Annex B: Certification Plan and Certification Basis (Steps 2a and 2b)
1. General
1.1 This annex provides guidance on developing the surveillance system certification plan and certification basis.
2. Rationale and Guidance – Certification Plan
2.1 The Applicant is responsible for developing the certification plan and, if the design change is out of scope, for submitting it to DTAES 3 for approval. DTAES 3 will staff the plan to DTAES 6 for the review of the surveillance system technical aspects of the plan, specifically the certification basis, means and methods of compliance, and surveillance system criteria. During the development of the plan, it is recommended that the Applicant consult DTAES 6 staff for assistance.
2.2 In addition to the standard certification plan requirements defined in the TAM (regulatory reference 3.2.1.a), Parts 2 and 3, the plan must include the following:
- the currently approved type design and any already approved surveillance system capabilities;
- the new surveillance system capabilities to be certified (Step 1);
- the current and proposed aircraft surveillance system equipment configuration to be approved, including any differences across the fleet;
- any operating configurations and equipment restrictions that affect surveillance capabilities, including those for mission equipment and external stores. This information is used to determine the scope of compliance demonstration tests and analyses; and
- the proposed certification basis (Step 2a).
3. Rationale and Guidance – Certification Basis
3.1 As described in paragraph 4.2.2.b.(1) of the advisory, the certification requirements that will form the certification basis must be selected from one of the approved civil or military airworthiness codes identified in the ADSM (regulatory reference 3.2.1.b).
3.2 Table B-1 provides a listing of the certification requirements that should be considered when defining the certification basis for a surveillance system design change. This table provides only an example of requirements, it does not constitute an exhaustive list of requirements involving Surveillance systems certification. Certain changes could involve, for example, control and stability requirements due to installation of large antennas on the exterior part of the aircraft.
3.3 The Applicant must include aircraft cybersecurity requirements within the certification basis. Table B-1 is FAA-centric and, at the time this TAA advisory was published, the FAA, unlike EASA, did not have specific Title 14 Code of Federal Regulations (14 CFR) paragraphs that dealt with Aircraft Cybersecurity. EASA has codified Aircraft Cybersecurity requirements by including paragraph 1319 into the following Certification Specifications (CS) 25, 27, and 29 (Table B-1 item 23). The EASA Aircraft Cybersecurity requirements for CS -2323 are addressed in EASA Guidance Material (GM) 23.2500(b). The ADSM (regulatory reference 3.2.1.b) Part 2, Chapter 6 – “Aircraft Cybersecurity” provides additional details on establishing an aircraft cybersecurity certification basis. Furthermore, DTAES 8 staff can provide assistance in establishing the aircraft cybersecurity certification basis.
4. Rationale and Guidance – Standards, Means and Methods of Compliance, and Guidance Documents
4.1 Table B-2 should be consulted to identify the appropriate standards, means and methods of compliance, and guidance material applicable to the required surveillance capabilities identified in Step 1. Once identified, the criteria should be collated to create the Surveillance Criteria Table, as described in Step 2c – Setting up the Surveillance Criteria Table.
Notes: 1. For clarity, only the FAA TSOs are listed in Table B-2. However, the equivalent Canadian TSO (CAN-TSO) or EASA TSOs (E-TSO) are also acceptable, unless otherwise indicated.
2. The FAA TSOs, CAN-TSOs and E-TSO will generally reference RTCA and EUROCAE specifications. Frequently, the TSO will add new requirements, modify or delete specific RTCA and EUROCAE requirements. Therefore, the RTCA and EUROCAE specifications associated with the TSOs identified in Table B-2 may also constitute acceptable standards, provided the TSO additions, modifications and/or deletions are addressed.
4.2 Specialist knowledge and experience are required to interpret and select the appropriate criteria. The DTAES 6 engineering support staff can be contacted to assist in the selection of the applicable criteria and the development of the Surveillance Criteria Table. Guidance material for the development of the Surveillance Criteria Table is provided in Annex C of this advisory.
