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Page Title: CONTINUITY
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PORTABLE DEFUEL PUMPS
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Aviation Boatswains Mate F - Aviation theories and other practices
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SHIPBOARD  AIRCRAFT  REFUELING PROCEDURES

is  to  insert  the  defueling  suction  hose  into  the  tank through  the  tank  fill  opening.  For  total  defueling, defuel through the aircraft pressure fueling adapter. The   discharge   hose   from   the   defueling   unit   is connected  to  the  fill  connection  through  a  special fitting. CONTINUITY Electrical continuity is a firm requirement for all aircraft refueling stations. Electrical continuity must be   present   and   maintained   to   ensure   personnel safety,  equipment  protection,  and  efficient   fueling operations. With electrical continuity present, the nozzleman fueling  the  aircraft  has  immediate  control  of  fuel flow.   This   is   essential   to   prevent   fuel   spills   and possible accidents during aircraft refueling. Electrical continuity  is  present  when  wires  are  provided  and switches are set to allow an electrical current to flow away  from  the  controller  and  back  to  it  through  a solid metallic path. Now, let’s follow the continuity circuit (fig. 5-17). Starting  the  defuel  pump  applies  power  to  the  solid state relay, but nothing happens, because the circuit is broken. Make sure your ground wire to the deck is grounded  to  metal.  Then  hook  it  to   the   aircraft. Remove  the  dust  cover  and  connect  the  nozzle.  Flip the  switch  in  the  quick-disconnect  housing  to  ON, which  closes  the  circuit.  The  ground  then  goes  back through the spiders in the quick-disconnect coupling to  the  wire  in  the  hose.  From  there,  it  goes  back  to the Figure 5-17.—Electrical continuity control for the Cla-Val fueling station. 5-16

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