AC 20-152

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Development Assurance for Airborne Electronic Hardware
FAA Publication
AbbreviationAC 20-152
Year started2005
Latest versionA
2022 (2022)
OrganizationFederal Aviation Administration
DomainAviation safety
WebsiteFAA

The Advisory Circular AC 20-152A, Development Assurance for Airborne Electronic Hardware, identifies the RTCA-published standard DO-254 as defining "an acceptable means, but not the only means" to secure FAA approval of complex custom micro-coded components within aircraft systems with Item Design Assurance Levels (IDAL) of A, B, or C.[1][2] Specifically excluding COTS microcontrollers,[3] complex custom micro-coded components include field programmable gate arrays (FPGA), programmable logic devices (PLD), and application-specific integrated circuits (ASIC), particularly in cases where correctness and safety can not be verified with testing alone, necessitating methodical design assurance.[4]

For DAL D hardware, as long as the applicant follows DO-254, the applicant does not need to apply this advisory circular since the FAA does not expect to examine the life cycle data.[2][5] However, if the applicant chooses to follow other design practices for DAL D hardware (as permitted by this AC) the FAA will review the data.[6]

Revision History[edit]

History of AC 20-152
Revision Year Title
AC 20-152 30 Jun 2005 Design Assurance Guidance for Airborne Electronic Hardware
AC 20-152A 07 Oct 2022 Development Assurance for Airborne Electronic Hardware

References[edit]

  1. ^ AC 20-152, FAA, Office AIR-100, 2007.
  2. ^ a b Cary Spitzer; Uma Ferrell; Thomas Ferrell, eds. (2015). Digital Avionics Handbook, Avionics, Development and Implementation (3rd ed.). Boca Raton, FL: CRC Press. p. 14-6. ISBN 978-1138076983. DAL D electronic hardware may use DO-254 or applicable in-house design assurance processes.
  3. ^ AC 20-152, FAA, Office AIR-100, page 2, 2007.
  4. ^ "Simple Electronic Hardware and RTCA Document DO-254 and EUROCAE Document ED-80, Design Assurance Guidance for Airborne Electronic Hardware" (PDF). Certification Authorities Software Team Position (CAST-30). FAA. August 2007. Retrieved 2019-09-30.
  5. ^ AC 20-152, FAA, Office AIR-100, page 2, 2007.
  6. ^ ORDER 8110.105A "Simple and Complex Electronic Hardware Approval Guidance" (PDF). FAA. p. 1-1.

External links[edit]