MIL-PRF-5350G
Table II. Engine mounted transmitters
Displacement in double amplitude
Frequency (Hz)
(inch)
and acceleration (g), if applicable
5-10
0.2
10-18
0.2 to 0.06 at ±1g
18-99
0.06
99-2000
0.06 to 0.00015 at ±30g
4. VERIFICATION
4.1 Classification of inspections. The inspection requirements specified herein shall be in
accordance with the associated specification and this document and are classified as
follows:
a. First article or qualification inspection (see 4.2).
b. Conformance inspection (see 4.3).
4.2 First article or qualification inspection. Transmitters shall be subjected to all tests in
4.6 and the tests specified in the associated specification.
4.3 Conformance inspection. Conformance inspection shall consist of the following:
a. Individual tests (see 4.3.1)
b. Sampling tests (see 4.3.2)
4.3.1 Individual tests. Each transmitter shall be subjected to the following tests.
a.
Examination (see 4.6.1)
b.
Scale error at room temperature (see 4.6.2)
c.
Friction error (see 4.6.3)
d.
Aircraft attitude (see 4.6.4)
e.
Dielectric strength (see 4.6.5)
f.
Sealing (see 4.6.6)
g.
Electrical zero (see 4.6.7)
4.3.2 Sampling tests. Transmitters shall be subjected to the following sampling tests
According to ANSI/ASQ Z1.4, at the inspection level (normal, tightened, or reduced)
specified in the acquisition document (see 6.2).
a. Electrical characteristics (see 4.6.8)
b. Seasoning (see 4.6.9)
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