4.3 The final step in demonstrating compliance is the identification of compliance artefacts, which will be provided to support the findings of compliance and design assessment. Examples of compliance artefacts include:
- Design description documents;
- Design analysis reports;
- Integration lab test reports;
- Aircraft ground and flight test reports;
- TSO Authorization (TSOA) or Military Standard Order (MSO) approval references; and
- Approvals from other Airworthiness Authorities.
4.4 Table B-3 provides an ADS-B Out example of surveillance system certification basis and compliance matrix. The first three columns in the table relate to the certification basis.
Table B-2 Design Standards, Means and Methods of Compliance, and Guidance Material by Type of Surveillance Capability
Mode A/C
| Design Standards | Means and Methods of Compliance or Guidance Material |
|---|---|
FAA TSO-C74 (b), (c) or (d) FAA TSO-C88 (AR) |
FAA AC 23-8C – Transponder specific content FAA AC 25-7C – Transponder specific content FAA AC 27-1B – Transponder specific content FAA AC 29-2C – Transponder specific content |
| EASA CS-ACNS Issue 4 | EASA CS-ACNS Issue 4 |
Mode S
| Design Standards | Means and Methods of Compliance or Guidance Material |
|---|---|
FAA TSO-C112 (e) |
FAA AC 20-131A – Mode S specific content FAA AC 20-151C – Mode S specific content |
| EASA CS-ACNS Issue 4 | EASA CS-ACNS Issue 4 |
ADS-B Out
| Design Standards | Means and Methods of Compliance or Guidance Material |
|---|---|
| TCCA AWM 551.103 | TCCA AC 500-029 Issue 2 |
FAA TSO-C166 (b) |
FAA AC 20-165B |
| EASA CS-ACNS Issue 4 | EASA CS-ACNS Issue 4 |
ADS-B In
| Design Standards | Means and Methods of Compliance or Guidance Material |
|---|---|
FAA TSO-C195 (b) |
FAA AC 20-172B |
IFF Mode 1, 2, 3 and 5
Department of Defense (DoD) Air Traffic Control Radar Beacon System, Identification Friend or Foe, Mark XII/Mark XIIA, Systems (AIMS) 17-1000
NOTE: Although not explicitly considered as technical airworthiness standards, the U.S. DoD AIMS standards have been included for reference purposes.
| Certification Requirement and Title | Certification Requirement Text [Caution: Exact requirement will depend on |
Notes | Means of Compliance | Compliance Artefacts | Finding Authority |
|---|---|---|---|---|---|
14 CFR xx.1301 Function and Installation |
Each item of installed equipment must: (a) Be of a kind and design appropriate to its intended function; (b) Be labeled as to its identification, function, or operating limitations, or any combination of these factors; (c) Be installed according to limitations specified for that equipment; and (d) Function properly when installed. |
n/a | Applicable portions of: AC 23-8C. 25-7D, 27-1B , 29-2C, and 20-165B, as defined in the Criteria Table |
Design Data, Analysis and Test Reports Design Assessment Report |
FA Avionics and Software |
14 CFR xx.1309 Equipment, Systems and Installations |
The equipment, systems, and installations whose functioning is required by this subchapter, must be designed to ensure that they perform their intended functions under any foreseeable operating condition. |
n/a | AC 23/25.1309, and applicable portions of AC 27-1B, 29-2C, AC 20-165B, as defined in the Criteria Table | Design Data, Analysis and Test Reports Design Assessment Report |
FA Avionics and Software |
14 CFR xx.1309 Equipment, Systems and Installations |
The airplane systems and associated components, considered separately and in relation to other systems, must be designed so that (1) The occurrence of any failure condition which would prevent the continued safe flight and landing of the airplane is extremely improbable, and (2) The occurrence of any other failure conditions which would reduce the capability of the airplane or the ability of the crew to cope with adverse operating conditions is improbable. |
n/a | AC 23/ 25.1309, and applicable portions of AC 27-1B, 29-2C, AC 20-165B, as defined in the Criteria Table |
Design Data, Analysis and Test Reports Design Assessment Report |
FA Avionics/ Software and System Safety |
14 CFR 25.1310 Power Source and Distribution |
