1 Demonstrate understanding of materials commonly used in aircraft and their general application and heat treatment and metal working processes (AM.I.E.K1 & K2)
2 Demonstrate understanding of forces placed on aircraft materials (e.g., tension, compression, torsion, bending, strain, and shear) (AM.I.E.K3)
3 Demonstrate understanding of hardware commonly used in aircraft (e.g., bolts, nuts, screws, pins, washers, turnlock fasteners, cables, cable fittings, and rigid line couplings) (AM.I.E.K4)
4 Demonstrate understanding of safety wire and safety clip requirements and techniques and precision measurement tools, principles, and procedures (AM.I.E.K5 & K6)
5 Demonstrate understanding of soldering preparation, types of solder, and flux usage (AM.I.E.K7)
6 Demonstrate understanding of torqueing tools, principles, and procedures and suitability and compatibility of materials and hardware used for maintenance (AM.I.E.K8 & K9)
7 Demonstrate understanding of relationship between torque and fastener preload and identification markings on materials and hardware (AM.I.E.K10 & K11)
8 Demonstrate understanding of the characteristics of acceptable welds, characteristics of unacceptable welds, and procedures for weld repairs (AM.I.E.K12 - K14)
9 Demonstrate understanding of measuring tools, including calipers, micrometers, and gauges (AM.I.K.K1)
10 Demonstrate understanding of calibration and tool accuracy requirements and nondestructive testing (NDT) procedures and methods (AM.I.K.K2 & K3)
11 Demonstrate understanding of aircraft inspection programs (e.g. progressive, 100-hour, annual, and other FAA-approved inspections). (AM.I.K.K4)
12 Demonstrate understanding of aircraft inspection methods and tools for materials, hardware, and process (AM.I.K.K5)
13 Demonstrate the ability to identify, assess, and mitigate risks associated with the use of personal protective equipment (PPE) (AM.I.E.R1)
14 Demonstrate the ability to identify, assess, and mitigate risks associated with improper torque; used hardware or suspected unapproved parts (SUPS); and torqueing techniques on critical, highly-stressed fasteners (AM.I.E.R2 - R4)
15 Demonstrate the ability to identify, assess, and mitigate risks associated with demagnetizing a component following a magnetic particle inspection (AM.I.K.R1)
16 Demonstrate the ability to identify, assess, and mitigate risks associated with using precision measuring instruments; calibration of precision measuring equipment; and selection of inspection techniques (AM.I.K.R2 - R4)
17 Demonstrate the ability to identify, assess, and mitigate risks associated with damage prevention to aircraft components and test equipment using an ohmmeter. (AM.I.K.R5)
18 Demonstrate the ability to install safety wire on nuts, bolts, and turnbuckles (AM.I.E.S1)
19 Demonstrate the ability to determine and properly torque aircraft hardware (AM.I.E.S2)
20 Demonstrate the ability to inspect and check welds (AM.I.E.S3)
21 Demonstrate the ability to identify aircraft materials and hardware based on manufacturer's markings; and select and install bolts (AM.I.E.S4 & S5)
22 Demonstrate the ability to make precision measurements with an instrument that has a Vernier scale and check the concentricity of a shaft (AM.I.E.S6 & S7)
23 Demonstrate the ability to identify aircraft control cable components and fabricate a cable assembly using a swaged end fitting (AM.I.E.S8 & S9)
24 Demonstrate the ability to select the correct aluminum alloy for a structural repair; identify rivets by physical characteristics; and determine suitability of material and aircraft repairs (AM.I.E.S10 - S12)
25 Demonstrate the ability to distinguish between heat-treated and non-heattreated aluminum alloys (AM.I.E.S13)
26 Demonstrate the ability to check for proper calibration of a micrometer (AM.I.E.S14)
27 Demonstrate the ability to use Vernier calipers; use micrometers; and use measurement gauges (AM.I.K.S1 - S3)
28 Demonstrate the ability to perform a visual inspection; perform a dye penetrant inspection; inspect aircraft for compliance with an AD; identify NDT methods for composite, surface metal, and subsurface metal defects; and perform a tap test on a composite component (AM.I.K.S4 - S8)