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Course Details
KTO KARATAY UNIVERSITY
School of Applied Sciences
Programme of School of Applied Sciences
Course Details
Course Code Course Name Year Period Semester T+A+L Credit ECTS
04050103 Aircraft General Knowledge II 3 Autumn 5 66+0+0 3 3
Course Type Compulsory
Course Cycle Bachelor's (First Cycle) (TQF-HE: Level 6 / QF-EHEA: Level 1 / EQF-LLL: Level 6)
Course Language Turkish
Methods and Techniques -
Mode of Delivery Face to Face
Prerequisites -
Coordinator SAFFET ÖZGÜN
Instructor(s) -
Instructor Assistant(s) -
Course Content
SYSTEM COMPONENTS, DESIGN, OPERATION, SYMPTOMS AND WARNINGS, GROUND/FLIGHT GUARDS, EMERGENCY RELEASE SYSTEMS
Objectives of the Course
THE STUDENT HAS GENERAL INFORMATION ABOUT AIRCRAFT – COMMITTEE TO BODY/SYSTEMS/ENGINE SYSTEMS
Contribution of the Course to Field Teaching
Basic Vocational Courses X
Specialization / Field Courses X
Support Courses
Transferable Skills Courses
Humanities, Communication and Management Skills Courses
Relationships between Course Learning Outcomes and Program Outcomes
Relationship Levels
Lowest Low Medium High Highest
1 2 3 4 5
# Program Learning Outcomes Level
P9 To have knowledge of aircraft design, performance, and operational characteristics. 5
Course Learning Outcomes
Upon the successful completion of this course, students will be able to:
No Learning Outcomes Outcome Relationship Measurement Method **
O1 Defines the basic components of aircraft design and lists the main parts of aircraft. P.9.1 1
O2 Assesses whether an aircraft design is suitable for a particular use or purpose. P.9.4 1
O3 Analyzes the impact of various components in aircraft design on overall performance. P.9.6 1
** Written Exam: 1, Oral Exam: 2, Homework: 3, Lab./Exam: 4, Seminar/Presentation: 5, Term Paper: 6, Application: 7
Weekly Detailed Course Contents
Week Topics
1 AIRCRAFT GENERAL INFORMATION – BODY/SYSTEMS/ENGINE
2 SYSTEM DESIGN, LOADS, STRESSES, MAINTENANCE
3 MAINTENANCE METHODS: DEPENDING ON TIME AND SITUATION
4 HYDRAULICS
5 LANDING GEAR, WHEELS, TIRES AND BRAKES
6 FLIGHT CONTROLS
7 PNEUMATIC – PRESSURIZATION AND VENTILATION SYSTEMS
8 ANTI-ICING AND DE-ICING SYSTEMS
9 FUEL SYSTEM
10 RECIPROCATING ENGINES
11 TURBINE ENGINES
12 PROTECTION AND DETECTION SYSTEMS
13 OXYGEN SYSTEMS
14 PREPARATIONS TO THE FINAL EXAM
Textbook or Material
Resources SHGM
Evaluation Method and Passing Criteria
In-Term Studies Quantity Percentage
Attendance - -
Practice - -
Field Study - -
Homework - -
Presentation - -
Projects - -
Quiz - -
Midterms - -
Final Exam 1 100 (%)
Total 100 (%)
ECTS / Working Load Table
Quantity Duration Total Work Load
Course Week Number and Time 1 66 66
Out-of-Class Study Time (Pre-study, Library, Reinforcement) 14 1 14
Midterms 0 0 0
Quiz 0 0 0
Homework 0 0 0
Practice 0 0 0
Laboratory 0 0 0
Project 0 0 0
Workshop 0 0 0
Presentation/Seminar Preparation 0 0 0
Fieldwork 0 0 0
Final Exam 1 10 10
Other 0 0 0
Total Work Load: 90
Total Work Load / 30 3
Course ECTS Credits: 3
Course - Learning Outcomes Matrix
Relationship Levels
Lowest Low Medium High Highest
1 2 3 4 5
# Learning Outcomes P9
O1 Defines the basic components of aircraft design and lists the main parts of aircraft. 5
O2 Assesses whether an aircraft design is suitable for a particular use or purpose. 5
O3 Analyzes the impact of various components in aircraft design on overall performance. 5