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|  MIL-L-23822C(AS)
4.5.4.7.2 (Cont'd)
based upon atmosphere of NACA Report No. 1235. Calcuated
thrust shall fall within the thrust requirements of Table I.
4.5.5
Leakage.
The rocket engine of 3.1 shall be
visually examined. for leakage of propellant prior to and during
the test of 4.5.2 (See Table I.)
4.6
Reliability tests. The rocket engine reliability
requirements of 3.6 shall be satisfied upon satisfactory con-
formance of the sample selected in accordance with 4.3.4 to the
static firing tests of 4.5.4.1, and the corrective action of 4.8
in the event of a rejection.
4.7
Rejections.
4.7.1
Quality conformance sample rejection. The
failure of any quality conformance sample (4.3.2) to pass the
inspection and test outlined in this specification shall cause
conditional rejection of all rocket engines represented by that
sample, and all subsequent lots, subject to corrective action
and retest (4.8).
4.7.1.1
Performance rejection.
In the event the quality
conformance sample performs outside the limits specified in
the QVT Data Report (4.3.2.1), the lot represented by the QVT
sample shall be considered conditionally rejected. Analysis of
the limit(s) exceeded shall be prepared and submitted to the pro-
curing agency for lot acceptance or lot rejection directions,
4.7.2
Salvaged pieces.
Any piece(s) from a rejection
rocket engine may be salvaged for use subject to approval by
the procuring agency, providing each salvaged piece is inspected
and is found to be in complete accordance with the requirements
of this specification and the associated drawings and specifications.
4.8
Corrective action and retest.
4.8.1
Corrective action. In the event any sample repre-
senting a quality conformance lot fails to pass the inspection and
tests outlined herein, the supplier may have the opportunity of
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