- An Aircraft B737 800 T Stiffener Beam Located In The Forward Cargo Hole Was Found Damaged Due To Impact The Damaged Por 1 (72.89 KiB) Viewed 15 times
An Aircraft B737-800 T-Stiffener beam located in the forward cargo hole was found damaged due to impact. The damaged por
-
answerhappygod
- Site Admin
- Posts: 899604
- Joined: Mon Aug 02, 2021 8:13 am
An Aircraft B737-800 T-Stiffener beam located in the forward cargo hole was found damaged due to impact. The damaged por
An Aircraft B737-800 T-Stiffener beam located in the forward cargo hole was found damaged due to impact. The damaged portion of the T-Stiffener was completely removed by splicing where the removed section is shown as green shaded area in the following figure. The details of affected T-Stiffener are also illustrated in the following figure. Given DATA of AL7075-T6 Strength of Bearing Ultimate =32KSI or 32000Ibff22 Strength of Shear Ultimate =38KSI or 38000Ibfin2 Strength of Tensile Ultimate =78KSI or 78000Jbf′in2 Question 1.1 (10 Marks) Determine the total load loss of the affected T-Stiffener Beam's removed section for repair. Question 1.2 (5 Marks) If the prepared material is not available in stock, discuss the alternative materials that can be used as a repaired part to avoid corrosion. Question 1.3 (10 Marks) What is the preferred material and total cross-sectional thickness of your repaired nart And Explain why have you chosen the material specifications as answered above?
Join a community of subject matter experts. Register for FREE to view solutions, replies, and use search function. Request answer by replying!