001Pump · failedLEFT ENGINE FUEL FLOW DROPPED FROM 25 GALLONS AN HOUR AT TOP OF CLIMB TO 7 GALLONS AN HOUR AT ALL POWER SETTINGS. ELECTRIC FUEL PUMP SWITCH ALSO FAILED. PILOT USED ENGINE PRIMER BUTTON TO KEEP ENGINE RUNNING. USE OF PRIMER BUTTON INCREASED FUEL FLOW TO 25 GSDR CA130722010Pump · low pressure(CAN) ON AN INSPECTION PRE-RUN UP IT WAS FOUND BY MAINTENANCE THAT THE FUEL PRESSURE WAS ON THE LOW SIDE OF THE GREEN BUT NOT IN THE STANDARD RANGE. FURTHER INSPECTION REVEALED A WORN ENGINE DRIVEN FUEL PUMP, THE FUEL PUMP WAS R & R WITH AN O/H UNIT AND THE SDR CA130824002Pump · warning light(CAN) AFTER T/O, PILOT NOTICED NR 1 FUEL AUX PUMP ADVISORY LIGHT HAD REMAINED ON. ALSO NOTICED NR 1 FUEL TANK QUANTITY 200 LBS LOWER THAN NR 2. BOTH WERE ABOUT EVEN DURING TAXI. FUEL QUANTITY INDICATORS SELF TEST NORMAL. FUEL FLOW INDICATORS INDICATED EQUASDR SWAA2013062017449Pump · malfunctionedUPON INITIATING DESCENT NR 2 ENGINE COMPRESSOR STALLED. R & R MAIN ENGINE FUEL CONTROL & FUEL PUMP IAW M/M.SDR ASAA2013061595146Pump · leakingNR 2 ENGINE FUEL PUMP PAD DRAIN LEAKING FUEL, 45 DROPS IAW MIN. ACFT GROUNDED. REMOVED FUEL PUMP PACKAGE. INSTALLED HMU ONTO PUMP IAW MM 73-21-10-400-801-F00, ITEM 1. INSTALLED FUEL INLET TUBE ONTO PUMP PACKAGE MM 73-11-01-400-801-F00, ITEM H2 (A)-(C) INSTASDR 2013FA0000347Pump · failedLEVEL CRUISE ENROUTE AT 25K FEET WHEN THE LT ENGINE LOST POWER. LT FUEL FLOW DROPPED TO ZERO. PILOT FEATHERED LT PROP AND FOLLOWED EMERGENCY PROCEDURES. ATTEMPTS TO RELIGHT FAILED. DIVERTED. MX PERSONNEL REPORTED THAT THE LT ENGINE FUEL PUMP SHAFT FAILED.SDR PCPR2013061301Pump · leakingDURING UNSCHEDULED MX, FOUND ENGINE DRIVEN FUEL PUMP LEAKING AT RELIEF VALVE GASKET. ENGINE COMPARTMENT COVERED WITH FUEL RESIDUE.SDR AWHA20130530001Drive Shaft · detachedDURING ROUTINE FUEL PUMP GARLOC SEAL REPLACEMENT FOR LEAKAGE, THE MECHANIC INSPECTED THE FUEL PUMP DRIVE GEAR AND IT BECAME DECOUPLED FROM THE FUEL PUMP. THIS IS NOT NORMAL FOR THIS MODEL PUMP. THE ACCESSORY DRIVE GEAR IS HOLLOW AND HAD THE FUEL PUMP DRIVE MSDR UALA2013052103508Pump · leakingLEFT ENGINE DRIPPING FUEL AT A RATE OF 24 DROPS PER MINUTE. PERFORMED LEAK CHECK AND FOUND DRAIN NR 3 LEAKING FUEL AT A RATE OF 24 DROPS A MINUTE. ITEM CARRIED FORWARD IAW AMM 71-71-00, PAGE 604, REF: NOTE 4, FOR 50 HRS. FOUND FUEL LEAKING FROM FUEL PUMP DRSDR JJBA20130519017Pump · malfunctionedCREW REPORTED THAT THE NR 1 ENGINE LOST POWER AT CRUISE AND THEN STARTED SURGING. MX REPLACED THE NR 1 ENGINE MFC AND HP FUEL PUMP.SDR UALA2013050603128Pump · leakingFUEL LEAKING FROM RT ENGINE. EVIDENCE OF FUEL LEAK FROM NR 5 FUEL PUMP