![]() FAA Publication | |
Abbreviation | AC 20-152 |
---|---|
Year started | 2005 |
Latest version | A 2022 |
Organization | Federal Aviation Administration |
Domain | Aviation safety |
Website | FAA |
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 electronic hardware for use within the airspace subject to FAA authority. Commonly, the DO-254 has been interpreted as applying to complex custom micro-coded components within aircraft systems with Item Design Assurance Levels (IDAL) of A, B, or C. [1] [2] However, Revision A of this AC clarifies that AC 20-152() and DO-254 applies to all type certification of all electronic hardware aspects of airborne systems, including all electronic hardware that is not complex, that is, "simple electronic devices". Revision A also defines objectives in addition to those identified in DO-254; applicants choosing to follow DO-254 under the authority of AC 20-152A must also accomplish these additional objectives.
Specifically excluding COTS microcontrollers [3] (see AC 20-115()/ DO-178C()), 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 through testing alone, necessitating methodical design assurance. [4] Simple devices are those that are verifiable with testing alone, such that the FAA may agree that methodical design assurance is unnecessary.
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] [3] 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. [5]
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 |
DAL D electronic hardware may use DO-254 or applicable in-house design assurance processes.
![]() FAA Publication | |
Abbreviation | AC 20-152 |
---|---|
Year started | 2005 |
Latest version | A 2022 |
Organization | Federal Aviation Administration |
Domain | Aviation safety |
Website | FAA |
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 electronic hardware for use within the airspace subject to FAA authority. Commonly, the DO-254 has been interpreted as applying to complex custom micro-coded components within aircraft systems with Item Design Assurance Levels (IDAL) of A, B, or C. [1] [2] However, Revision A of this AC clarifies that AC 20-152() and DO-254 applies to all type certification of all electronic hardware aspects of airborne systems, including all electronic hardware that is not complex, that is, "simple electronic devices". Revision A also defines objectives in addition to those identified in DO-254; applicants choosing to follow DO-254 under the authority of AC 20-152A must also accomplish these additional objectives.
Specifically excluding COTS microcontrollers [3] (see AC 20-115()/ DO-178C()), 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 through testing alone, necessitating methodical design assurance. [4] Simple devices are those that are verifiable with testing alone, such that the FAA may agree that methodical design assurance is unnecessary.
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] [3] 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. [5]
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 |
DAL D electronic hardware may use DO-254 or applicable in-house design assurance processes.