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Page Title: LOCATION AND DESCRIPTION OF MAJOR COMPONENTS.
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TM   10-4930-246-13&P 1-8. LOCATION AND     DESCRIPTION OF   MAJOR COMPONETS. Major   components  of  the D-1R   Nozzle   are shown  in figure   1-1.1 4 2 5 7 3 6 Figure    1-1.1   Location    and  Description     of  Major    Components     (D-1R) a. Nozzle    Body. The   nozzle    body   (1)  contains    the  poppet   assembly   and  fuel   strainer. b.     Nozzle  Collar. The  nozzle  collar   (2)  mates with   aircraft   receptacle. The  bumper  on  face of  collar  and the  internal slots  allow   positioning    of  the nozzle   before  poppet  valve   can be  opened, c. Handle  Assembly. The  handle  assembly  (3)  allows  the  poppet  assembly  to  he opened and  closed. d. Swivel   Elbow.     The  swivel  elbow  (4)  rotates with   the  nozzle  engaged allowing    the hose to  be positioned   free  of kinks   or  twists. e. Cover.     A  cover  (5)  is  furnished   to cover  the  nozzle  outlet  when  not  connected to  a system for   servicing. f. Ground  cable.    A  ground  cable  (6)  is  provided  for  grounding   and bonding  the  nozzle  to  the  aircraft   prior   to connection. g. Coupling   Assembly.     The  coupling   assembly (7)  allows  the  nozzle assembly  to  be connected to  and disconnected from  a fuel   service  source. h.     Hose  End  Regulator.     The  hose end regulator   (8)  provides  relatively   constant  pressure of  45 psi.   It  responds to increases in pressure  within   the  aircraft   fuel  manifold   caused by  closure  of  the aircraft's    fuel  tank  level   control valves  to  either   maintain   desired   pressure  or  to  close  to  prevent  an  excessive  "surge"   pressure  from  being   sensed within the aircraft. 1-4 Change     1

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