MIL-STD-1796 Avionics Integrity Program AVIP This standard identifies the design tasks needed to achieve high reliability, long life, safe operation and supportability of aviation electronics in operational environments.

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MIL-STD-1796A(USAF)

CONTENTS

PARAGRAPH                                                                                                                                            PAGE

5.5.4       Characterizing materials and components............................................................. 19

5.5.5       Identification and tracking of critical items and critical functions ......................... 19

5.5.6       Analysis ................................................................................................................... 19

5.5.7       Tests and demonstrations ...................................................................................... 19

5.5.8       Life management .................................................................................................... 19

6       NOTES.................................................................................................................................... 19

6.1      Intended use................................................................................................................... 19

6.2      Acquisition requirements............................................................................................... 19

6.3      Subject term (key word) listing ...................................................................................... 20

6.4      Changes from previous issue ......................................................................................... 20

FIGURES

FIGURE 1.  Tolerance and margin relationship. .............................................................................. 5

TABLES

TABLE I.  Summary of AVIP requirements. ..................................................................................... 9

TABLE II.  Timing of environmental and life testing...................................................................... 11

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