07/18/23
Message Overview:
Message Description:
Refuel/Defuel Control Panel High-Level Test did not give expected results.
Possible Causes:
- Refuel/Defuel Shut-off Valve
- High-Level Sensor
- Fuel Quantity Gauging Computer (FQGC) (A57)
- Refuel/Defuel Control Panel (PL41)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin:
- AW300-28-0269 - Fuel Tank High Level Sensor
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| Pressure Refueling | AMM 12-11-01-650-801 |
| Suction Defueling | AMM 12-11-09-650-801 |
| Removal of the Refuel/Defuel Control Panel | AMM 28-23-01-000-801 |
| Installation of the Refuel/Defuel Control Panel | AMM 28-23-01-400-801 |
| Operational test of the Refuel/Defuel Control Panel | AMM 28-23-01-710-801 |
| Removal of the Refuel/Defuel Manifold | AMM 28-23-09-000-801 |
| Installation of the Refuel/Defuel Manifold | AMM 28-23-09-400-801 |
| Removal of the Refuel/Defuel Shutoff Valve | AMM 28-23-13-000-801 |
| Installation of the Refuel/Defuel Shutoff Valve | AMM 28-23-13-400-801 |
| Removal of the Fuel Quantity Computer | AMM 28-41-01-000-801 |
| Installation of the Fuel Quantity Computer | AMM 28-41-01-400-801 |
| Data Download from the Maintenance Diagnostic Computer (MDC) | AMM 45-45-01-970-802 |
| Wiring - Maintenance Practices - ALL | SPM 20-12-00-02 |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 |
Troubleshooting Recommendations:
- Make sure there are no FUEL QTY FAULT/FAIL EICAS messages. If a fault is found, carry out appropriate troubleshooting.
- Verify MDC CURRENT FAULTS for 'L(R) TNK HI LVL' fault (B3-007142/B3-007864).
- If fault code is present, carry out B3-007142/B3-007864 troubleshooting.
- If fault code is not present, continue with next step.
- Select the active MDC fault or equation from the drop down below prior to following the troubleshooting below.
- If any of the fault codes, listed on that page are present on the aircraft, troubleshoot these fault codes first.
- If none of the fault codes are present, continue with next step.
- Make sure that RDCPC CB6-C5 (REFUEL DEFUEL VALVES) and CB6-C4 (REFUEL DEFUEL CTL) circuit breakers are pushed in.
- On Refuel/Defuel Panel, verify that both H. LEVEL DETECTOR lights are OFF before initiating the High Level Test.
NOTE: Extremely low ambient temperature (below -40°C (-40°F)) can create a false high level indication and prevent refueling.- If one H. LEVEL DETECTOR light is ON and its tank is not full, interchange high level Sensors.
- If problem follows, replace faulty high level sensor.
- If problem does not follow, verify wiring between high level sensor and FQGC.
- If wiring is found serviceable, go to next step.
- If both H. LEVEL DETECTOR lights are ON and their respective tanks are not full, go to next step.
NOTE: A failure of a SOV to OPEN shall not be considered faulty if the corresponding tank was already filled up to the High Level Sensor at initiation of the test.
- If one H. LEVEL DETECTOR light is ON and its tank is not full, interchange high level Sensors.
- Re-rack the Fuel Quantity Gauging Computer (FQGC). Is the fault message still present?
- If YES, go to next step.
- If NO, do close out.
- Replace the Fuel Quantity Gauging Computer (FQGC).
- Carry out the High Level Test as follow:
- Connect the fuel nozzle from the fuel tender to the refuel/defuel adapter
- Pressurize the fueling hose between 30 and 50 psi (206.84 and 345.74 kPa).
- Set the Refuel/Defuel control panel power switch to ON.
- Wait 10 seconds.
- Carry out lamp test.
- Set the fuel selector knob to TEST.
- On the Refuel/Defuel control panel, make sure that:
- SOV indication CL lights go off
- SOV indication OP lights come on
- L/R H. LEVEL DETECTORS lights come on
- SOV indication OP lights go off
- SOV indication CL lights come on.
- After approximately 20 seconds, make sure that:
- L/R H. LEVEL DETECTORS lights go off
- SOV indication CL lights stay on.
- If the test is not instigated or the H. LEVEL DETECTORS lights do not come on, do the following:
- Remove R/D Panel from the aircraft.
- Set the R/D Panel to the following configuration:
POWER SWITCH ON ROTARY SELECTOR TEST - On the R/D Panel back connector, check for continuity between pins 36 and 3 while tapping on the rotary selector.
- If there is no continuity, replace R/D Panel.
- If there is continuity, go to next step.
- Verify wiring between FQGC per the following table.
FROM TO A57BP1 (FQGC) pin 28 PL41P1 (R/D Panel) pin 36 - If wiring is found serviceable, replace FQGC.
- During test, if both SOV do not close, replace FQGC.
- During test, if one SOV does not close, replace the applicable SOV.
- During the test, if one SOV does not open, do the following:
- Verify that the fueling hose was pressurized to 50 psi at step 5. If not, pressurize the fueling hose to 50 psi and carry out step 5 again.
- If raising the pressure to 50 psi opens the faulty valve, consider replacing the valve.
- Access Refuel/Defuel SOV through access panel 181BL.
- Have a person close to the SOV that will listen for a solenoid clicking.
- Set the Refuel/Defuel control panel power switch to ON.
- Pressurize the fueling hose between 30 and 50 psi (206.84 and 345.74 kPa).
- Set the fuel selector knob to FUEL MAN.
- Set the SOV toggle switch of the SOV that did not open to ON.
- If the SOV solenoid was heard clicking but the 'open' indication light on the R/D Panel does not illuminate, replace SOV.
- If the SOV solenoid did not click, go to next step.
- Disconnect the fueling hose from the aircraft.
- Set the Refuel/Defuel control panel power switch to ON.
- Set the fuel selector knob to DEFUEL.
- Set the SOV toggle switch of the SOV that did not open to ON.
- If the SOV solenoid did not click, replace SOV.
- If the SOV solenoid was heard clicking, verify wiring as per the following table:
LH R/D SOV RH R/D SOV A57BP1 A59P2 A57BP1 A59P1 PIN 20 PIN 3 PIN 18 PIN 3 - If wiring is found serviceable, replace FQGC.
- Verify that the fueling hose was pressurized to 50 psi at step 5. If not, pressurize the fueling hose to 50 psi and carry out step 5 again.
- During test, if neither SOV opened, replace FQGC.
- Do close out.