Each installation whose functioning is required for type certification or under operating rules and that requires a power supply is an “essential load” on the power supply. The power sources and the system must be able to supply the following power loads in probable operating combinations and for probable durations |
n/a | Applicable portions of AC 25-7D and AC 20-165B, as defined in the Criteria Table | Design Data, Analysis and Test Reports Design Assessment Report |
FA Electrical |
Mil HDBK 516 section 13.2.4 Lightning Effects |
516-Criterion: Verify that the air system has met all requirements for lightning, |
Or CFR 23.1306 or CFR 25/27/29.1316 Lightning Protection |
Mil Std 464 or AC 20-136B, and applicable portions of AC 27-1B, 29-2C, and AC 20-165B, as defined in the Criteria Table |
Design Data, Analysis and Test Reports Design Assessment Report |
FA E3 |
14 CFR 23.1308, 25/27/29.1317 High-intensity Radiated Fields (HIRF) Protection. |
Each electrical and electronic system that performs a function (1) The function is not adversely affected during and after the |
n/a | FAA AC 20-158A, and applicable portions of AC 27-1B, 29-2C and AC 20-165B, as defined in the Criteria Table | Design Data, Analysis and Test Reports Design Assessment Report |
FA E3 |
14 CFR xx.1321 Flight Instruments |
Each flight, navigation, and power plant instrument for use by any pilot must be plainly visible to him from his station with the minimum practicable deviation from his normal position and line of vision when he is looking forward along the flight path. |
n/a | Applicable portions of AC 27-1B, 29-2C and AC 20-165B, as defined in the Criteria Table | Design Data, Analysis and Test Reports Design Assessment Report |
FA TN – Avionics/ HFE |
14 CFR xx.1322 Flight Crew Alerting |
Flight crew alerts must: (1) Provide the flight crew with the information needed to: |
n/a | Applicable portions of AC 27-1B, 29-2C and AC 20-165B, as defined in the Criteria Table | Design Data, Analysis and Test Reports Design Assessment Report |
FA Avionics |
| 14 CFR xx. Electronic Equipment |
(a) In showing compliance with § 25.1309 (a) and (b) with respect to radio and electronic equipment and their installations, critical environmental conditions must be considered. (b) Radio and electronic equipment must be supplied with power under the requirements of § 25.1355(c). (c) Radio and electronic equipment, controls, and wiring must be installed so that operation of any one unit or system of units will not adversely affect the simultaneous operation of any other radio or electronic unit, or system of units, required by this chapter. (d) Electronic equipment must be designed and installed such that it does not cause essential loads to become inoperative as a result of electrical power supply transients or transients from other causes. |
Applicable portions of AC 27-1B, 29-2, 20-151C and AC 20-165B, as defined in the Criteria Table | Design Data, Analysis and Test Reports Design Assessment Report |
FA EMC | |
| 14 CFR xx.1529 | Instructions for Continued Airworthiness (ICAs) | n/a | Applicable portions of AC 20-151C and 20-165B, as defined in the Criteria Table | Reports | DTAES 4 |
14 CFR xx.1581 Flight Manual |
An Airplane Flight Manual must be furnished with each airplane, and it must contain the following: (1) Information required by §§25.1583 through 25.1587; (2) Other information that is necessary for safe operation because of design, operating, or handling characteristics. |
n/a | AC 25.1581, applicable portions of AC 23-8C, 25-7D, 27-1B, 29-2C and 20-165B, as defined in the Criteria Table | FM/AOI and/or FM/AOI changes | FA AFM |
Aircraft Cybersecurity EASA CS 25.1319 Equipment, systems and network information protection Note: CS 27/29.1319 contain similarly worded requirements. Note: Guidance on CS 23 is provided in GM 23.2500(b). |
Consulting ADSM Part 2, Chapter 6 and DTAES 8 when developing An example of an acceptable cybersecurity requirement that could (a) Aeroplane equipment, systems and networks, considered (b) When required by paragraph (a), the applicant must make procedures and ICA available that ensure that the security protections of the aeroplane’s equipment, systems and networks are maintained. |
n/a | EASA AMC - 25.1319 EASA AMC 20-42 |
Design Assessment Report Design Data, Analysis and Test Reports |
DTAES 8 |