CCOG for AMT 212 Winter 2025


Course Number:
AMT 212
Course Title:
Sheet Metal
Credit Hours:
4
Lecture Hours:
0
Lecture/Lab Hours:
90
Lab Hours:
0

Course Description

Covers methods for sheet metal repairs to aircraft and methods of forming repair parts for damaged aircraft. Prerequisites: AMT 102, AMT 203, AMT 204, AMT 105, AMT 106 and AMT 107. Audit available.

Addendum to Course Description

This course is part of a Program designed to meet some of the requirements of the Code of Federal Regulations (CFR) for certification of Aviation Mechanics, and approved by the Federal Aviation Administration (FAA). Upon completion of the Program the student should be able to:

  1. Meet the applicable Degree and/or Certificate Outcomes identified in the document found at www.pcc.edu/degree-outcomes/amt as appropriate to coursework level completed.
  2. Successfully complete FAA Knowledge testing, as identified in the following documents, as appropriate:
    1. 14 CFR Part 65—Certification: Airmen Other Than Flight Crewmembers
    2. FAA Airman Knowledge Testing Matrix
      (Currently available at www.faa.gov/training_testing/testing/testing_matrix)
    3. FAA Order 8080.6H (or latest revision)—Conduct of Airman Knowledge Tests
  3. Successfully complete FAA Oral and Practical (knowledge and skill) testing, as identified in the following documents, as appropriate:
    1. FAA-S-ACS-1 (or latest revision)—Aviation Mechanic General, Airframe, and Powerplant Airman Certification Standards (ACS)
      (Currently available at www.faa.gov/training_testing/testing/acs)
    2. FAA-G-ACS-1 (or latest revision)—Companion Guide to the Aviation Mechanic ACS
    3. 14 CFR Part 65—Certification: Airmen Other Than Flight Crewmembers

Intended Outcomes for the course

Upon completion of the course students will be able to:

  1. Identify and apply computation skills and interpret drawings and instructions for the preparation of aircraft structural repairs and alterations.
  2. Identify and use appropriate aircraft sheet metal hand and shop tools during the preparation and fabrication of aircraft structural repair parts.
  3. Select and install various sizes of conventional rivets and special fasteners using proper preparation and technique.
  4. Identify and apply acceptable methods, techniques and practices during the assembly and repair of aircraft sheet metal structures.

Course Activities and Design

Concepts, knowledge, and theory will be introduced through a variety of methods including lecture, discussions, and demonstration sessions, supported by written instructional materials. Supervised lab and shop projects will give participants the opportunity to receive guided instruction, engage in “hands-on” skill and proficiency development, and gain experience in the methods, techniques, and practices that are acceptable to the FAA and commonly utilized in the aerospace industry.
Courses are designed to prepare students with the knowledge and skills necessary to be successful in the testing required for FAA certification of Aviation Maintenance Technicians, as well as entry-level employment in the industry.

The assignment of four credit hours to this course indicates that students will be involved with the course content for approximately 120 hours. Class participants will be expected to invest time outside of the official scheduled class hours in their efforts to master the course content. For this course to be creditable toward the FAA-authorized Certificate of Completion, the total hours recorded for the course must not be less than 90% of the hours offered during the module (typically 90 hours). Material missed by students during allowed absence will be made available to them in one or more ways, as selected by the instructor. The student is responsible for checking with the instructor following any absence, and for accessing the missed material that is made available.

Outcome Assessment Strategies

Evaluation methods include written and oral testing, attendance and class participation, and satisfactory completion of class projects. Evaluations and assessments will be conducted in accordance with guidelines published by the FAA (including, but not limited to, the documents identified in the Addendum to Course Description section of this CCOG), as well as applicable PCC policies and grading standards. A letter grade of “C” (minimum 76%) or higher is required for this course to be creditable toward the FAA-authorized Certificate of Completion.

Course Content (Themes, Concepts, Issues and Skills)

This course is designed to comply with FAA requirements for content including, but not limited to, those identified in the Addendum to Course Description section, and principally outlined in the Aviation Mechanic Airman Certification Standards (FAA-S-ACS-1). The following subject matter areas refer to that document.

II.A. – Metallic Structures
  • Select, install, and remove special fasteners for metallic structures.
  • Inspect and repair sheet-metal structures.
  • Install conventional rivets.
  • Form, lay out, and bend sheet metal.

Related Instruction

Computation
Hours: 28

  1. Identify and apply computation skills and, interpret drawings and instructions, for the preparation of aircraft structural repairs and alterations.
  2. Identify and use appropriate aircraft sheet metal hand and shop tools during the preparation and fabrication of aircraft structural repair parts.

  1. Direct instruction, student skill development, and practice in:

    1. Repair layout design, including fastener layout location and limits or tolerances.

    2. Aluminum forming, layout, and bending design; special attention is directed at the geometry of metal bending and required calculations.

    3. Measuring, cutting, or trimming aluminum stock to size per instructions within tolerances for various repair methods.

    4. Locating and drilling holes per instructions within tolerances for various repair methods.

  2. Read and interpret graphs, charts, and tables, and perform interpolation of chart/graph data to calculate and obtain values (required dimensions, radii, tolerances, etc.) in projects and during in-class exercises.

  3. Calculate appropriate dimensions and tolerances from drawings and data in manufacturer or governmental publications in preparation of creating a new drawing or sketch.

Human Relations
Hours: 5

4. Identify and apply acceptable methods, techniques and practices during the assembly and repair of aircraft sheet metal structures.

  1. Direct instruction related to aircraft repair evaluation and available repair options with special emphasis given to customer input and relationships, manufacturer approved repair methods, and FAA-required documentation and approvals.