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Table 2-7.  Mixing Ratios
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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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Aeroquip  Corporation  Series  3700  and  3750  Quick  Thread  Couplings.

TM 1-1500-204-23-3 1    Examine all accessible fuel cell interconnects, fuel cell access covers, drains, boost pump mounting points, and fuel line connections.  Follow periodic instructions given in applicable aircraft maintenance technical manuals. 2    If  the  aircraft  has  not  had  an  engine  run-up,  operate  fuel  boost  pumps  keeping  main  fuel  shutoff valve closed.  Check for leaks in the lines upstream of the main fuel shutoff valve. (g) Leak detection for engine runup.  If engine runup or test flight is programmed, the leakage test may be conducted any time after the aircraft has been fueled.  Only yellow dyed fuel may be used for engine runup testing on the ground,  after  an  engine  change,  or  for  test  flights  after  a  periodic  or  phased  inspection.    The  dyed  fuel  is  particularly useful  in  checking  for  leakage  near  the  engine  hot  section  area,  where  high  temperatures  prevent  leaking  fuel  from leaving a wet spot.  When the dyed fuel evaporates from a surface, the dye remains as a deposited residue. 1 Perform engine runup or test flight in accordance with applicable directives. 2 Upon   completion,   carefully   examine   main   fuel   line   shutoff   valve   connections   and   all   other connectors downstream from it.  Any dye deposit indicates leakage. WARNING Dry-cleaning  solvent  is  flammable  and  solvent  vapors  are  toxic.    Use  P-D-680, Type  II  Solvent  in  a  well-ventilated  area.    Keep  away  from  open  flames.    Avoid prolonged solvent contact with skin. 3 When a leak has been repaired, remove the dye stain with the aircraft fuel or dry-cleaning solvent conforming  to  P-D-680,  Type  II,  and  repeat  the  applicable  test.    Recheck  repaired  areas  to  verify  leakage  has  been stopped. (h)    Disposition of dyed fuel.  JP-4 fuel dyed with yellow dye may be left in the fuel system, following leak detection operations and used in normal operations. 1    Yellow dyed fuel which must be removed from the fuel system may be placed in bulk storage and used without dilution or mixed with other dyed fuel which has been diluted. 2 JP-4 fuel dyed with red dye liquid will be diluted in the aircraft 10 to 1 with undyed fuel and used in normal operations or removed from the aircraft and placed in bulk storage where it is diluted 10 to 1 with undyed fuel. This fuel may then be issued to base assigned aircraft for normal use. 3    The bulk tank in which the dyed fuel is stored or mixed with standard fuel will be marked with signs 4 x  12  inches,  black  letters  on  white  background,  which  will  be  prepared  using  wood  or  similar  material.    The  signs  will read:  THIS  TANK  CONTAINS  LEAK  DETECTION  DYED  FUEL.    These  signs  will  be  temporarily  attached  to  the receiving  and  issuing  valves.    When  all  of  the  dyed  fuel  has  been  issued,  the  signs  will  be  removed.    This  should  be accomplished in order to avoid confusion with colored gasoline. 4    Any excess liquid stain on aircraft, fuel cell, or storage equipment may be removed by wiping with a cloth.    The  dye  will  lose  color  over  a  short  period  of  time;  therefore,  it  is  not  necessary  to  take  special  measures  to remove all stains. (i)    Servicing procedures to transient aircraft.    Dyed fuel stored in bulk storage facilities will be serviced to locally assigned aircraft.  It will not be serviced to transient aircraft.  The presence of dyed fuel in transient aircraft could be  falsely  construed  by  air  crews  and  maintenance  personnel  as  contaminated  fuel.    If  emergencies  arise  requiring servicing  of  dyed  fuel  to  transient  aircraft,  the  crew  will  be  advised  and  note  made  on  aircraft  form  that  aircraft  was serviced with dyed fuel. (2) Approved testing fluids.  The following approved calibrating fluids and their uses are listed as follows: CAUTION Equipment  calibrated  with  MIL-C-7024  Type  I  will  not  be  operated  using  other fluids.   Incorrect calibration may result. · MIL-C-7024,  Type I is used to test switches on aircraft using AVGAS. · MIL-C-7024A,  Type I is used to test fuel system components for reciprocating engines. · MIL-C-7024,  Type II is used to test switches on aircraft using jet fuel. 2-30

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