Question: Task 0 4 - Load and stress Calculation the load lost Doubler strength Margin of Safety Stress check Net tension Shear out Buckling Crippling Fasteners

Task 04- Load and stress
Calculation the load lost
Doubler strength
Margin of Safety
Stress check
Net tension
Shear out
Buckling
Crippling
Fasteners shears (number of fasteners)
Task 05- Repair life
Based on the stress analysis, establish the life of the repair and the inspection interval
Task 06- Repair Instruction
Write instruction to embody the repair onto aircraft, the instruction must have;
Damage inspection, removal
Fabrication of repair parts
Preparation for installation
Installation
Inspection
Task 07- Repair Approval (Part 21 Subpart M)
Review CAAM Part 21 Subpart M
Develop compliance matrix for Part 21 Subpart M
Letter to CAAM
Complete package for approval
Task 0 4 - Load and stress Calculation the load

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