Module 6 Pipes and Unions.
Chapter 4/11: Corrosion (page 4.1 to 4.24).
Chapter 5/11: Fasteners (page 5.1 to 5.48).
Chapter 6/11: Pipes and Unions (page 6.1 to 6.14).
Chapter 7/11: Springs (page 7.1 to 7.8).
Chapter 8/11: Bearings (page 8.1 to 8.6).
Materials and Hardware (4164 Questions)
Sample – Materials Exams ( 40 questions 30 min),
Category A – Materials and Hardware Exams ( 52 questions 65 min),
Category B1 – Materials and Hardware Exams ( 72 questions 90 min),
Category B2 – Materials and Hardware Exams ( 60 questions 75 min),
Category B3 – Materials and Hardware Exams ( 60 questions 75 min),
EASA Part 66 Module 6 Book Forum
Module 6: Materials and Hardware
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EASA Part 66 Module 6 PDF Content:
MATERIAL IDENTIFICATION Before making repairs to any aircraft tubing, it is important to make accurate identification of tubing materials easa part 66 module 6 pdf. Aluminum alloy, steel, or titanium tubing can be identified readily by sight where it is used as the basic tubing material. However, it is difficult to determine whether a material is carbon steel or stainless steel, or whether it is 1100, 3003, 5052-0, 6061-T6 or 2024-T3 aluminum alloy. To positively identify the material used in the original installation, compare code markings of the replacement tubing with the original markings on the tubing being replaced.
On large aluminum alloy tubing, the alloy designation is stamped on the surface. On small aluminum tubing, the designation may be stamped on the surface; but more often it is shown by a color code, not more than 4″ in width, painted at the two ends and approximately midway between the ends of some tubing. When the band consists of two colors, one half the width is used for each color. easa part 66 module 6 pdf
If the code markings are hard or impossible to read, it may be necessary to test samples of the material for hardness by hardness testing. easa part 66 module 6 pdf