Master’s in Helicopter Certification and Testing Engineering
Online master's programme of 1,900 hours in helicopter certification and testing engineering, with 12 modules covering the CS-27/CS-29 and Part 21 framework, certification bases, structural, systems and powerplant certification, flight testing of performance and handling qualities, vibration and noise testing, military airworthiness and continuing airworthiness, with an assigned technical tutor.
Master’s in Helicopter Certification and Testing Engineering — studying from Australia
Defence is one of Australia's largest engineering employers, with major programmes in land systems, naval platforms, aircraft and integrated systems managed through the Department of Defence. Land systems engineering supports armoured vehicles, weapons and logistics equipment, often through prime contractors and local industry partners. Industry involvement is strongly encouraged through the Defence industry policy framework. Engineers work on sustainment, capability development, systems integration and safety assurance, typically in Canberra, Adelaide, Melbourne and regional defence precincts.
Fees for Australia: A$14,200 (AUD), with instalments and employer sponsorship available.
Relevant bodies in Australia
Typical roles
Questions from Australia
How does defence engineering recognition work in Australia?
Defence engineering in Australia is largely run through the Department of Defence and its industry partners, which set their own security clearance and qualification requirements. Engineers Australia is the professional body for accreditation. SEIUM's private qualifications are not accredited by these bodies, so recognition is for employers or the relevant body to decide.
Which Australian employers hire in defence and land systems?
Australia has defence prime contractors, the Department of Defence, and specialist land systems firms. Many of these roles require Australian security clearances, which depend on citizenship and background checks rather than course completion. Ask employers how they weigh private qualifications against experience and clearance requirements.
Is the course manageable with a job, and does it need a visa?
The programmes are 100% online and taught in English, so you can study from Australia without a student visa. Specialist courses take 300 hours, diplomas 800 and master's 1,900. An assigned technical tutor supports you, fees are payable in instalments, and employer sponsorship may be possible.
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
Apply the European and military rotorcraft certification framework.
Establish certification bases and compliance matrices.
Plan structural and systems certification.
Certify the powerplant and transmission.
Design and conduct flight tests with risk management.
Assess performance and handling qualities.
Manage continuing airworthiness.
Who it's for
- Certification engineers working on CS-27 and CS-29 programmes.
- Flight test engineers planning and analysing test campaigns.
- Continuing airworthiness engineers handling ADs, repairs and modifications.
- CS-29 compliance specialists preparing compliance matrices and documents.
- Test instrumentation engineers responsible for telemetry and data acquisition.
- Design organisation managers overseeing Part 21 approvals.
- Engineering or science graduates seeking to enter the aerospace industry.
What you'll work with
- CS-29 (EASA certification specifications for large rotorcraft)
- CS-27 (EASA certification specifications for small rotorcraft)
- Regulation (EU) 748/2012 (airworthiness certification, Part 21)
- Regulation (EU) 2018/1139 (common rules in civil aviation, EASA)
- ADS-33E-PRF (handling qualities requirements for military rotorcraft)
- EMAR 21 (European military airworthiness requirements)
- MIL-HDBK-516C (airworthiness certification criteria)
- ICAO Annex 16, Volume I (aircraft noise)
- MATLAB
- IADS (Curtiss-Wright)
- FLIGHTLAB
- MSC Nastran
- IBM DOORS
12 modules · 1900 h
1.1The European airworthiness system1.2Regulation (EU) 2018/11391.3Part 21: type certification1.4CS-27 and CS-29 specifications1.5FAA Part 27 and 29 certification1.6EMAR military airworthiness1.7Bilateral validation1.8Design and production organisations1.9Ethics and responsibility of the certifier1.10Case study: certification process of a light helicopter
