4A011E - Theory of Flight Fundamentals for Aircraft Maintenance Engineers 01 Sep 2026 - 31 Aug 2032 | Version 0
Associated Module Information
| Module Code: | 4A011E | ||
|---|---|---|---|
| Module Title: | Theory of Flight Fundamentals for Aircraft Maintenance Engineers | ||
| Faculty: | Faculty of Computing, Engineering and Science | ||
| Faculty Group: | Engineering | ||
| Faculty Sub Group: | Aircraft Maintenance Engineering | ||
| Module Leader: | |||
| Module Team: | Bethan Llewellyn, Polly Blaikie, Andrew Carter, Nyam Nutalapati, Ward Broughton, Giuseppe Leogrande, Osama Siddique | ||
| First Intended Intake: | SEP 2026 | Final Year of Intake: | 2031 |
| Date Closed: | |||
| Credit Value: | 20 | Credit Level: | 4 |
| 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 introduce students to the fundamental principles of aerodynamics, theory of flight, airframe structures and aircraft systems, developing an understanding of the aircraft as an integrated engineering system.
To provide students with the foundational knowledge required to support safe working practices and undertake routine maintenance, basic functional checks and the identification of common defects within aircraft structures and systems.
Content Summary
This module introduces the physical principles that govern the atmosphere and aircraft aerodynamics, enabling students to develop an understanding of how lift, drag and controlled flight are generated and sustained. Core aerodynamic terminology and performance concepts are explored through the study of airflow behaviour, the forces acting on an aircraft in flight, aircraft stability, and the factors affecting flight performance.
The module examines the aerodynamic characteristics, construction and operation of primary and secondary flight controls, including high-lift and drag-producing devices, and considers their contribution to aircraft controllability and performance throughout different phases of flight. Students investigate the relationship between aerodynamic theory and aircraft design, developing an appreciation of how aerodynamic principles influence aircraft operation and maintenance.
Building on this foundation, the module introduces the basic structure of aircraft and the layout and operation of key aircraft systems. Students examine major airframe structural components and their functions, together with the principles of operation of common aircraft systems. Through the study of aircraft structures and systems as interconnected elements, students develop an understanding of the aircraft as an integrated engineering system and gain the knowledge required to support safe maintenance practices, routine inspections and the identification of common defects.
Learning and Teaching Methods
| Activity Type | Hours |
|---|---|
| Lecture | 42 |
| Tutorial | 6 |
| Independent Study | 92 |
| Directed Study | 60 |
| Total Hours Selected | 200 |
Learning Outcomes
| # | Learning Outcome |
|---|---|
| LO1 | Explain the physics of the atmosphere and the aerodynamic principles that enable sustained and controlled flight, using appropriate terminology to describe aircraft behaviour and performance. |
| LO2 | Analyse and compare the aerodynamic characteristics, functions and operational behaviour of flight controls and high-lift/drag devices, demonstrating a coherent understanding of core aerodynamics and theory of flight. |
Module Requisites
N/A
Assessment Criteria
| Assessment Category | Assessment Type | Description | Duration | Word Count | Weight (%) | Best of? | Pass Mark |
|---|---|---|---|---|---|---|---|
| Asynchronous Assessment | Project | Preliminary wing design consideration for unpowered flight project to include a group presentation | 10 | N/A | 50 | No | 40 |
| Synchronous Onsite Assessment | Classroom Test - Time Constrained (Onsite) | Closed Book Exam | 120 | N/A | 50 | No | 40 |
Assessment Matrix
| Assessment Type | Learning Outcomes | ||
|---|---|---|---|
| LO1 | LO2 | ||
| Project | ✔ | ✔ | |
| Classroom Test - Time Constrained (Onsite) | ✔ | ✔ | |