# Service difficulty reports: JASC 7324

A list on [JASC 7324](https://openairdocs.org/jasc/7324.md).

Reports filed under 7324 · Fuel Divider, newest first.

Page 1 of 2 · 74 reports

- [SDR 2023FA0000241](https://openairdocs.org/sdr/2023FA0000241.md): Fuel Divider · inoperative · May 1, 2023 · N163CD · Cirrus SR20
  > PILOT 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 AIRCRAFT
- [SDR Q5QA20230303004](https://openairdocs.org/sdr/Q5QA20230303004.md): O-Ring · broken · Mar 3, 2023 · Pilats PC1245
  > DURING 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-
- [SDR Q5QA20230222002](https://openairdocs.org/sdr/Q5QA20230222002.md): O-Ring · broken · Feb 27, 2023 · N26VW · Pilats PC1245
  > FUEL 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
- [SDR HALA2022071400130](https://openairdocs.org/sdr/HALA2022071400130.md): Wire Harness · failed · Jul 14, 2022 · N226HA · Airbus A321271N
  > ETOPS - 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 SERVICE
- [SDR HALA2022071400129](https://openairdocs.org/sdr/HALA2022071400129.md): Probe · failed · Jul 14, 2022 · N483HA · Boeing 717200
  > ATB 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
- [SDR 8LFA2021081900237](https://openairdocs.org/sdr/8LFA2021081900237.md): Flow Divider · loose · Aug 17, 2021 · N901LF · Agusta AW109SP
  > WE 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 BAC
- [SDR CA190822001](https://openairdocs.org/sdr/CA190822001.md): Flow Divider · malfunctioned · Aug 4, 2019 · Bombdr DHC8402
  > (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 RE
- [SDR CA190731015](https://openairdocs.org/sdr/CA190731015.md): Flow Divider · malfunctioned · Jul 29, 2019 · Bombdr DHC8400
  > (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, EN
- [SDR CA190726004](https://openairdocs.org/sdr/CA190726004.md): Flow Divider · malfunctioned · Jul 11, 2019
  > (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)
- [SDR CA190628012](https://openairdocs.org/sdr/CA190628012.md): Flow Divider · malfunctioned · Jun 21, 2019 · Bombdr DHC8400
  > (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# 20190628
- [SDR YN8R201809260001](https://openairdocs.org/sdr/YN8R201809260001.md): Attach Bracket · broken · Sep 26, 2018 · N2290A · Cessna 172S
  > FUEL 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 SINC
- [SDR 7C7A2018071600453](https://openairdocs.org/sdr/7C7A2018071600453.md): Flow Divider · unknown · Jul 13, 2018 · N893E · Dhav DHC8106
  > COCKPIT AND CABIN SMELLED LIKE FUEL AFTER STARTING ENGINE NR 2. REMOVED AND REPLACED NR 2 ENGINE FUEL FLOW DIVIDER OPS AND LEAK CHECK GOOD.
- [SDR AALA201608179003](https://openairdocs.org/sdr/AALA201608179003.md): Valve · faulted · Aug 16, 2016 · N542UW · Airbus A321231
  > FLIGHT 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.
- [SDR MK9A20151208001](https://openairdocs.org/sdr/MK9A20151208001.md): Flow Divider · leaking · Dec 8, 2015 · N852MA · Cessna 208B
  > DEPARTING 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 F
- [SDR CA151130007](https://openairdocs.org/sdr/CA151130007.md): Flow Divider · defective · Nov 14, 2015 · Cessna 560CESSNA
  > (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.
- [SDR JIKA2013121601](https://openairdocs.org/sdr/JIKA2013121601.md): Fuel Divider · defective · Dec 16, 2013 · N347AF · Beech 1900C
  > DURING 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 & DECLA
- [SDR FINL2012101700001](https://openairdocs.org/sdr/FINL2012101700001.md): Valve · contaminated · Oct 15, 2012 · Robsin R44
