Term
| What is the total fuel capacity? |
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Definition
- 6,238lbs with one recognition light
- 6,198lbs with two recognition lights |
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Term
| How many fuel jet pumps are there and where are they located? |
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Definition
| 4 - one in each tip tank and one in each wing |
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Term
| If and engine is shutdown during flight can you use all the tip tank fuel assuming that the respective tank was full at shutdown? |
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Definition
| No. approximately 600lbs, or half, will not be usable |
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Term
| If a jet pump failed during flight would there be sufficient fuel supply to the engine without using the standby pump? |
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Definition
| Theoretically, the engines will suction feed at 25,000' and below |
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Term
| What occurs when the XFER-FILL switch is moved to FILL? |
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Definition
1. Transfer valve opens
2. Crossflow valve opens
3. Standby pumps are energized
4. Transfer pump is disabled |
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Term
| What occurs when the XFER-FILL switch is in FILL and the fuselage tank becomes full? |
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Definition
1. Transfer valve closes
2. Crossflow valve closes
3. Standby pumps are deenergized
4. Green full light illuminates |
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Term
| What occurs when the XFER-FILL switch is moved to XFER? |
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Definition
1.Transfer valve opens
2. Crossflow valve opens
3. Standby pumps are deenergized
4. Transfer pump is energized |
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Term
| When selecting transfer with the fuselage tank full, what does the white light on the fuel panel indicate? |
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Definition
| Insufficient pressure (2.75psi) in the line, possibly failure of the transfer pump, faulty pressure switch (xfer line) or even a faulty wing fuel pressure switch. |
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Term
| What do the jet pump switches control? |
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Definition
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Term
| When does the low fuel light illuminate? |
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Definition
| When either wing or float switches reach 400-500 lbs. |
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Term
| What does a fuel filter light indicate? |
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Definition
| Light illuminates at 1.25 delta, one or both the airframe fuel filters are bypassed at 2.25 delta. Light is actually impending a bypass situation |
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Term
| What fuel tanks are vented directly by the fuel vent system? |
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Definition
| The fuselage and the tip tanks |
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Term
| What are the limitations with regard to the utilization of 100LL? |
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Definition
1. Maximum 500 gallons per 100 hours of operation per engine.
2. Minimum fuel temperature of -54 degrees C.
3. Both jet pumps must be on and operating
4. Flight is limited to 15,000' |
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Term
| What differential is allowed between tanks while fueling? |
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Definition
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Term
| What are the requirements for using anti-icing fuel additive? |
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Definition
20 fluid ounces per 105-206 gallons, MIL-I-27686 (Hi-Flo Prist 20, Quell 20, D-Ice 20) also a biocide
20 fluid ounces per 105-155 gallons, MIL-I-85470 (Hi Flash Prist, D-Ice Flash 190) not a biocide |
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Term
| Wing and Wingtip fuel capacity? |
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Definition
4898 lbs total:
>L tip tank = 1215
>R tip tank = 1175
>L and R main wing tanks each 1245 lbs |
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