MIL-DTL-45360H(AT)
b. Disconnect the air cleaner hose between the air cleaner and engine intake at the air
cleaner outlet. Place an air restrictor boot over the engine intake to completely
shut off the supply of air to the engine. (The air restrictor boot shown in figure 1
has proven satisfactory for engine preservation.)
c. Place the engine fuel control to the "ON" position. Open the regulator valve on
the auxiliary container. Crank the engine with the starter (NOTE: Engine may fire
for approximately 5 seconds) for not less than 30 seconds and not greater than
45 seconds. If the red-colored preservative oil is not observed within the 30- to
45-second period, rest the starter for a period of 3 minutes and repeat the cranking
procedure.
CAUTION: Special precautions shall be taken to assure that the time limits specified are
not exceeded. Damage to the starter solenoid or hydrostatic lock may
result.
d. Close the regulator valve on the auxiliary container and disconnect it from the fuel
pump supply line and reconnect the fuel pump supply line to the primary filter.
Remove the transparent fuel line, and reconnect the vehicle fuel return line at the
quick disconnect coupling. Turn on the vehicle fuel supply system. Remove the
air restrictor boot and reinstall the hose to the air cleaner (see 4.5.2.3).
3.1.8.6.3 Preservation through air intake and exhaust system, without turbocharger.
Atomize 1 ounce of preservative oil conforming to grade 1 of MIL-P-46002 into the exhaust
opening. Seal the opening with tape conforming to type IV of MIL-T-22085. Disconnect the
hose at the air intake and atomize 1 ounce of preservative oil conforming to grade 1 of
MIL-P-46002 into the intake manifold. Seal the opening with tape conforming to Type IV of
MIL-T-22085 (see 4.5.2.3).
3.1.8.6.4 Preservation through air intake and exhaust system, with turbocharger.
Atomize 1 ounce of preservative oil conforming to grade 1 of MIL-P-46002 into the external
exhaust opening. Seal the opening with tape conforming to type IV of MIL-T-22085. Remove
the exhaust tube between the turbocharger and left exhaust manifold. Atomize 1 ounce of
preservative oil conforming to grade 1 of MIL-P-46002 into the left exhaust manifold, then
atomize 2 ounces of grade 1 of MIL-P-46002 into the right exhaust manifold and the bottom of
turbocharger through the left opening in the bottom of turbocharger, and replace the left exhaust
tube. Disconnect the air cleaner hose at the turbocharger inlet, and atomize 1 ounce of grade 1 of
MIL-P-46002 into the turbocharger. Seal the opening with tape conforming to type IV of
MIL-T-22085 (see 4.5.2.3).
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