EASA PART 66 Module 6 Part 2 Material and Hardware , Non-Ferrous,Composite and Non-Metallic

MODULE 6. MATERIALS AND HARDWARE LEVEL Part 2

6.2 Aircraft Materials — Non-Ferrous(b)

Testing of non-ferrous material for hardness, tensile strength, fatigue strength and impact resistance.

6.3 Aircraft Materials - Composite and Non- Metallic(a)

• Characteristics, properties and identification of common composite and nonmetallic materials, other than wood, used in aircraft;
• Sealant and bonding agents.