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Page Title: LOCATION AND DESCRIPTION OF MAJOR COMPONENTS
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TM 10-4930-247-13&P 1-10.  LOCATION AND DESCRIPTION OF MAJOR COMPONENTS - cont. (1) (Model  HTARS100)  Elbows.    Two  elbows  are  supplied  with  the  system  and  are  installed  to  prevent  sharp bends in the fuel hose.  Each elbow is equipped with drylock couplings. (Model  HTARS101)  Elbows.    Two  elbows  are  supplied  with  the  system  and  are  installed  to  prevent  sharp bends in the fuel hose.  Each elbow is equipped with drylock couplings and manually operated ball valves to  control  fuel  flow  through  the  elbow.    Valves  must  be  set  to  CLOSE  position  before  connecting  or disconnecting couplings.  Valves are set to OPEN position during operation. (2) 2-Inch Hose Assemblies.  Ten 2-inch hose assemblies are used to connect components of the HTARS into four  pumping  stations.    Each  hose  is  50  feet  long  with  drylock  couplings  at  both  ends.    Each  coupling  is equipped with a manually operated ball valve to control fuel flow through the hose.  Valves must be set to CLOSE  position  before  connecting  or  disconnecting  couplings.    Valves  are  set  to  OPEN  position  during operation.  The hose assemblies incorporate internal ground wires that are built into the hose material. (3) DELETED. (4) (Model HTARS100) Single  Point  Refueling  Nozzle  (Type  D1).    Four  D1  nozzles  are  supplied  with  HTARS for  refueling  aircraft  with  pressurized  fuel  systems.    The  D1  nozzles  are  non-regulating,  so  fuel  pressure must be controlled by the HEMTT tanker.  The nozzle is internally grounded through the fuel hose.  (Model HTARS101)  Single  Point  Refueling  Nozzle  (Type  D1).    Four  Dl  nozzles  are  supplied  with  HTARS  for refueling aircraft with pressurized fuel systems.  The D1 nozzle incorporates a pressure regulator designed to  limit  maximum  fuel  pressure  to  45  psi.    A  coarse  screen  inside  the  drylock  coupling  prevents  large particles  of  contamination  from  entering  the  aircraft  fuel  system.    The  D1  nozzle  is  internally  grounded through the fuel hose. (5) Ground Rods.  Four ground rods are supplied, one for each refueling point.  The ground rods incorporate a built-in slide hammer to aid installation and removal. (6) Closed Circuit Refueling (CCR) Nozzle.  Four CCR nozzles are supplied with the HTARS.  The CCR nozzle locks  onto  the  aircraft  refueling  adapter  and  regulates  fuel  pressure  to  the  aircraft.    An  automatic  shutoff stops fuel flow when the nozzle is disconnected.  Each nozzle is supplied with a ground clamp and plug for electrical  bonding  of  the  nozzle  to  the  aircraft.    The  CCR  nozzle  can  be  used  to  refuel  aircraft  with  gravity feed  fuel  tanks  by  connecting  the  open  port  nozzle  to  the  fuel  discharge  coupling.    The  CCR  nozzle  is required to connect the recirculation nozzle to the HEMTT tanker. (7) Port Nozzle.  Four open port nozzles  are  supplied  with  the  system  for  refueling  gravity-fill  type  fuel  tanks and containers.  The open port nozzle must be connected to the CCR nozzle for operation. (8) Recirculation   Nozzle.      One   recirculation   nozzle   is   supplied   with   HTARS.      The   recirculation   nozzle   is installed between the fuel system supply points and the HEMTT tanker to allow fuel to re-enter the tanker. The  nozzle  is  equipped  with  a  hand  operated  ball  valve  to  allow  sampling  of  fuel  entering  the  tanker. Operation of the recirculation nozzle requires connection of the CCR nozzle. (9) Tees.  Three tees are supplied with the system.  Each tee is equipped with drylock couplings and manually operated  ball  valves  to  control  fuel  flow  through  the  tee.    Valves  must  be  set  to  CLOSE  position  before connecting or disconnecting couplings.  Valves are set to OPEN position during operation. 1-4  Change 4

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