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|  MIL-S-85419 (AS)
TABLE I - FUEL CONTAMINANTS
3.6.22 Lubrication System. The lubrication system can be
provided with oil from the aircraft main engine at a maximum
continuous flow rate of 85 gal/hr. with an initial bulk
temperature of 300F in an outside ambient of 122F and an engine
compartment temperature of 158F. The lubrication system shall
be designed to use MIL-L-23699 oil and shall be compatible with
MIL-L-7808 oil and its intermittent use.
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