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8 Cards in this Set

  • Front
  • Back

Fuel tanks

- No 1 (left wing)


- No 2 (right wing)


- CTR


Fuel available to engines from all 3



- center tank pumps fuel at higher pressure, fuel consumed first (w/ pumps ON)


- center pumps must be ON if > 1000lbs


- CONFIG alert if > 1600lbs and pumps off w/ either engine running


- main tanks must be full if CTR tank contains more than 453 kgs

ENG VALVE & SPAR VALVE lights

SPAR VALVE - upline before 1st stage fuel pump


ENG VALVE- downline after FMU



- allow fuel to flow to engine when both valves open



DIM blue = valve closed


Ext = valve open


Bright blue = valve in transit or disagree



- both closed when engine start lever moved to CUTOFF or ENGINE FIRE switch pulled


- open when start lever to idle (+ eng fire switch in)

Crossfeed selector

- DC battery bus pwrd


- allows L & R engine fuel manifolds to interconnect



VALVE OPEN light stays illum bright blue =


Crossfeed selector inop

Fuel pumps

- 2 in ea tank


- AC pwrd


- fuel passing through cools and lubricates

LOW PRESSURE illum

Center tank


= output press low AND switch ON


- pump will auto shutoff after delay



Main tank


= output press low OR switch is off


- engine can draw fuel from corresponding main tank through suction feed line if both pumps fail


- however dissolved air from fuel may restrict FF at higher altitudes

Fuel temp

- gauge AC pwrd



* maintain 5F/3C above fuel freeze pt OR -45F/-43C, the higher (prior to TO & in flight)


- may req alt change, speed inc, deviation to warmer air mass

Max fuel imbalance

Between main wings tanks (all phases)



= 453kg

To balance fuel

Cnt tank pump switches (if tank fuel) ... OFF


Crossfeed selector ... OPEN


- verify VALVE OPEN bright then dim


Fuel pump switches (low tank) ... OFF



When quantity balanced:


Fuel pump switches ... ON


Cnt tank pump switches ... ON


Crossfeed selector ... close


- verify VALVE OPEN bright then ext