Subject area A of 15
Metallic Structures
5-15% of the A&P Airframe test, about 5 to 15 of the 100 questions. The FAA's test standard lists 17 knowledge elements and 5 risk management elements for this area. Here is every one, plus sample questions to try.
What the FAA tests
From the aviation mechanic test standard, FAA-S-ACS-1.
Knowledge: what you must know
- AM.II.A.K1Inspection/testing of metal structures.
- AM.II.A.K2Types of sheet metal defects.
- AM.II.A.K3Selection of sheet metal repair materials.
- AM.II.A.K4Layout, forming, and drilling of sheet metal components.
- AM.II.A.K5Selection of rivets, hardware, and fasteners for a sheet metal repair.
- AM.II.A.K6Heat treatment processes for aluminum.
- AM.II.A.K7Rivet layout.
- AM.II.A.K8Rivet removal and installation methods.
- AM.II.A.K9Maintenance safety practices/precautions for sheet metal repairs or fabrications.
- AM.II.A.K10Flame welding gases.
- AM.II.A.K11Storage/handling of welding gases.
- AM.II.A.K12Flame welding practices and techniques.
- AM.II.A.K13Inert-gas welding practices and techniques.
- AM.II.A.K14Purpose and types of shielding gases.
- AM.II.A.K15Types of steel tubing welding repairs.
- AM.II.A.K16Procedures for weld repairs.
- AM.II.A.K17Types of structures and their characteristics.
Risk management: hazards you must be able to spot and manage
- AM.II.A.R1Selection of repair materials.
- AM.II.A.R2Utilizing maintenance safety practices/precautions for sheet metal structures.
- AM.II.A.R3Use of PPE when working with sheet metal structures.
- AM.II.A.R4Handling, storage, and use of compressed gas bottles.
- AM.II.A.R5Use of electric welding equipment.
Try a sample question
Metallic Structures ยท AM.II.A.K5
The figure shows a countersunk rivet joining two sheets. In your repair the upper sheet is 0.040 inch thick, the lower sheet is 0.063 inch thick, and the rivet is 1/8 inch in diameter. What is the minimum length for the dimension marked 1?
Practice all of metallic structures
The full course has questions on every element listed here, with an explanation and FAA source for each.