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Page Title:
Fuel System Components: General Specification For |
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|  MIL-F-8615D
29 March 1976
SUPERSEDING
MIL-F-8615C
26 February 1969
MILITARY SPECIFICATION
GENERAL SPECIFICATION FOR
FUEL SYSTEM COMPONENTS:
This specification is approved for use by all Departments
and Agencies of the Department of Defense.
SCOPE
1.
1.1 Scope. This specification covers the requirements for aircraft fuel,
vent, and propulsion system functional components.
1.2 Classification. Components shall be identified by class based upon a
-
temperature environment in accordance with table I.
TABLE 1.
Temperature classification.
T
- High operational fuel temperature
- High fuel test temperature
.
- High ambient temperature
1.2.1 Non-standard environment. Wherever the temperature environment exceeds
the classes of 1.2, or where unusual circumstances exist, the lowest and high-
est fluid, vapor, and ambient temperatures shall be identified. A component
may still belong to one of the above classes if the exposure to a higher ambient
temperature
is transitory and does not result in heating the component
for more than 15 minutes total
more than 30C above the test temperature
during 10 hours of operation.
FSC 2915
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