Master’s in Military Certification and Airworthiness Engineering (EMAR/EASA Mil)
Online master's programme of 1,900 hours in military certification and airworthiness engineering (EMAR/EASA Mil). 12 modules covering European military airworthiness, EMAR 21, EMACC, MIL-HDBK-516, continuing airworthiness, EMAR 145/66/147, system and software safety, unmanned systems, certification testing, safety management and programme ethics, with an assigned technical tutor.
Take the controls.
Run a real engineering trade-off from this field. Move the sliders, watch the model react in real time and beat the challenge.
What you will be able to do
Understand the European military airworthiness framework.
Apply EMAR 21 to design and production certification.
Use the EMACC and MIL-HDBK-516C as technical criteria.
Manage continuing airworthiness according to EMAR M.
Audit maintenance and training organisations.
Certify systems, software and unmanned aircraft.
Manage safety and ethics in the certification function.
Who it's for
- Military airworthiness engineers
- Certification engineers
- Continuing airworthiness managers
- Auditors of aviation organisations
- System safety engineers
- Design organisation managers
- Engineering or science graduates aiming to join airworthiness authorities
What you'll work with
- EMAR 21 (European military airworthiness requirements)
- EMAR 145 (maintenance organisations)
- EMAR M (continuing airworthiness)
- EMACC (European military airworthiness certification criteria handbook)
- MIL-HDBK-516C (airworthiness certification criteria)
- STANAG 4671 (airworthiness requirements for unmanned aircraft systems)
- SAE ARP4754A (guidelines for development of civil aircraft and systems)
- DEF STAN 00-970 (design and airworthiness requirements for service aircraft)
- IBM DOORS
- AMOS (Swiss AviationSoftware)
- Isograph FaultTree+
- MATLAB
- SAP PM
12 modules · 1900 h
1.1The concept of airworthiness1.2Differences between civil and state aviation1.3European Defence Agency and the MAWA Forum1.4EMAR requirements1.5National military airworthiness authorities1.6Spanish military airworthiness framework1.7Recognition between authorities1.8Ethics and responsibility1.9Evolution of the European framework1.10Case study: map of airworthiness authorities in Europe
2.1Military type certification2.2Approved design organisations2.3Approved production organisations2.4Certification bases2.5Changes and repairs2.6Certificates of airworthiness2.7Use of EASA civil certification2.8Comparison with Part 212.9Approval documentation2.10Practical: application for design organisation approval
3.1The EMACC handbook3.2Structure of the criteria3.3Structures3.4Flight systems3.5Propulsion3.6Avionics and software3.7Electrical systems3.8Human factors3.9Selection of applicable criteria3.10Lab: EMACC matrix for a system
4.1Structure of MIL-HDBK-516C4.2Criteria by discipline4.3The US certification process4.4DEF STAN 00-9704.5UK MAA regulation4.6Comparison of approaches4.7Multinational programmes4.8Cross-certification credits4.9Lessons from programmes4.10Case study: EMACC versus MIL-HDBK-516C comparison
5.1EMAR M and airworthiness management5.2CAMO management organisations5.3Maintenance programmes5.4Airworthiness directives5.5Airworthiness reviews5.6Aircraft registration5.7Reliability data5.8Occurrence reporting5.9Life extension5.10Practical: airworthiness review of an aircraft
6.1EMAR 145 maintenance organisations6.2EMAR 66 personnel licensing6.3EMAR 147 training organisations6.4Quality systems6.5Human factors in maintenance6.6Certificates of release to service6.7Tools and equipment6.8Subcontracting6.9Authority audits6.10Workshop: audit of an EMAR 145 organisation
7.1ARP4761 safety assessment7.2ARP4754A development7.3DO-178C software7.4DO-254 hardware7.5MIL-STD-882E7.6Safety cases7.7DO-326A cybersecurity7.8COTS components7.9Risk management7.10Case study: safety analysis of an avionics change
8.1Airworthiness of military UAS8.2STANAG 46718.3STANAG 47038.4UAS risk categories8.5Software and autonomy8.6Command and control links8.7Airspace integration8.8Certification of operations8.9Ethics and human oversight8.10Practical: certification basis for a light UAS
9.1Test planning9.2Ground tests9.3Flight tests9.4Instrumentation9.5Test risk management9.6Data analysis9.7Compliance reports9.8Review boards9.9Safety in testing9.10Case study: certification test plan for a modification
10.1Safety management systems10.2Airworthiness risk analysis10.3Just culture10.4Occurrence reporting and analysis10.5Safety indicators10.6Military accident investigation10.7Lessons learned10.8Integration with operations10.9Safety auditing10.10Workshop: occurrence trend analysis
11.1Programme certification strategy11.2Certification cost and schedule11.3Managing the relationship with the authority11.4International cooperation11.5Export control11.6Independence of the certification function11.7Legal liability11.8Professional ethics11.9Transparency11.10Case study: certification strategy for a multinational programme
12.1Selection of the product or change12.2Applicable regulatory framework12.3Certification basis12.4Compliance matrix12.5Safety analysis12.6Test plan12.7Continuing airworthiness plan12.8Conclusions12.9Master's Thesis report12.10Master's Thesis: defence before a panel
How you'll learn
The programme is delivered 100% online on the SEIUM campus, with downloadable material, recorded classes and an assigned technical tutor. There are no fixed timetables: you progress at your own pace within each intake, so you can combine it with your job.
Each module combines theory, guided reading of the original standard and applied exercises. The working software is IBM DOORS, AMOS (Swiss AviationSoftware), Isograph FaultTree+, MATLAB and SAP PM, in free, academic or evaluation versions. Testing is studied through real procedures for building certification bases and EMACC matrices, auditing EMAR 145 organisations and safety analysis of design changes. Assessment is continuous by module, plus the final Master's Thesis.
Standards covered: EMAR 21; EMAR 145; EMAR M; EMACC; MIL-HDBK-516C; STANAG 4671; SAE ARP4754A; DEF STAN 00-970.
Build it end to end
Your final project follows the real engineering workflow, step by step, reviewed by your tutor.
Where this takes you
Requirements
- A university degree in engineering, science or architecture, or equivalent demonstrable professional experience.
- An internet connection and a computer capable of running the programme software.
- English sufficient to read technical standards.
Ready to start?
Send your application today. Our admissions team replies within 72 hours with your study plan and funding options.
Frequently asked questions
The programme totals 1,900 hours over 12–14 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.
You work with IBM DOORS, AMOS (Swiss AviationSoftware), Isograph FaultTree+, MATLAB and SAP PM, using free, academic or evaluation versions. Your tutor indicates the free alternative wherever one exists.
A SEIUM Institute diploma, awarded on passing the continuous assessment and the Master's Thesis. It is SEIUM's own qualification, not an official state degree; its recognition depends on the programme completed and the regulations of each country.
Yes. Modules passed in a course or postgraduate diploma in the same area are recognised in the higher programme. Ask about the recognition policy when you enrol.
A university degree in engineering, science or architecture (or equivalent professional experience), a computer able to run the programme software and English sufficient to read technical standards.
Start dates are set by SEIUM's faculty for each intake. Our admissions team will confirm the next available date when you apply.
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