Downloaded from https://www.everyspec.com MIL-STD-810D 19 July 1983 d. Tk&QwaQw . For prooedure 1, the test duration should be representative of the anticipated service environment, but a test duration of at least 1 hour is considered adequate for most equipment. Procedures II and 111 do not require extended periods at the test pressure, once it haa been reached and any required funotions are performed. e. lest item confLswLbn. Configure the test item in a manner that is characteristic of its normal configuration, i.e., operational for high ground elevation simulation,,in its shipping/atorage 00ntainer for air tranaport, etc. -. f. .
Review the equipment specification and requirements documents, Apply any additional guidelines neceaaary. I-Q.1 ~. Failure criteria for procedures I and II are aa described n General Requirements, 4.9. + For procedure III, the teat item fails only if rap~d decompression causes a hazard to the aircrSft or to the. personnel; the test item need not show satisfactory peat-test performance unless otherwise specified. 1-4.2 &.umnarvof teat information re~~. The following information is required in the test plan for adequate conduct of the tests of section II: o a. Test procedure. b. Test altitude(s). c. Altitude change ratea. d. Test duration. e. Test item configuration. f.
Additional guidelines used. / Extremes for ~. . 15 December 1973.a” / , / .3 b. s of lal tarv ~ m Bedford, MA: Air Force Cambridge Research Laboratories, 19’/4. D;IC number AD-780-508. /~ I-5 E.E+CES / MIL-STD-21O, ~atio / .. c. . t@idbOOk Of Gwr@iiks and S.PaceEnvironmw. Bedford, MA: US Air Force Cambridge Researoh Laboratories, Office of Aerospace Research, 1965. ~ d. ~: 1976. NOAIVMSAIUSAF , 1976. MSTHOD 500.2 500.2-5 19 JUIY 1983 ,-