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Page Title: Figure 2-18. Straight Flow Ball / Valve-Type Coupling
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Aeroquip  Corporation  Series  3700  and  3750  Quick  Thread  Couplings.
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TM-1-1500-204-23-3 General Aircraft Maintenance (Maintenance Practices for Fuel and Oil Systems) Volume 3 Manual
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Table 2-8.   Quick-Disconnect Coupling Inspection Values

TM 1-1500-204-23-3 Figure 2-17.  Full Grip Push/Pull-Type Coupling Figure 2-18.  Straight Flow Ball / Valve-Type Coupling Figure 2-19.  Ball Lock-Type Coupling i. Closed-Circuit   Refueling   Receptacles.      Closed- Circuit Refueling (CCR) is a system of equipment in which a  special  aircraft  fill  port  (receiver)  and  a  special  nozzle mate  to  form  a  vapor-proof  seal.    This  system  prevents vapors   from   escaping   at   the   aircraft   fill   port,   and   so reduces  the  danger  of  ignition  from  static  electricity  or engine heat.  Use of closed-circuit equipment is especially ,desirable   when   aircraft   are   being   serviced   by   the   riot refueling  method.    Hot  refueling  is  used  to  reduce  the ground     time     needed     to     refuel     aircraft,     particularly helicopters used in support of combat operations.  Closed -circuit refueling prevents spills, prevents fuel vapors from escaping  at  the  aircraft  fill  port,  and  prevents  dirt,  water or, and other contaminants from entering the aircraft fuel supply during refueling.  These factors contribute to safe ground operations by reducing fire hazards and contribute to  safe  flight  operations  by  protecting  the  quality  of  the fuel used. (1) Types.          Any     closed     system     of     aircraft refueling  depends  on  two  basic  pieces  of  equipment:  a receiver  that  is  mounted  in  the  aircraft,  and  a  nozzle. These  two  pieces  of  equipment  are  designed  for  each other,   to   mate   or   lock   together   before   fuel   can   flow through   them.      The   Army   has   two   such   equipment systems,  the  CCR  system  that:  is  part  of  the  Forward Area  Refueling  Equipment  (FAIRE)  system  and  the  D-1 pressure system (also called the centerpoint system). (2) Inspection.    The  CC:R  receiver  as  shown  in figure 2-20 is inspected as follows: (a)    Check receiver structural support assembly  for  damage,  corrosion,  and  galling  of  flanges and webs. (b)    Check  retainer  four  condition,  cracks,  or scoring of grooved breakaway tabs.  Replace a retainer if damaged. (c)    Check receiver for condition and corrosion,  floats  for  freedom,  and  fuel  nozzle  receptacle for scoring or damage. (3) Maintenance.        Maintenance    of    the]    CCR receiver    consists    of    inspection    (and    replacement    if necessary) in accordance with the applicable maintenance    manuals.        Scoring    and    nicks     iin    the cylindrical    fuel    nozzle    opening    may    be    repaired    by polishing out damage. Refer to the applicable maintenance manual for polishing procedures. j. Fuel    System    Troubleshooting.        Troubleshooting should   be   accomplished   in   accordance   with   applicable aircraft  maintenance  manuals.    A  typical  troubleshooting chart and a schematic are shown in table 2-9 and figure 2- 21. 2-33

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