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General fuel cell cleaning.
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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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Depreservation.

TM 1-1500-204-23-3 NOTE It is not necessary to preserve the fuel cells which will be fueled in 10 days or less. (e) PLIOCEL preservation.  If the interior of the cell was not completely coated with the glycerine during the cleaning process, coat the interior of fuel cell with a solution of equal parts of water and glycerine.  This coating may be applied by painting, spraying, fogging, or sloshing.  Drain the excess glycerine solution prior to storage or shipment. Preserve metal fittings with corrosion preventive compound, MIL-C-16173, grade 2.  Cover all small openings with grade A barrier material, MIL-B-121, and secure with tape, PPP-T-60.  Install original cover plates on all access openings.  If cover plates are not available, install polyethylene-lined (L-P-378) plywood plates. NOTE This operation should be done in a well ventilated room to avoid health and fire hazards. (f) Metal tank preservation.  Using aromatic, fuel resistant lacquer, MIL-L-6047, slush the tank interior. Thoroughly   drain   tank.      Rotate   as   necessary   to   remove   any   puddles.      Coating   must   be   thin,   without   puddles. Immediately start aerating tank with air heated to 120   °F (49 °C) for a minimum of 2 hours.  Continue hot air circulation until  a  firm  thumb  pressure  will  not  move  coating.    Allow  lacquer  to  completely  cure  in  a  warm  dry  atmosphere  for  a minimum of 24 hours.  Even when completely dry, this material has a tacky surface.  Complete solvent evaporation must be ensured.  Otherwise, deterioration will occur when the lacquerfilm is exposed to fuel. (6) Handling.  Fuel cells should not be handled any more than necessary.  Observe the following procedures for handling fuel cells: (a) Do not remove cells from original containers until needed for installation. (b) When a cell is uncrated for installation, retain crate for use in packing cell which is removed from service. (c) Cells provided with supporting ribs will have these ribs installed at all times, except when removed to allow  cells  to  be  collapsed  immediately  prior  to  installation  or  removal.    All  cells  not  provided  with  ribs  will  have  a temporary wood brace fitted internally to support cell in normal position while in storage. (d) Do not lift or support cells by fittings. (e) Cells should be transported only on dollys or trucks. (f) Handle  cells  with  extreme  care  to  prevent  their  coming  in  contact  with  sharp  or  pointed  objects  or abrasive surfaces. (g) Do not bend or fold cold cells.  When cells have been stored at low temperatures, allow sufficient time for cell materials to reach temperatures of approximately 70  °F (21 °C) before flexing. (h) Thoroughly  inspect  interior  of  fuel  cell  for  dirt,  foreign  objects/material  prior  to  installation  of  tank fittings. (7) Storage.  Prepare the cleaned and preserved fuel cell for storage as follows: (a) Roll or fold flexible bladder type or Goodyear Nylon (Pliocel) fuel cells as smoothly as possible, and place a roll of corrugated fiberboard, PPP-F-320, covered with polythylene sheeting, L-P-378, inside each fold or roll to prevent creasing. NOTE · Self-sealing  fuel  cells  cannot  be  folded  or  collapsed  for  storage;  however,  they  will  be wrapped in accordance with paragraph (a).  Cells having suspension straps will be hung in a cleated  plywood  box,  PPP-B-601,  or  other  suitable  wooden  box  in  the  normal  on  aircraft position  with  dunnage  used  to  support  this  configuration.    Cells  not  having  suspension straps must be supported inside and out with dunnage. · Dunnage may consist of wood, fiberboard, PPP-P-291 or PPP-F-320, rubberized hard, PPP- C-1   120,   or   foam   plastics,   PPP-C-850,   MIL-P-26514.      All   dunnage   will   be   wrapped   with polyethylene  sheeting,  L-P-378,  or  a  similar  plastic  to  prevent  abrasion  and  contamination. The dunnage will be so placed as to provide support for the fuel cells in the box in the on aircraft configuration.  All self-sealing fuel cells must be supported to prevent collapse and creasing. 2-22

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