JASC 7324

Service difficulty reports · 74

Reports filed under 7324 · Fuel Divider, newest first.

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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 = '7324'
  ORDER BY difficulty_date DESC"

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SDR 2023FA0000241Fuel Divider · inoperativePILOT COMPLETED A SATISFACTORY ENGINE RUN. CLIMBING OUT, ENGINE STARTS TO RUN ROUGH. PILOT NOTICES FUEL DROPLETS ON WINDSCREEN. ENGINE QUITS WHILE THROTTLE IS FULL POWER AND MIXTURE IS FULL RICH. PILOT CIRCLES BACK, DECLARES EMERGENCY AND SAFELY LANDS AIRCRAFTMay 1, 2023 · N163CD · Cirrus SR20SDR Q5QA20230303004O-Ring · brokenDURING A FUEL NOZZLE AND FLOW DIVIDER CHANGE IT WAS NOTED THAT A O-RING WAS FOUND TO BE BROKEN. THIS O-RING WAS FOUND BROKEN PRIOR TO INSTALLATION ON THE FLOW DIVIDER POSITION. THE O-RING WAS SUPPLIED WITH A FUEL NOZZLE KIT FROM HERITAGE TURBINES, INC. P/N AS-Mar 3, 2023 · Pilats PC1245SDR Q5QA20230222002O-Ring · brokenFUEL INLET ADAPTOR ASSEMBLY WAS REPLACED ON THE ENGINE. SUBSEQUENT ENGINE RUN-UP AND LEAK CHECK WAS SATISFACTORY. HOWEVER, A FUEL LEAK WAS NOTED THE FOLLOWING DAY UNDER THE FUEL FLOW DIVIDER. INSPECTION DISCLOSED THAT ONE OF THE O-RINGS USED TO INSTALL THE Feb 27, 2023 · N26VW · Pilats PC1245SDR HALA2022071400130Wire Harness · failedETOPS - ENG 2 FADEC SYS FAULT ALERT IN CRUISE. REMOVED AND REPLACED WO3 EEC WIRING HARNESS PER AMM 73-21-63. OPS CHECK GOOD. OK FOR SERVICEJul 14, 2022 · N226HA · Airbus A321271NSDR HALA2022071400129Probe · failedATB ENG L FADEC ALTN DISPLAYED. FAULTING 732116 P20/T20 PROBE. REMOVED AND REPLACED P20/T20 PROBE PER FIM 73-21 TASK 816. RTS TEST FPR P20/T20 PROBE FAILED. AS 17605 7/13/22. REQUIRES FURTHER T/S. PERFORMED WIRING CK REF FIM 7321 TASK 816 STEP F ALL WIRES CK Jul 14, 2022 · N483HA · Boeing 717200SDR 8LFA2021081900237Flow Divider · looseWE HAD JUST COMPLETING OEI TRAINING WITH THE TRAINING MODE ON THE NUMBER ONE ENGINE. AFTER COMPLETING OUR OEI TRAINING, ROGER PLACED THE TRAINING MODE BACK TO CENTER POSITION AND ALL INDICATIONS ON THE NUMBER ONE ENGINE WERE NORMAL. I PLACE THE RPM SWITCH BACAug 17, 2021 · N901LF · Agusta AW109SPSDR CA190822001Flow Divider · malfunctioned(CAN) THE CUSTOMER REPORTED THAT THE CREW ABORTED THE TAKE-OFF TWICE BECAUSE THE AUTO FEATHER UNIT FAILED TO FUNCTION. GROUND RUNS CONFIRMED THAT #2 ENGINE DID NOT INCREASE ABOVE 50% TORQUE. THE FMU, WF TRANSMITTER AND FMV WERE