2.1Establishing the certification basis2.2Special conditions2.3Equivalent levels of safety2.4Exemptions2.5Certification review items2.6Acceptable means of compliance2.7Compliance matrix2.8Compliance documents2.9Interaction with the authority2.10Practical: drafting a compliance matrix
3.1Flight and landing loads3.2Static testing3.3Fatigue and damage tolerance in rotorcraft3.4Life-limited dynamic components3.5Composite materials3.6Crashworthiness and seats3.7Bird strike3.8Lightning protection3.9Structural documentation3.10Lab: static test plan for a component
4.1System safety assessment4.2CS 29.1309 requirements4.3Functional hazard analysis4.4Fault tree analysis4.5Software and hardware4.6Electrical and hydraulic systems4.7Fuel systems4.8Fire protection4.9Emergency equipment4.10Case study: 1309 analysis of a hydraulic system
5.1CS-E engine certification5.2Engine installation5.3Transmissions and rotors5.4Transmission endurance testing5.5Operation with loss of lubrication5.6Category A and engine failure5.7Ice protection5.8Intakes and particles5.9Compliance documentation5.10Practical: loss-of-lubrication demonstration plan
6.1Flight test organisation6.2Test pilots and flight test engineers6.3Test instrumentation6.4Telemetry6.5Test planning6.6Risk management in testing6.7Test techniques6.8Data reduction6.9Test reports6.10Lab: analysis of data from a performance test
7.1Hover performance7.2Climb and maximum speed7.3Height-velocity diagrams7.4Autorotation7.5Category A performance7.6Take-offs and landings7.7Correction to standard conditions7.8Flight manual7.9Hot and high testing7.10Case study: height-velocity diagram from test data
8.1Static and dynamic stability8.2Controllability8.3Cooper-Harper rating scale8.4ADS-33 mission task elements8.5Flight with degraded systems8.6Crosswind and hover8.7Night and instrument operation8.8Autopilot testing8.9Workload assessment8.10Practical: assessment with the Cooper-Harper scale
9.1In-flight vibration testing9.2Flutter and aeroelastic stability testing9.3Ground resonance testing9.4Noise certification9.5Testing in icing conditions9.6Cold and hot weather testing9.7Electromagnetic compatibility9.8Cockpit lighting tests9.9Mission equipment testing9.10Workshop: noise certification plan
10.1Military airworthiness in Europe10.2EMAR 21 and its application10.3MIL-HDBK-516 as a reference10.4Certification of mission equipment10.5Use of civil certification credit10.6Acceptance testing10.7National military airworthiness authorities10.8Military continuing airworthiness10.9Ethics and oversight10.10Case study: certification strategy for a state version
11.1Instructions for continued airworthiness11.2Airworthiness directives11.3Occurrence reporting11.4Fleet monitoring11.5Modifications and repairs11.6Supplemental type certificates11.7Safety management in the design organisation11.8Lessons learned11.9Continuous improvement11.10Practical: analysis of an airworthiness directive
12.1Selection of the product or modification12.2Certification basis12.3Compliance matrix12.4Ground test plan12.5Flight test plan12.6Safety analysis12.7Test risk management12.8Conclusions12.9Master'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, making it compatible with work.
Each module combines theory, guided reading of the original standard and applied exercises. The working software is MATLAB, IADS (Curtiss-Wright), FLIGHTLAB, MSC Nastran and IBM DOORS, in free, academic or evaluation versions. Testing is studied through real procedures for flight test planning and analysis, drafting compliance matrices and structural and systems certification testing. Assessment is continuous by module, plus the final Master's Thesis.
Standards covered: CS-29, CS-27, Regulation (EU) 748/2012 (Part 21), Regulation (EU) 2018/1139, ADS-33E-PRF, EMAR 21, MIL-HDBK-516C and ICAO Annex 16 Volume I.
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
- University degree in engineering, science or architecture, or equivalent demonstrable professional experience.
- 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 MATLAB, IADS (Curtiss-Wright), FLIGHTLAB, MSC Nastran and IBM DOORS, 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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