AC 20-140A - Guidelines for Design Approval of Aircraft Data Communications Systems
Document Information
20-140A - Guidelines for Design Approval of Aircraft Data Communications Systems
- Date Issued
- April 07, 2010
- Responsible Office
- AIR-130, Aviation Safety - Aircraft Certification Service, Aircraft Engineering Division
- Description
a.
The guidance in this advisory circular (AC) provides one acceptable means of
b.
supplemental type certificates (STC) involving aircraft data link systems intended to support air
traffic services. This AC will standardize these approvals among the aircraft certification offices
(ACOs) in their assessment of aircraft data link systems for design approval.
Use the guidance in this AC to gain approval for type certificates (TC) andc.
Organization (ICAO) Annexes and guidance material, RTCA Inc. documents (RTCA DO) and
European Organization for Civil Aviation Equipment documents (EUROCAE ED). It is based
on published safety and performance (SPR) standards and interoperability (INTEROP) standards
for data link systems in different types of operating environments.
This AC was developed in consideration of the International Civil Aviationd.
guidelines and to outline a means of showing that an aircraft data link system complies with
airworthiness requirements.
This AC is not mandatory and does not constitute a regulation. It is issued to providee.
with a data link system installed. It identifies specific configurations of aircraft data link systems
intended for air traffic services in order to facilitate operational approvals for aircraft that comply
with this AC. AC 120-70A, Operational Authorization Process for Use of Data Link
Communication System, or latest revision provides guidelines for the operational authorization
needed to use the data link capability. Appendix A of this AC provides a list of related
documents. Appendix B of this AC contains a list of applicable acronyms.
This AC provides airworthiness requirements for the type design approval of aircraftcompliance, but not the only means, for type design approval of aircraft that have a data link
system installed.
- AC 20-140A (PDF, 130 KB)