Based on the United Nations International Civil Aviation Organization (ICAO) agreements, authorities must exist that ensure safe design of aircraft.
For the EU, EASA has been assigned this role by European regulation EU 2018/1139 (Basic Regulation). The procedures for design, production and other airworthiness tasks are
laid down in EU regulation 748/2012, also called Part 21.
Part 21 defines that a product (A/C, engine or propeller) needs a Type Certificate (TC) so that the design can be considered airworthy.
A TC needs to be applied for to EASA and only organisations that hold a Design Organisation Approval (DOA) from EASA can do so.
The process of obtaining a TC includes showing compliance of the product to the certification specifications (CS) and Special Conditions (SC) issued by EASA for various
A/C and product classes. This process is based on a certification programme that describes how compliance to every requirement from the certification base is shown.
Design Organizations (DO) work together with EASA to ensure safety of the design.
Especially, Part 21 demands that every DO has Certification Verification Engineers (CVE) who independently of the design team check if a design is compliant to the applicable requirements from EASA.
For software, product security and Airborne Electronic Hardware (AEH), dedicated sub-processes in the certification are undertaken to show that the design is safe and secure.
TSSC can support your new DO by defining procedures for the Design Organisation Handbook (DOH) for Software, security and AEH procedures.
TSSC has experience in defining certification programmes based on the specific CS and SC (e.g., SC E-18 and E-19 for electric propulsion systems) and can support with advice and guidance.
We can also supply a CVE for SW and security for your design organisation that does the independent checking and presents the SW and security process results to EASA.