  > DURING TROUBLESHOOTING FOR A ROUGH RUNNING ENGINE, A SMALL PIECE OF METAL WAS DISCOVERED ON THE VALVE OF THE FUEL DIVIDER.
- [SDR 9JLA2012101804297](https://openairdocs.org/sdr/9JLA2012101804297.md): Flow Divider · defective · Sep 25, 2012 · N100WT · Cessna 550
  > CREW 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.
- [SDR QMLA2012082512138](https://openairdocs.org/sdr/QMLA2012082512138.md): Valve · leaking · Aug 25, 2012 · N135TG · Urocop EC135T2
  > DURING 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 ASS
- [SDR 9JLA2012101904286](https://openairdocs.org/sdr/9JLA2012101904286.md): Flow Divider · leaking · Aug 8, 2012 · N100WT · Cessna 550
  > CREW 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.
- [SDR USAA2012022400003](https://openairdocs.org/sdr/USAA2012022400003.md): Valve · faulty · Feb 23, 2012 · N543UW · Airbus A321231
  > FLIGHT 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 AIRBU
- [SDR CA120213010](https://openairdocs.org/sdr/CA120213010.md): Fuel Divider · malfunctioned · Feb 2, 2012 · Bombdr DHC8400
  > (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. FU
- [SDR CA110601011](https://openairdocs.org/sdr/CA110601011.md): Cover · cracked · Jun 1, 2011 · Cessna 172R
  > ON 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.
- [SDR MASA2011042502495](https://openairdocs.org/sdr/MASA2011042502495.md): Flow Divider · leaking · Apr 23, 2011 · N436YV · Dhav DHC8202
  > FUEL DRIPPING FROM GANG DRAIN AT NR 2 ENGINE. R2 FLOW DIVIDER.
- [SDR CA110124004](https://openairdocs.org/sdr/CA110124004.md): Housing · damaged · Jan 3, 2011 · Dhav DHC8102
  > (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 PERFORMED
- [SDR CA100928002](https://openairdocs.org/sdr/CA100928002.md): O-Ring · damaged · Sep 14, 2010 · Bell 412EP
  > FLAMEOUT 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 PR
- [SDR CA091110006](https://openairdocs.org/sdr/CA091110006.md): O-Ring · damaged · Nov 9, 2009
  > (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 F
- [SDR CA090209005](https://openairdocs.org/sdr/CA090209005.md): Fuel Divider · leaking · Jan 22, 2009 · Beech 100BEECH
  > AIRCRAFT 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 L
- [SDR HNAA0700090](https://openairdocs.org/sdr/HNAA0700090.md): Flow Divider · malfunctioned · May 21, 2007 · N827EX · Dhav DHC8102
  > NR 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 FE
- [SDR 040607](https://openairdocs.org/sdr/040607.md): Flow Divider · leaking · Apr 6, 2007 · N411ET · Gulstm 500B
  > THE 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 LOOSE
- [SDR TRBA2007014](https://openairdocs.org/sdr/TRBA2007014.md): Flow Divider · defective · Mar 30, 2007 · N447AM · Aerosp ATR72
  > ON 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)
- [SDR TRBA2007010](https://openairdocs.org/sdr/TRBA2007010.md): Flow Divider · leaking · Mar 20, 2007 · N447AM · Aerosp ATR72212
  > WHILE 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
- [SDR MPVMANIFOLD](https://openairdocs.org/sdr/MPVMANIFOLD.md): Fuel Divider · leaking · Mar 28, 2006 · Cessna TU206G
  > FUEL MANIFOLD VALVE IS LEAKING FROM THE VENT PORT.
- [SDR 2006FA0000087](https://openairdocs.org/sdr/2006FA0000087.md): Poppet Valve · sticking · Jan 20, 2006 · N575TW · Cessna 172S
  > AIRCRAFT 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 FUEL
- [SDR CA050322009](https://openairdocs.org/sdr/CA050322009.md): Flow Divider · leaking · Mar 21, 2005 · Amd FALCON10
  > (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 SERV
