Term
| Where is the fuel flow transducer located on the aircraft? |
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Definition
| The fuel flow transducer is located on the right side of the engine compartment near the aft firewall. |
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Term
| When is the fuel low warning indicating system activated? |
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Definition
| The fuel low warning system is activated when 45 minutes of fuel remains at the present consumption rate. |
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Term
| The A/F FUEL FILTER caution light illuminates at ___ PSID and bypasses the filter at ___ PSID. |
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Definition
| The A/F FUEL FILTER caution light illuminates at 1 PSID and bypasses the filter at 4.5 PSID. |
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Term
| How many times is the fuel filtered before it is ignited? |
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Definition
| Fuel is filtered four times (A/F fuel filter, engine driven fuel pump, gas producer fuel control, and fuel nozzle) before it is ignited. |
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Term
| A dual boost pump failure is indicated by ____________________________________. |
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Definition
| A dual boost pump failure is indicated by a FUEL PUMP caution light and a fuel pressure drop to zero. |
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Term
| A single boost pump failure is indicated by __________________________. |
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Definition
| A single boost pump failure is indicated by a FUEL PUMP caution light and little or no change in fuel pressure. |
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