REPLACED AND THE AIRCRAFT HAS REAug 4, 2019 · Bombdr DHC8402SDR CA190731015Flow Divider · malfunctioned(CAN) REJECTED TAKEOFF DUE TO #1 ENGINE NOT GOING TO FULL POWER (MAX 50%). CREW RETURNED TO THE GATE DEPLANED PASSENGERS. RDC NP LDG SWITCH RESET AND AIRCRAFT POWER DOWN/POWER UP COMPLETED. ANOTHER RUN SAME RESULT. MAINTENANCE REPLACED THE #1 FLOW DIVIDER , ENJul 29, 2019 · Bombdr DHC8400SDR CA190726004Flow Divider · malfunctioned(CAN) THE PILOT ABORTED THE TAKE-OFF DUE TO RIGHT HAND ENGINE UNABLE TO ACHIEVE TAKE OFF POWER. THE ENGINE STAGNATES AT 40% TORQUE WITH POWER LEVER ANGLE (PLA) AT TAKE-OFF POWER. (TC# 20190726004)Jul 11, 2019SDR CA190628012Flow Divider · malfunctioned(CAN) PILOT REPORT REJECTED T.O. COULD ONLY ACHIEVE 49% TORQUE. ENGINE DID NOT ACHIEVE THE REQUIRED TORQUE CREW DID NOT BEGAN THE TAKE OFF ROLL. MAINTENANCE REPLACE THE FMU BUT HAD THE SAME PROBLEM LATER THE SAME DAY. FLOW DIVIDER WAS REPLACED. (TC# 20190628Jun 21, 2019 · Bombdr DHC8400SDR YN8R201809260001Attach Bracket · brokenFUEL INJECTION SPIDER BRACKET, P/N 07A22996, WAS FOUND BROKEN DURING ANNUAL INSPECTION. IT BROKE AT THE 90 DEGREE BEND IN THE METAL. AD2015-19-07 CALLS FOR THE FUEL INJECTION LINES AND CLAMPS TO BE INSPECTED IAW MSB342G. THIS WAS FOUND BROKEN 100 HOURS SINCSep 26, 2018 · N2290A · Cessna 172SSDR 7C7A2018071600453Flow Divider · unknownCOCKPIT AND CABIN SMELLED LIKE FUEL AFTER STARTING ENGINE NR 2. REMOVED AND REPLACED NR 2 ENGINE FUEL FLOW DIVIDER OPS AND LEAK CHECK GOOD.Jul 13, 2018 · N893E · Dhav DHC8106SDR AALA201608179003Valve · faultedFLIGHT CREW REPORTED AN ENGINE 1 FUEL HEAT SYSTEM FUEL RETURN VALVE OPEN FAULT MESSAGE. THE AIRCRAFT WAS GROUNDED. REPLACED THE 1ENGINE FUEL DIVERTER AND RETURN VALVE IAW AMM 73-13-42-400-010-A AND ACCOMPLISHED A SATISFACTORY LEAK & OPS CHECK.Aug 16, 2016 · N542UW · Airbus A321231SDR MK9A20151208001Flow Divider · leakingDEPARTING ON IFR FLIGHT PLAN, ACFT HAD PARTIAL POWER LOSS AT AROUND 3000’ ON 120 HEADING. THE ACFT RETURNED & LANDED WITHOUT INCIDENT. UPON TROUBLESHOOTING & INVESTIGATING THE CAUSE OF THE POWER LOSS, A FUEL LEAK WAS DISCOVERED AT THE FUEL FLOW DIVIDER & A FDec 8, 2015 · N852MA · Cessna 208BSDR CA151130007Flow Divider · defective(CAN) THE ENGINE HAD AN UNCOMMANDED FLAMEOUT ON APPROACH AT AROUND 2000 FT. ACFT LANDED UNEVENTFULLY. AFTER TROUBLESHOOTING, IT WAS DECIDED TO REPLACE THE FUEL FLOW DIVIDER.Nov 14, 2015 · Cessna 560CESSNASDR JIKA2013121601Fuel Divider · defectiveDURING CLIMB OUT FROM SFO, RT ENG LOST POWER AT APPROXIMATELY 100 FT AGL. BOTH RT SIDE ANNUNCIATOR’S ENG OIL PRESS & LOW FUEL PRESS WERE ILLUMINATED. ENG TORQUE WAS FLUCTUATING BETWEEN 0 & 500 FT LB. PILOT PULLED THE RT ENG CONDITION LEVER TO CUTOUT & DECLADec 16, 2013 · N347AF · Beech 1900CSDR FINL2012101700001Valve · contaminatedDURING TROUBLESHOOTING FOR A ROUGH RUNNING ENGINE, A SMALL PIECE OF METAL WAS DISCOVERED ON THE VALVE OF THE FUEL DIVIDER.Oct 15, 2012 · Robsin R44SDR 9JLA2012101804297Flow Divider · defectiveCREW REPORTED FUEL DRIPS FROM THE NR 2 ENGINE CASE DRAIN AT SHUTDOWN. TROUBLESHOOTING IDENTIFIED THE NR 2 ENGINE FLOW DIVIDER, PN 814900-6, SN F55971, AS DEFECTIVE. AN O/H FLOW DIVIDER WAS INSTALLED, LEAK/OPS CHECKS SATISFACTORY IAW MM 73-10-03.Sep 25, 2012 · N100WT · Cessna 550SDR QMLA2012082512138Valve · leakingDURING CRUISE FLIGHT AT 1,000 FT AGL, PILOT NOTICED AN ODOR OF FUEL IN COCKPIT. COULD SEE A CLEAR LIQUID RUNNING DOWN THE REAR CLAM SHELL DOOR. TURNED BACK TO THE AIRPORT AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION FOUND THE ADJUSTED FUEL VALVE ASSAug 25, 2012 · N135TG · Urocop EC135T2SDR 9JLA2012101904286Flow Divider · leakingCREW REPORTED FUEL LEAKING FROM LT ENGINE DRAIN MAST AFTER SHUTDOWN. GAINED ACCESS AND REPLACED THE FLOW DIVIDER VALVE. FUNCTIONAL CHECKS SATISFACTORY. REF: MM 73-10-03.Aug 8, 2012 · N100WT · Cessna 550SDR USAA2012022400003Valve · faultyFLIGHT ATTENDANTS IN MID AND AFT CABIN AS WELL AS PASSENGERS SMELLED RAW GAS ODOR / FUMES JUST AFTER ENGINE SHUT DOWN AT GATE. ALL DOORS WERE CLOSED - APU AND PACKS WERE ON. MAINTENANCE FOUND NR 2 ENGINE FUEL FLOW DIVIDER VALVE BAD. REPLACED VALVE IAW AIRBUFeb 23, 2012 · N543UW · Airbus A321231SDR CA120213010Fuel Divider · malfunctioned(CAN) DURING REVENUE FLIGHT, CREW RECEIVED POWERPLANT MESSAGE, TORQUE DROPPED TO 0 PERCENT, MOP FLUCTUATED AND FELL TO ZERO, MASTER CAUTION ILLUMINATED. CREW SECURED ENGINE, AND RETURNED TO DEPARTURE WHERE UNEVENTFUL SINGLE ENGINE LANDING WAS CARRIED OUT. FUFeb 2, 2012 · Bombdr DHC8400SDR CA110601011Cover · crackedON SCHEDULED INSPECTION, THE FLOW DIVIDER COVER PLATE WITH THE 4 COUNTERSUNK SCREWS HOLDING IT DOWN WAS FOUND TO HAVE MULTIPLE CRACKS FROM 3 OUT OF THE 4 BOLT HOLES ON BOTH SIDES.Jun 1, 2011 · Cessna 172RSDR MASA2011042502495Flow Divider · leakingFUEL DRIPPING FROM GANG DRAIN AT NR 2 ENGINE. R2 FLOW DIVIDER.Apr 23, 2011 · N436YV · Dhav DHC8202SDR CA110124004Housing · damaged(CAN) FLOW DIVIDER LEAKING AFTER 417.2 HOURS TSO. EXTERNAL VISUAL INSPECTION DAMAGE TO CHAMFER AND THREADS ON INLET PORT. FAILED EXTERNAL LEAKAGE TEST. FOUND THE LEAKAGE IS ATTRIBUTED TO THE DAMAGE ON THE CHAMFER AND THREADS OF THE INLET PORT. WORK PERFORMEDJan 3, 2011 · Dhav DHC8102SDR CA100928002O-Ring · damagedFLAMEOUT DURING CRUISE, THE NR 2 ENGINE FLAMED OUT WITH NO PRIOR WARNING. AN EMERGENCY SINGLE ENGINE LANDING WAS MADE. TROUBLESHOOTING REVEALED A FUEL LEAK FROM A DAMAGED O-RING ON THE FUEL LINE BETWEEN THE AUTOMATIC FUEL CONTROL AND THE FLOW DIVIDER. THE PRSep 14, 2010 · Bell 412EPSDR CA091110006O-Ring · damaged(CAN) ON TAKEOFF ROLL, ON MONDAY, NOVEMBER 9 2009, THERE WAS A PARTIAL LOSS OF PWR ON THE NR1 ENG NOTICED BY THE FLIGHT CREW. THE TAKEOFF WAS ABORTED AND THE ACFT TAXIED BACK TO THE RAMP. FURTHER INVESTIGATION REVEALED THAT THERE WAS A SIGNIFICANT AMOUNT OF FNov 9, 2009SDR CA090209005Fuel Divider · leakingAIRCRAFT RETURNED TO BASE NOTING HIGH FUEL CONSUMPTION ON RT ENGINE. AFTER LANDING LARGE AMOUNT OF FUEL NOTED LEAKING FROM RT NACELLE. FUEL LINE WAS RUPTURED FROM FCU TO START CONTROL. REF SDR 20080513005, 20080211006 AND 20080521010. THIS WAS THE FOURTH LJan 22, 2009 · Beech 100BEECHSDR HNAA0700090Flow Divider · malfunctionedNR 2 ENGINE POWER LOSS MOMENTARILY OF 30 TO 40 PERCENT TQ HAPPENED 3 TIMES ON CLIMBOUT. AIRCRAFT RETURNED TO FIELD AFTER TAKEOFF. LGA MAINTENANCE INSPECTED THE ENGINE CONDITION PANEL. CREW REPORTED THAT ENGINE PARAMETERS ALSO DROPPED WITH TORQUE AND CREW FEMay 21, 2007 · N827EX · Dhav DHC8102SDR 040607Flow Divider · leakingTHE RT ENGINE EXPERIENCED A LOSS OF POWER AND INDICATED A SIGNIFICANT INCREASE IN FUEL FLOW. THE ENGINE WAS SHUTDOWN AND A THE AIRCRAFT LANDED AT THE NEXT AVAILABLE AIRPORT. MAINTENANCE REVEALED THAT THE RETURN TO TANK LINE FROM THE FUEL FLOW DIVIDER WAS LOOSEApr 6, 2007 · N411ET · Gulstm 500BSDR TRBA2007014Flow Divider · defectiveON APPROACH RT ENGINE FLAME OUT, LANDED SUCCESSFULLY. REPLACED RT ENGINE FUEL NOZZLE KIT, AND FUEL FLOW DIVIDER IAW MM 71-01-40. PERFORMED ENGINE RUN-UP AND FOUND SATISFACTORY. (K)Mar 30, 2007 · N447AM · Aerosp ATR72SDR TRBA2007010Flow Divider · leakingWHILE IN CLIMB, NR 2 ENGINE TQ DROPS SLOWLY UP TO 25 PERCENT AND LOST POWER UNTIL THE ENGINE FLAMED OUT BY ITSELF. REPLACED FUEL FLOW DIVIDER IAW MM 72-01-40 AND FUEL NOZZLES 8,9,10,11 AND 12 TRANSFER TUBES AND SEALS IAW 72-01-40. PERFORMED ENGINE RUN UP NO Mar 20, 2007 · N447AM · Aerosp ATR72212SDR MPVMANIFOLDFuel Divider · leakingFUEL MANIFOLD VALVE IS LEAKING FROM THE VENT PORT.Mar 28, 2006 · Cessna TU206GSDR 2006FA0000087Poppet Valve · stickingAIRCRAFT WOULD NOT START. ENGINE & FUEL COLD SOAKED (JUST AT BELOW 32 DEG. F). THE FLOW DIVIDER POPPET VALVE WOULD STICK CLOSED AND PREVENT FUEL FLOW. AFTER TROUBLSHOOTING DETERMINED THAT UNIT WOULD STICK IN CLOSED AND OPEN POS. THE CLOSED POS. PREVENTS FUELJan 20, 2006 · N575TW · Cessna 172SSDR CA050322009Flow Divider · leaking(CAN) DURING GROUND RUN, FUEL WAS OBSERVED TO BE LEAKING FROM THE RT AFT ENGINE AREA. THE PROBLEM WAS FOUND TO BE A LEAKING FUEL FLOW DIVIDER. THE PART WAS REPLACED, A SATISFACTORY GROUND RUN AND LEAK CHECK WAS CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVMar 21, 2005 · Amd FALCON10SDR 2004FA0000289Diaphragm · improperMATERIAL TOO THIN OR TOO SOFT. WHEN TORQUING RETAINING SCREW MATERIAL SQUEEZES OUT WITH NR 5 TORQUE. FUEL FLOW DIVIDER, BENDIX.Mar 1, 2004SDR 2004FA0000059Flow Divider · bypassingFUEL FLOW DIVIDER, TEARDOWN AND TEST OF DIVIDER SHOWED UNIT WAS BY-PASSING FUEL , WHICH INTERRUPTED FLOW OF FUEL TO ENG UNDER HIGH POWER SETTINGS, LEADING TO INTERRUPTION OF ENG POWER AND/OR TOTAL LOSS OF ENG POWER. FURTHER TEAR DOWN, REVEALED DIAPHRAGM WAS SJan 12, 2004 · N4658J · Piper PA28R180SDR 2003FA0000258Flow Divider · stickingDURING CRUISE THE CREW REPORTED A ROUGH ENGINE. AFTER INSPECTING APPLICABLE SYSTEMS, THE FUEL FLOW DIVIDER WAS CHANGED AFTER HAVING BEEN FOUND STICKING INTERNALLY.Feb 10, 2003 · N409ER · Cessna 172SSDR 2003FA0000257Flow Divider · stickingDURING CRUISE THE CREW REPORTED AROUGH ENGINE. AFTER INSPECTING APPLICABLE SYSTEMS, THE FUEL FLOW DIVIDER WAS CHANGED AFTER HAVING BEEN FOUND STICKING INTERNALLY.Feb 10, 2003 · N409ER · Cessna 172SSDR 2003FA0000256Flow Divider · stickingDURING CRUISE THE CREW REPORTED AROUGH ENGINE. AFTER INSPECTING APPLICABLE SYSTEMS, THE FUEL FLOW DIVIDER WAS CHANGED AFTER HAVING BEEN FOUND STICKING INTERNALLY.Feb 10, 2003 · N409ER · Cessna 172SSDR SWIA200211510Flow Divider · malfunctionedON TAKEOFF ROLL BELOW 80 KTS, THE LT ENGINE SHUT DOWN. ABORTED THE TAKEOFF. REMOVED AND REPLACED LT ENGINE FLOW DIVIDER. RAN ENGINE. SYSTEM OPS CHECK AND LEAK CHECK GOOD IAW EMB120 MM 73-14-00 & P&W MM.Nov 18, 2002 · N223SW · Emb EMB120ERSDR AUS20020699Flow Divider · faulty(AUS) ENGINE FUEL SYSTEM FLOW DIVIDER FAULTY. IGNITION LEAD ALSO FOUNDTO BE UNSERVICEABLE. ENGINE WAS