DRAIN. APPROXIMATELY 16 DROPS PER MINUTE, NO LEAKS AFTER ENGINE SHUTDOWN. REPLACED NR 2 ENGINE FUEL PUMP PER MM. LEAK AND ENGINE RUN CHECKED GOOD.SDR SWAA2013041214759Pump · faultyDIVERSION -- NR 2 ENG N1 FLUCUATES +/- 3.5 TO 4.0% NR 1 ENG VIB. CLIMBS TO 3 - 5 ALONG WITH THE N1 CHANGES. N1 AND VIB. WILL STABILIZE FOR PERIODS OF 5 TO 10 MINUTES BEFORE IT BEGINS THE CHANGES AGAIN. REMOVED AND REPLACED NR 1 ENG FUEL PUMP AND MAIN FWD CSDR ASAA2013040794385Pump · failedON ENGINE START NO LIGHT OFF, REACHED 52 N2 THEN ROLLED BACK. RAN QRC/QRH PROCEDURE. ATTEMPTED SECOND START GOT LIGHT OFF, FUEL FLOW WAS VERY ERRATIC, AND ENGINE ROLLED BACK AGAIN, ABORTED START. ACFT GROUNDED. INSPECTION OF 5TH STAGE CHECK VALVE IS GOOD PER MSDR UALA2013040802318Pump · faultyREPLACE FUEL PUMP. REPLACED NR 1 ENGINE FUEL PUMP PER AMM, OPS AND LEAK CHECKED OKAY.SDR 2013FA0000184Pump · failedELECTRIC FUEL PUMP FAILURE.SDR CA130321007Pump · leaking(CAN) DURING SCHEDULED MAINTENANCE, AME NOTICED THAT THERE WAS FUEL LEAKING FROM THE BODY OF THE LOW PRESSURE FUEL PUMP. THE PUMP WAS REMOVED, SERVICEABLE PUMP WAS INSTALLED AND ACFT GROUND RUN SERVICEABLE.SDR HYIA20130320001Pump · malfunctionedFLIGHT CREW REPORTED THAT PRIOR TO TAKEOFF ALL INDICATIONS WERE NORMAL. SHORTLY AFTER TAKEOFF WHILE CLIMBING, THE CREW REPORTED THAT THE RT ENGINE SURGED AND THEN BEGAN TO LOSE POWER, AT WHICH POINT THE CREW NOTICED A SPIKE IN FUEL FLOW (295 PPH). CREW SHUTOFSDR A6WA201303144014Pump · malfunctionedDURING CLIMBOUT, LOSS OF POWER ON LEFT ENGINE (LOW FUEL LOW PRESS MESSAGE) N2 DROP 15% WITH VIBRATION AND YAW TO LEFT (LT MAIN EJECTOR) MESSAGE, POWER UP, LOSS OF POWER 3X. SMOOTHED OUT (LOW FUEL, LOW PRESS ON LANDING). REMOVED AND REPLACED LEFT ENGINE FUEL SDR 2013FA0000183Pump · defectiveENGINE WILL NOT PERFORM PROPERLY DURING ENGINE START AND IDLE OPERATION. INSTALLED (4 DEFECTIVE NEW ENGINE DRIVEN FUEL PUMPS (PN 200F-5006) BY THE DIRECTION OF FIELD TECH. FINALLY RECEIVED MFG APPROVAL TO INSTALL A DIFFERENT MFR ENGINE DRIVEN FUEL PUMP O/H PNSDR CA130228003Pump · cavitates(CAN) DURING THE GROUND RUN FOLLOWING THE 50/100 HR INSPECTION THE AUXILIARY FUEL PUMP WAS FOUND TO BE CAVITATING. AUXILIARY FUEL PUMP REMOVED AND AUXILIARY FUEL PUMP, PN: D8187-B, TSO 1123 HRS WAS INSTALLED. SECOND AUXILIARY FUEL PUMP WAS FOUND TO BE INOPERSDR MT9A201302180001Pump · corrodedFOUND THE ENGINE DRIVEN FUEL PUMP DRIVE SPLINE HAD CORRODED. AIRFRAME FUEL SYS SHOWED NO SIGNS OF CONTAMINATION. FUEL PUMP OUTLET FILTER WAS CONTAMINATED & CHANGED, FUEL SYS PURGED AND FUEL NOZZLES CHANGED OUT. HC
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