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Page Title: PORTABLE DEFUEL PUMPS
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GRAVITY (OVERWING) FUELING NOZZLE
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Aviation Boatswains Mate F - Aviation theories and other practices
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CONTINUITY

Figure 5-16.—Gravity fueling nozzle. smaller   valve,   and   the   nozzle   is   then   completely closed. Never block the gravity fueling nozzle in an open position. Ratcheted handles that allow the operator to lock  the  handle  in  the  open  position  are  prohibited. The  nozzle  must  always  be  controlled  by  hand,  so that the flow of  fuel  may  be  instantly  stopped  when necessary. A strainer or screen installed in the nozzle provides a last means of stopping any  dirt or foreign matter  from  entering  the  aircraft  fuel  tanks.  This strainer should never be left out of the nozzle if it is to be used for fueling aircraft. DEFUEL PUMP The defuel pump used in Cla-Val fueling stations is  the  Blackmer  rotary  vane,  positive  displacement pump.  It  is  described  in  detail  in  chapter  4  of  this manual. Flight and hangar deck station defuel pumps are normally    set    to    pump    100    gpm    at    15    psi. PORTABLE DEFUEL PUMPS The portable defueling pumps are either an air- motor-driven internal gear pump or  an  air  twin-dia- phragm pump mounted on a mobile cart. Both pumps are operated off the ship’s low-pressure air system. Three hoses are used with the defueling unit: an air hose, which has a 1/2- or 3/4-inch inside diameter, and  two  defueling  hoses,  which  have  1  1/2  or  2  1/2- inch inside diameter. One defueling hose is used as a suction  hose.  It  should  be  as  long  as  necessary  to reach  from  the  aircraft  to  the  defueling  unit.  The longer the  hose,  the  less  effective  the  defueling  unit is. The other defueling hose is used for the defueling unit discharge hose. The length of this hose has little effect  on  the  defueling  unit  operation  as  long  as  it does not become kinked. The  defueling  suction  hose  is  connected  to  the aircraft in several different ways. For jet aircraft hav- ing single-point fueling/defueling capability, the hose is   connected   to   the   aircraft   through   a   pressure fueling   nozzle.   For   aircraft   drop   tanks,   the   hose without a fitting is inserted into the tank fill opening or pushed up over a drain fitting on the bottom of the tank.  When  defueling  drop  tanks  only,  the  method normally used 5-15

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