Airframe Loading

Question 1

The vertical force where the structure will fail is called?

Answer 1

• G loading
• Ultimate Load

Question 2

A Light wing is more susceptable to?

Answer 2

Aerodynamic Flutter

Question 3

What is MZFM?

Answer 3

Max permissible aircraft weight disregarding fuel. This should neve be exceeded in flight or on the ground.

Question 4

Load between ultimate load and limit load will cause?

Answer 4

Perminent deformation but should not lead to perminant damage.

Question 5

Metal fatigue is a result of?

Answer 5

Cumulative forces applied and removed in a load causing catastrophic failure.

Question 6

What is ultimate stress?

Answer 6

The fail point of a single application on a static load.

Question 7

Fuel left in the wing will reduce?

Answer 7

• Aerodynamic flutter
• Forces applied to the centre box or wing route

Question 8

Where is the max load on a wing?

Answer 8

At the wing route.

Question 9

Damage tolerant or fails safe allows?

Answer 9

Allow a system to fail until discovered durin the next inspection

Question 10

While an aircraft is in the air and on the ground what stress does the wing endure?

Answer 10

• Compression
• Tension

Question 11

The safety factor between the limit laod and ultimate load is?

Answer 11

+ or - 1.5

Question 12

The maximum taxi (ramp) mass is governed by?

Answer 12

Structural Considerations

Question 13

How much are children considerd to weigh in standard values on all types of aircraft?

Answer 13

35 Kg