MIL-PRF-38039D
j. If identification of the industrially accepted test methods for altitude, acceleration, and
solar radiation testing is required (see 4.5.7).
k. Packaging requirements (see 5.1).
l. Maximum power consumption requirement (3.6.5).
6.3 Suggested processes. Procedures discussed in the following paragraphs have proven
successful in previous procurements of Warning, Caution, and Advisory Illuminated Systems.
6.3.1 Wiring. MIL-STD-681 has been satisfactorily used as guide for color coding of
internal wiring.
6.3.2 Finish. Color No.36231, and Color No. 37038 of FED-STD-595 are accepted
industry standards for the color of the nonfunctional portion of the system exposed to view from
the aircraft cockpit.
6.3.3 Solar radiation tests. MIL-STD-810, Method 505.4, Procedure II has been
satisfactorily used in previous procurements to verify the solar radiation requirement.
6.3.4 Label. SAE-AS18012 has been satisfactorily used in previous procurements as a
labeling guide. Color No. 37875, lusterless white, in FED-STD-595 is an accepted industry
standard for the color of the labels.
6.3.5 Acceleration test. In previous procurements, MIL-STD-810, Method 513.5,
Procedure I, at 10 g has been satisfactorily used to verify the acceleration requirement.
6.3.6 Altitude test. MIL-STD-810, Method 500.4, Procedure I has been satisfactorily
used in previous procurements to verify the altitude requirement.
6.4 Subject term (key word) listing.
Control panel
Hermetic seal
Indicator display
6.5 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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