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Fabrication and Testing
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Fluid Power - Intro to Hydraulics, Pneumatics, and how it all works
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Installation

3. be designed to give adequate performance and service  for  infrequent  transient  pressure  peaks up to 150 percent of the working pressure of the  hose,  and 4.  have  a  safety  factor  with  a  burst  pressure  at a  minimum  of  4  times  the  rated  working pressure. There are temperature restrictions applied to the use of hoses. Rubber hose must not be used where the operating temperature exceeds 200°F. PTFE hoses in high-pressure air systems must not be  used  where  the  temperature  exceeds  350°F. PTFE hoses in water and steam drain applications must not be used where the operating temperature exceeds  380°F. FABRICATION  AND  TESTING The fabrication of flexible hose assemblies is covered in applicable training manuals, technical publications,   and   NAVAIR   01-1A-20.   After   a hose assembly has been completely fabricated it must  be  cleaned,  visually  inspected  for  foreign materials,  and  proof  tested. A   hose   assembly   is   proof   tested   by   the application  of  a  nondestructive  pressure  for  a minimum  of  1  minute  but  not  longer  than  5 minutes to ensure that it will withstand normal working  pressures.  The  test  pressure,  known  as normal proof pressure, is twice the rated working pressure.  While  the  test  pressure  is  being  applied, the  hose  must  not  burst,  leak,  or  show  signs of  fitting  separation.  NAVAIR  01-1A-20  and NAVSEA S6430-AE-TED-010, volume 1, provide detailed  instructions  on  cleaning  of  hoses,  cleaning and test media, proof pressure and proof testing. After  proof  testing  is  completed,  the  hose  must be  flushed  and  dried  and  the  ends  capped  or plugged to keep dirt and other contaminants out of  the  hose. IDENTIFICATION The final step after fabrication and satisfac- tory testing of a hose assembly is the attachment of identification tags as shown in figure 5-11 (for ships)  and  in  figure  5-12  (for  aircraft).  The  tag shown  in  figure  5-12,  view  B,  is  used  in  areas where a tag maybe drawn into an engine intake. Hose assemblies to be installed in aircraft fuel and oil  tanks  are  marked  with  an  approved  electric engraver  on  the  socket-wrench  flats  with  the required   information. Figure 5-11.—Hose assembly identification tags (ships). 5-10

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