ZS-001 / REV. 0220-02

20-02
FAA Airframe Aileron Fabrication Project

Overview

An airframe training project combining aluminum fabrication, fiberglass layup, structural riveting and documented repairs.

Riveted aileron skin with repair patches
FIGURE 01 — Riveted aileron skin with repair patches

Objective

The goal of the project was to design and construct a structurally sound aileron using both aluminum and composite materials, following FAA standards used in airframe mechanic training. After fabricating the control surface, I was required to create intentional damage and then perform FAA approved repairs, including full documentation and a completed FAA Form 337 (Major Repair and Alteration).

Engineering constraints

Aluminum and composite construction; intentional damage followed by documented repairs; rivet pitch, edge distance and rivet-count calculations; and a completed FAA Form 337.

My contributions

To demonstrate repair competency, I intentionally damaged both the aluminum and composite skins and performed the following FAA-approved repair types:

For each repair, I calculated rivet pitch, edge distance, and total rivet count to ensure FAA compliance.
I also:

Design and fabrication process

Fabrication Process

Metal Components

Composite Components

Assembly

Results

The completed aileron passed all dimensional, structural, and alignment inspections, demonstrating correct material handling, precision assembly, and proper execution of aluminum and composite repair techniques.

This project gave me extensive hands on experience with:

It strengthened my understanding of both traditional and modern aerospace manufacturing and repair processes, reflecting the exact skills used daily by licensed airframe mechanics.

Skills and tools

Aircraft Sheet-Metal Forming, Composite Layup & Repair, Heat Treatment, Technical Drawing, Pneumatic Riveting, FAA Compliance & Inspection, Structural Fabrication, Precision Assembly