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NOT MEASUREMENT SENSITIVE MIL-STD-1796A(USAF) 13 October 2011 SUPERSEDING MIL-STD-1796(USAF) 31 July 1986 MIL-HDBK-87244(USAF) 30 January 1995 DEPARTMENT OF DEFENSE STANDARD PRACTICE AVIONICS INTEGRITY PROGRAM (AVIP) Reinstated after 13 October 2011 and may be used for new and existing designs and acquisitions. AMSC N/A FSG 15GP DISTRIBUTION STATEMENT A. Approved for public release, distribution is unlimited. Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:43Z Check the source to verify that this is the current version before use. MIL-STD-1796A(USAF) ii FOREWORD 1. This standard is approved for use by the Department of the Air Force and is available for use by all Departments and Agencies of the Department of Defense. 2. The Avionics Integrity Program (AVIP) identifies the desi
......................................................... 11 Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:43Z Check the source to verify that this is the current version before use. MIL-STD-1796A(USAF) 1 1 SCOPE 1.1 Scope. This standard identifies the design tasks needed to achieve high reliability, long life, safe operation and supportability of aviation electronics in operational environments. 1.2 Use. This standard should be applied to avionics subsystem and system development programs for military aircraft. Apply the requirements of section 5 to acquisitions by calling out MIL-STD- 1796 as a contractual compliance document. Include the potential of a developer to execute section 5 requirements as source selection evaluation criteria and as statement of work tasking. This
artment of Defense. 2. The Avionics Integrity Program (AVIP) identifies the design tasks needed to achieve high reliability, long life, safe operation and supportability of aviation electronics in operational environments. 3. This standard replaces the Avionics/Electronics Integrity Process (AVIP) handbook, MIL- HDBK-87244. AVIP originated in the mid-1980s as a "reliability by design" standard to improve electronic products used in military applications, then was replaced in the late 1980’s by a less prescriptive handbook. This new version of AVIP revives the original MIL-STD-1796 number and title and is, once again, a standard which can be cited as a contractual requirement. 4. AVIP is focused on the “integrity” performance requirements (tolerate the environment, perform reliably, etc.),
://assist.dla.mil -- Downloaded: 2026-07-20T01:47Z Check the source to verify that this is the current version before use. MIL-HDBK-516D 10 MIL-STD-1587 Material and Process Requirements for Aerospace Weapons Systems MIL-STD-1760 Aircraft/Store Electrical Interconnection System MIL-STD-1787 Aircraft Display Symbology MIL-STD-1791 Designing for Internal Aerial Delivery in Fixed Wing Aircraft MIL-STD-1791-1 Criteria for Nonstandard Airdrop Equipment and Payloads MIL-STD-1796 Avionics Integrity Program (AVIP) MIL-STD-1797 Flying Qualities of Piloted Aircraft MIL-STD-1798 Mechanical Equipment and Subsystems Integrity Program MIL-STD-3009 Lighting, Aircraft, Night Vision Imaging System (NVIS) Compatible MIL-STD-3013 Glossary of Definitions, Ground Rules, and Mission Profiles to Define Air Vehic
ing, Military Flight Operations Quality Assurance, etc.) with the mandatory crash survivable recorder requirement when identifying an aircraft flight data parameter recording, storage, and transmission capability. DAFI20-101_ 63-101 16 FEBRUARY 2024 81 5.4.1.2. Product and System Integrity. For each Aircraft Mission Design Series, the DAF acquires, uses, or leases, the PM establishes integrity programs. 5.4.1.2.1. The PM develops, documents, and executes integrity programs by applying DAFI 63-140, and tailoring and integrating to the extent practicable: MIL-STD-1530D, Aircraft Structural Integrity Program (ASIP); MIL-STD-1796, Avionics Integrity Program (AVIP); MIL-STD-1798C, Mechanical Equipment and Subsystems Integrity Program; MIL-STD-3024, Propulsion System Integrity Program; and MIL-H
e recorder requirement when identifying an aircraft flight data parameter recording, storage, and transmission capability. 5.4.1.2. Product and System Integrity. For each Aircraft Mission Design Series, the DAF acquires, uses, or leases, the PM establishes integrity programs. 5.4.1.2.1. The PM develops, documents, and executes integrity programs by applying DAFI 63-140, and tailoring and integrating to the extent practicable: MIL-STD-1530D, Aircraft Structural Integrity Program (ASIP); MIL-STD-1796, Avionics Integrity Program (AVIP); MIL-STD-1798C, Mechanical Equipment and Subsystems Integrity Program; MIL-STD-3024, Propulsion System Integrity Program; and MIL-HDBK- 513, Low Observable Integrity Program. 5.4.1.2.2. PMs integrate corrosion prevention and control into the Mission Design Seri
tric Field (V/m – rms) Peak Average 0.01 2 88 27 2 30 64 64 30 150 67 13 150 225 67 36 225 400 58 3 400 700 2143 159 700 790 554 81 790 1000 289 105 1000 2000 3363 420 2000 2700 957 209 2700 3600 4220 455 3600 4000 148 11 4000 5400 3551 657 5400 5900 3551 657 5900 6000 148 4 6000 7900 344 14 7900 8000 148 4 8000 8400 187 70 8400 8500 187 70 8500 11000 6299 238 11000 14000 2211 94 14000 18000 1796 655 18000 50000 533 38 Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:47Z Check the source to verify that this is the current version before use. MIL-STD-464D 19 Systems exposed to more than one of the defined EMEs shall use the worst case composite of the applicable EMEs. External RF EME covers compatibility with, but is not limited to, EME’s from like platforms (such as aircraft in
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