Name: Structural Repair for Engineers - Part II
Description:
This course is a continuation of the Aircraft Structural Repair for Engineers Part I course. It focuses on the design of repairs to structure loaded in compression. Concepts of bending and column stability will be discussed. Repairs to airplane structural members will be analyzed for beam bending, buckling and crippling failure modes.
Objectives: This course satisfies ATA 104 Level IV objectives. Upon completion of the course, the students will be able to: Analyze beam structural repairs for bending. Analyze structural repairs for Euler column and inter-fastener buckling failure modes. Analyze structural repairs for crippling and Johnson-Euler column failure modes. Apply Part I and Part II analysis methods to the design of typical floor beam repairs.
Prerequisites: 462 Designing Repairs with the Boeing Heritage Structural Repair Manual. 463 Structural Repair for Engineers Part I. Engineering degree or equivalent experience.
Duration: 5 training days