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Page Title: Option 2: Epoxy and Self-Tapping Screw
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TM  9-2320-356-BD Procedural    Steps: Option   1:   Weld. 1. Locate   leak   and   remove   reservoir   if   necessary. 2. Clean   the   hole(s)   with   sandpaper   or   file. 3. Form-fit   a   piece   of   similar   metal   over   damaged   area. 4. Weld   a   two-pass   bead   around   the   patch   metal. 5. I n s t a l l    r e s e r v o i r. 6. Start   engine   and   check   for   leaks. 7. Record   the   BDAR   action   taken. When   the   mission   is   completed,   as   soon   as practicable,    repair   using   standard   maintenance   procedures. Option   2: Epoxy   and   Self-Tapping   Screw. 1. Locate   leak   and   remove   reservoir. 2. Clean   area   around   hole   with   sandpaper. 3. Fill   holes   with   available   material   such   as   self-tapping   sheet   metal   screw,   and cover   with   a   quick-drying   epoxy   plastic;   or   force   a   sheet   metal   screw   through   a makeshift   washer   (leather   or   rubber).   Use   a   washer, if   available,   to   back   up   the rubber   or   leather. Install   into   hole. Tighten    securely. 4. I n s t a l l    r e s e r v o i r. 5. Record   the   BDAR   action   taken. When   the   mission   is   completed,   as   soon   as practicable,   repair   using   standard   maintenance   procedures. Option   3: Use   One   Reservoir;   Isolate   Damaged   One. 1. Disconnect   the   air   line   from   the   damaged   air   reservoir. 2. Remove   the   line   connecting   both   reservoirs. 3.   Attach   air   line   from   compressor   to   the   good   reservoir. 4. Plug   holes   in   reservoir   to   be   used   with   appropriate   size   pipe   plugs. 5. Start   engine   and   check   for   leaks. 6. Record   the   BDAR   action   taken. When   the   mission   is   completed,   as   soon   as practicable,   repair   using   standard   maintenance   procedures. 11-12

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