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|  MIL-P-5238C
4.5.24.3 Icing test. The pump shall be operated in the above-conditioned
fuel (step j) for 30 minute periods at 30F, 20F,
and
The fluid
temperature shall be maintained within the limits of plus 1F and minus 5F
throughout the tests. The pump output and power input, and leakage, shall
be recorded.
4.5.25 Disassembly and inspection. Following completion of all tests, each
test pump shall be disassembled for inspection. There shall be no evidence
of any problem that will affect either safety or performance or may cause
premature wearout Photographs shall be taken of each part and of any crit-
ical area discussed in the test report.
4.6 Safety , reliability, and maintainability. The safety analysis report
and the reliability and maintainability demonstration plans shall be provided
in accordance with the procurement document.
PREPARATION FOR DELIVERY
5.
5.1 Preservation and packaging and packing shall be in accordance with the
detail specification.
5.2 Marking of shipments. In addition to any special marking required by
the contract or order interior packages and exterior shipping containers
shall be marked in accordance with MIL-STD-129.
5.2.1 Reinspection dates. Reinspection data marking shall be added as
specified by the procuring activity.
NOTES
6.
6.1 Intended use. The pumps covered by this specification are intended for
use in aircraft fuel tanks to pump fuel to the engines and to transfer fuel
from tank to tank and may also have other specified USCS.
Procurement documents should specify the following:
6.2 Ordering data.
Title, number and date of this specification.
a.
b.
The reviewing and approval activity.
Instructions for delivering of data (6.3).
c.
d. If additional testing is required, the number of test samples and the
test activity. (See 4.3)
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