- [SDR 2004FA0000289](https://openairdocs.org/sdr/2004FA0000289.md): Diaphragm · improper · Mar 1, 2004
  > MATERIAL TOO THIN OR TOO SOFT. WHEN TORQUING RETAINING SCREW MATERIAL SQUEEZES OUT WITH NR 5 TORQUE. FUEL FLOW DIVIDER, BENDIX.
- [SDR 2004FA0000059](https://openairdocs.org/sdr/2004FA0000059.md): Flow Divider · bypassing · Jan 12, 2004 · N4658J · Piper PA28R180
  > FUEL 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 S
- [SDR 2003FA0000258](https://openairdocs.org/sdr/2003FA0000258.md): Flow Divider · sticking · Feb 10, 2003 · N409ER · Cessna 172S
  > DURING CRUISE THE CREW REPORTED A ROUGH ENGINE. AFTER INSPECTING APPLICABLE SYSTEMS, THE FUEL FLOW DIVIDER WAS CHANGED AFTER HAVING BEEN FOUND STICKING INTERNALLY.
- [SDR 2003FA0000257](https://openairdocs.org/sdr/2003FA0000257.md): Flow Divider · sticking · Feb 10, 2003 · N409ER · Cessna 172S
  > DURING CRUISE THE CREW REPORTED AROUGH ENGINE. AFTER INSPECTING APPLICABLE SYSTEMS, THE FUEL FLOW DIVIDER WAS CHANGED AFTER HAVING BEEN FOUND STICKING INTERNALLY.
- [SDR 2003FA0000256](https://openairdocs.org/sdr/2003FA0000256.md): Flow Divider · sticking · Feb 10, 2003 · N409ER · Cessna 172S
  > DURING CRUISE THE CREW REPORTED AROUGH ENGINE. AFTER INSPECTING APPLICABLE SYSTEMS, THE FUEL FLOW DIVIDER WAS CHANGED AFTER HAVING BEEN FOUND STICKING INTERNALLY.
- [SDR SWIA200211510](https://openairdocs.org/sdr/SWIA200211510.md): Flow Divider · malfunctioned · Nov 18, 2002 · N223SW · Emb EMB120ER
  > ON 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.
- [SDR AUS20020699](https://openairdocs.org/sdr/AUS20020699.md): Flow Divider · faulty · Jul 11, 2002 · Beech B200C
  > (AUS) ENGINE FUEL SYSTEM FLOW DIVIDER FAULTY. IGNITION LEAD ALSO FOUNDTO BE UNSERVICEABLE. ENGINE WAS UNDERGOING GROUND RUNS FOLLOWINGENGINE INSTALLATION. PERSONNEL/MAINTENANCE ERROR.
- [SDR VJ32002F00050](https://openairdocs.org/sdr/VJ32002F00050.md): Flow Divider · failed · Jun 28, 2002 · N5582X · Beech F33A
  > AT 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.
- [SDR 2002FA0000771](https://openairdocs.org/sdr/2002FA0000771.md): Flow Divider · fluctuates · Jun 11, 2002 · N8240T · Beech F33A
  > FUEL 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 OVE
- [SDR 2001FA0000505](https://openairdocs.org/sdr/2001FA0000505.md): Flow Divider · defective · Oct 29, 2001 · N5582X · Beech F33A
  > ENGINE 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.
- [SDR VJ32001F00006](https://openairdocs.org/sdr/VJ32001F00006.md): Flow Divider · sticks · Oct 29, 2001 · N5582X · Beech F33A
  > ENGINE 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.
- [SDR AUS20010773](https://openairdocs.org/sdr/AUS20010773.md): Gasket · faulty · Jul 23, 2001
  > (AUS) FLOW DIVIDER GASKET FAULTY. NEW ITEM FROM MANUFACTURER.
- [SDR USAABB01066](https://openairdocs.org/sdr/USAABB01066.md): Manifold · leaking · Jul 18, 2001 · N653US · Boeing 7672B7
  > PIT - 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 PRESS
- [SDR C2XA01CL157](https://openairdocs.org/sdr/C2XA01CL157.md): Fuel Line · loose · Jun 27, 2001 · N81553 · Beech 1900D
  > CLE 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.
- [SDR 20010613CW013](https://openairdocs.org/sdr/20010613CW013.md): Flow Divider · stuck · May 17, 2001 · N5609S · Beech F33A
  > ENGINE 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.

Next page: https://openairdocs.org/jasc/7324/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/jasc/7324/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.