UNDERGOING GROUND RUNS FOLLOWINGENGINE INSTALLATION. PERSONNEL/MAINTENANCE ERROR.Jul 11, 2002 · Beech B200CSDR VJ32002F00050Flow Divider · failedAT NORMAL POWER SETTINGS THE ENGINE RAN ROUGH AT 6000 TO 7000 FEET. REMOVED FUEL FLOW MANIFOLD VALVE AND INSTALLED NEW FUEL FLOW MANIFOLD VALVE. GROUND OPERATION OF THE ENGINE CHECKED NORMAL. PART SENT IN FOR WARRANTY.Jun 28, 2002 · N5582X · Beech F33ASDR 2002FA0000771Flow Divider · fluctuatesFUEL FLOW FLUCTUATES IN-FLIGHT AND THE ENGINE WAS ROUGH RUNNING AT ALTITUDE, AT LOW ALTITUDE THE ENGINE WAS SMOOTH IN OPERATION. OPERATION CHECK OF ENGINE ON THE GROUND FOUND THE FUEL FLOW DIVIDER WOULD FLUCTUATE. REMOVED FLOW DIVIDER AND INSTALLED A NEW OVEJun 11, 2002 · N8240T · Beech F33ASDR 2001FA0000505Flow Divider · defectiveENGINE RUN ROUGH AND SOMETIME WOULD NOT SHUT DOWN. THE FUEL FLOW DIVIDER WOULD STICK OPEN, LETTING CONTINUOUS FUEL FLOW TO THE ENGINE. THE FLOW DIVIDER WAS REMOVED AND REPLACED WITH A NEW ONE, OPERATION OF ENGINE CHECKED OUT NORMAL.Oct 29, 2001 · N5582X · Beech F33ASDR VJ32001F00006Flow Divider · sticksENGINE RUN ROUGH AND SOMETIME WOULD NOT SHUT DOWN. THE FUEL FLOW DIVIDER WOULD STICK OPEN LETTING FUEL TOO CONTINUAL TO THE ENGINE. THE FLOW DIVIDER WAS REMOVED AND REPLACED WITH A NEW ONE, OPERATION OF ENGINE CHECKED OUT NORMAL.Oct 29, 2001 · N5582X · Beech F33ASDR AUS20010773Gasket · faulty(AUS) FLOW DIVIDER GASKET FAULTY. NEW ITEM FROM MANUFACTURER.Jul 23, 2001SDR USAABB01066Manifold · leakingPIT - FLT 48 - ON TAKEOFF ROLL IN PIT, THE LEFT ENGINE REACHED 80 PERCENT N1 AND THEN FAILED. THE TAKEOFF WAS ABORTED AT 60 KNOTS. THE FLIGHT RETURNED TO THE GATE, WHERE IT WAS NOTED THAT FUEL WAS LEAKING FROM THE LEFT ENGINE. MAINTENANCE FOUND A FUEL PRESSJul 18, 2001 · N653US · Boeing 7672B7SDR C2XA01CL157Fuel Line · looseCLE FLIGHT 3375 THE CREW REPORTED A FUEL SMELL IN THE CABIN WHILE TAXIING. THE BLEED AIR VALVES WERE ON ALONG WITH THE BLOWERS. MAINTENANCE INSPECTED AND RESECURED THE FUEL LINE ON THE FLOW DIVIDER ON THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD.Jun 27, 2001 · N81553 · Beech 1900DSDR 20010613CW013Flow Divider · stuckENGINE RUN ROUGH AND SOMETIME WOULD NOT SHUT DOWN, THE FUEL FLOW DIVIDER WOULD STICK OPEN, LETTING FUEL TOO CONTINUAL TO THE ENGINE. THE FLOW DIVIDER WAS REMOVED AND REPLACED WITH A NEW ONE, OPERATION OF ENGINE CHECKED OUT NORMAL.May 17, 2001 · N5609S · Beech F33A
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