MIL-DTL-83454A
6. NOTES
(This section contains information of a general or explanatory nature that may be helpful,
but is not mandatory.)
6.1 Intended use. The blind plate stud terminals covered by this specification are
intended for use in aircraft applications requiring high mechanical and electrical reliability and
high resistance to physical extremes of temperature, vibration, and shock.
6.2 Acquisition requirements. Acquisition documents should specify the following:
a.
Title, number, and date of this specification.
b.
Complete PIN (see 1.3).
d.
Nuts, lock washers, and flat washers, if required (see 3.3.1).
d.
e.
Sampling plan, if required (see 4.3.3).
AQL (see 4.4.2.1).
f.
Inspection periodicity, if required (see 4.4.3).
g.
Test condition, if different (see 4.5.5).
h.
Type of thermal shock test, liquid or air (see 4.5.5).
i.
Electrical load conditions for high frequency vibration test, if required (see 4.5.6).
j.
k.
Electrical conditions for humidity testing, if required (see 4.5.9).
Packaging requirements (see 5.1).
l.
6.3 Subject term (key word) listing.
Aircraft
Cadmium
Electromagnetic
Electronic
EMI
Hazard
IMI
Interference
Intermodulation
Lug
Radiation
Radio frequency
Rivet
RFI
Shielding
Vibration
6.4 Changes from previous issue. Marginal notations are not used in this revision to
identify changes with respect to the previous issue due to the extent of the changes.
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