Fuel Supply System 1-29 Flashcards

1
Q

Usable amount of fuel (single point)?

A

approximately 1100 pounds

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2
Q

Usable amount of fuel (over the wing)?

A

1200 lbs

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3
Q

What is the primary refueling

method?

A

Single point pressure refueling is the primary refueling

method.

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4
Q

How many integral tanks?

A

3

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5
Q

When parking on ramps with greater than_______, the fuel system may vent fuel
overboard through a pressure relief valve.

A

1% slope

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6
Q

The fuel system incorporates an auto balance system to
keep the fuel level in the wing tanks within ________ of
each other.

A

20 pounds

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7
Q

When a fuel imbalance of________ or more is

detected for more than_________, the transfer valve will close the motive flow line to the light tank.

A

20 pounds; 30 seconds

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8
Q

If the fuel imbalance is not
reduced to less than___________ within__________ , the FUEL BAL annunciator will illuminate and the auto balance system will shut off

A

30 lbs; 2 minutes

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9
Q

The FUEL BAL annunciator will remain illuminated until the system is reset.

A

True.

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10
Q

If the auto balance system shuts off without reducing the fuel imbalance to 30 pounds or less, the auto balance system may be reset to
provide an additional 2 minutes to balance
the fuel load.

A

True

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11
Q

The fuel system includes ______ annunciators to indicate fuel system operations

A

6

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12
Q

What are the six fuel system annunciators?

A
red FUEL PX
amber L FUEL LO 
amber R FUEL LO
amber FUEL BAL
green M FUEL BAL
green BOOST PUMP
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13
Q

When will the red FUEL PX annunciator illuminate?

A

less than 10 psi fuel

pressure in the motive flow/return flow supply line.

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14
Q

When will the green BOOST PUMP annunciator illuminate?

A
  1. manually by selecting the BOOST PUMP switch ON,
  2. automatically by the low-pressure switch if the PCL is
    above the IDLE position,
  3. whenever the starter is
    activated regardless of fuel pressure
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15
Q

When will the amber L/R FUEL LO annunciator illuminate?

A

activated by optical sensors and indicate fuel quantity below approximately 110 pounds in the respective wing tank.

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16
Q

When will the amber FUEL BAL illuminate?

A

if indicated fuel imbalance exceeds 30 pounds for 2

minutes or a fuel probe fails.

17
Q

When will the green M FUEL BAL illuminate?

A

if the fuel balance switch is in the MAN/RESET position.

18
Q

When should you not attempt to manually balance fuel load?

A

if alternate engine data display is indicating

FP FAIL. Reading may not be correct.

19
Q

The fuel quantity indicating system uses ______ fuel probes.

A

seven.

three in each wing tank and one in the collector tank.

20
Q

The outer probe provides fuel readings until approximately ______,

A

445±50 pounds

21
Q

The middle probe provides fuel readings until approximately ______,

A

308±50 pounds.

22
Q

The inner probe provides fuel readings until approximately ______,

A

20 pounds since the collector tank only has one probe and divides its capacity equally between the left and right fuel tank readings.

23
Q

If a fuel probe fails, what will illuminate?

A

the amber FUEL BAL annunciator will illuminate and FP FAIL will display in amber text in the lower center portion of the AEDD

24
Q

If the fuel gage does not show an imbalance in the event of an FP FAIL light, what can you conclude?

A

the failed probe is not being used to sense fuel.

25
Automatic fuel balancing will not be available with FP FAIL, and the low fuel warning lights cannot be trusted to provide an accurate indication of minimum fuel level.
False. the low fuel warning | lights will continue to provide an accurate indication of minimum fuel level.
26
Fuel gravity drains from outboard to inboard wing cavities where________ pumps supply fuel to the _______ tank.
transfer jet pumps; collector
27
A _______ valve | in the collector tank supplies fuel to the engine
fuel pickup
28
During inverted flight, a weighted rod in the pickup valve closes off the normal fuel pickup, and opens the inverted flight fuel pickup.
True
29
The weighted rod provides a minimum of _______ of fuel regardless of orientation, and prevents air ingestion into the fuel system.
60 seconds
30
A ________ or ________ in the collector tank feeds fuel to the engine-driven low pressure fuel pump.
primary jet pump ; electric boost pump
31
The _________ supplies fuel to the engine-driven high pressure fuel pump which supplies fuel to the FMU.
low pressure fuel pump
32
The electric boost pump provides fuel for engine start and serves as a backup to the engine-driven low pressure fuel pump.
True
33
If both the electric boost pump and the engine-driven low pressure pump fail, the engine-driven high pressure fuel pump will?
Suction feed sufficient fuel for continued engine operation but will not allow an engine restart
34
With both the electric boost pump and the engine-driven low pressure pump fail you can still perform an engine restart?
False.
35
The fuel supply line to the engine incorporates two manually operated _________ and a________.
shutoff valves; fuel filter
36
One shutoff valve is provided to isolate the fuel system for engine or fuel filter maintenance. What activates the other?
The firewall shutoff handle
37
If the FUEL PX annunciator illuminates and the boost pump activates during inverted flight, do what?
cease inverted maneuvers and notify maintenance after flight.