6C003E - Aircraft Systems and Structural Integration 01 Sep 2026 - 31 Aug 2032 | Version 0
Associated Module Information
| Module Code: | 6C003E | ||
|---|---|---|---|
| Module Title: | Aircraft Systems and Structural Integration | ||
| Faculty: | Faculty of Computing, Engineering and Science | ||
| Faculty Group: | Engineering | ||
| Faculty Sub Group: | Aircraft Maintenance Engineering | ||
| Module Leader: | |||
| Module Team: | Bethan Llewellyn | ||
| First Intended Intake: | SEP 2026 | Final Year of Intake: | 2031 |
| Date Closed: | |||
| Credit Value: | 40 | Credit Level: | 6 |
| Language: | English | ||
| Percentage of Module Taught in Welsh: | 0 | ||
| Equivalent Module: | |||
| HECOS codes: | 100163 - electrical and electronic engineering | ||
| HECOS Code Weighting: | 100 | ||
Document Version Information
| Version | 0 |
|---|---|
| Valid From | 01 Sep 2026 |
| Valid To | 31 Aug 2032 |
Module Aims
To enable students to critically analyse and evaluate the aerodynamic principles, aircraft systems and structural behaviours that underpin modern aeronautical engineering practice, applying advanced theoretical knowledge to complex maintenance and operational scenarios. Students will develop the ability to interpret system interactions, assess structural integrity and make informed engineering judgements that support safe, compliant and effective aircraft performance.
Content Summary
This module develops an advanced understanding of aircraft aerodynamic behaviour, structural design principles and the operation of major mechanical and avionic systems found on large gas turbine aircraft. Students examine subsonic, transonic and supersonic aerodynamic characteristics, together with the function, integration and performance implications of primary and secondary flight controls. Structural study encompasses fuselage, wing and stabiliser construction, modern manufacturing methods, and the analysis of load paths, failure modes and structural integrity. Learners also explore cabin furnishings, interior systems and legislatively mandated safety equipment.
The module further investigates the architecture and operation of key mechanical systems, including pneumatic supply, fire protection, low-pressure fuel systems, hydraulics and landing gear assemblies. Avionic coverage includes aircraft instrumentation, electrical power generation and distribution, lighting systems, integrated modular avionics, onboard maintenance systems, cabin management systems and aircraft information systems. Throughout, emphasis is placed on system interdependence, diagnostic reasoning and the application of engineering judgement to complex operational and maintenance scenarios.
Learning and Teaching Methods
| Activity Type | Hours |
|---|---|
| Lecture | 84 |
| Tutorial | 12 |
| Independent Study | 204 |
| Directed Study | 100 |
| Total Hours Selected | 400 |
Learning Outcomes
| # | Learning Outcome |
|---|---|
| LO1 | Critically evaluate aerodynamic behaviours, aircraft structural design principles, and the performance characteristics of major mechanical and avionic systems, demonstrating an advanced understanding of how these factors interact to influence aircraft operation, integrity and safety. |
| LO2 | Apply specialist analytical and diagnostic techniques to complex, authentic maintenance and operational scenarios, interpreting system data, assessing structural and system faults, and formulating evidence-based engineering judgements that support safe and compliant aircraft performance. |
Module Requisites
N/A
Assessment Criteria
| Assessment Category | Assessment Type | Description | Duration | Word Count | Weight (%) | Best of? | Pass Mark |
|---|---|---|---|---|---|---|---|
| Asynchronous Assessment | Essay | Written report based on a mechanical subject | 0 | 3500 | 50 | No | 40 |
| Asynchronous Assessment | Essay 1 | Written report based on an Avionic subject | 0 | 3500 | 50 | No | 40 |
Assessment Matrix
| Assessment Type | Learning Outcomes | ||
|---|---|---|---|
| LO1 | LO2 | ||
| Essay | ✔ | ✔ | |
| Essay 1 | ✔ | ✔ | |