Structure: Name the different sub-assemblies of the structure
(Instruction Manual - Basic 1 - Main Systems, Chapter 2, Paragraph 2.1.1)

Structure: What is the structural design of the body structure?
Designed as a Rigig Hexahedron
It supports:
(Instruction Manual - Basic 1 - Main Systems, Chapter 2, Paragraph 2.2)

Structure: How is the bottom structure and cabin floor attached to the body structure?
By two beams
(Instruction Manual - Basic 1 - Main Systems, Chapter 2, Paragraph 2.3)

Structure: In which direction does the horizontal stabilizer produces lift?
Downward - in order to create a more comfortable attitude during flight
(Instruction Manual - Basic 1 - Main Systems, Chapter 2, Paragraph 2.2)
Structure: What is the purpuse of the step on the left hand side of the horizontal stabilizer?

To create more downward lift on the left hand side of the horizontal stabilizer, by providing a more cambered profile - thus counteracting the right skid low attitude.
(Instruction Manual - Basic 1 - Main Systems, Chapter 2, Paragraph 2.7.1)

Structure: What is the purpose for the different aerodynamic design of the upper and lower vertical fin?
Upper vertical fin (cambered profile)
Lower vertical fin (symmetrical profile)
(Instruction Manual - Basic 1 - Main Systems, Chapter 2, Paragraph 2.7)
Structure: How is the landing gear cross tube attached to the aircraft?
Structure: What is the purpose of the steel stribs bent downwards extending at the rear part of the skid?
Prevent ground resonance
(Instruction Manual - Basic 1 - Main Systems, Chapter 2, Paragraph 2.10.3)
Structure: How many anti-vibration devices is installed in the aircraft?
3