Week 1: Aircraft Electrical Systems Demonstrates understanding of:
Generators, DC generation systems, and DC power distribution systems, Alternators, AC generation systems, and AC power distribution systems, starter generators, Constant Speed Drive (CSD) and Integrated Drive Generator (IDG) systems and components, voltage regulators and over-volt and overcurrent protection, inverter systems, aircraft wiring sizes, types, selection, and installation, de-rating factors in switch selection, aircraft wiring shielding, aircraft lightning protection, aircraft bonding and protection, aircraft lighting systems, electrical system troubleshooting, soldering preparation, types of solder, and/or flux usage, aircraft electrical connectors, splices, terminals, and switches, electrical system measurement, adjustment, or testing, and aircraft battery troubleshooting and maintenance.
Ability to identify, assess, and mitigate risks, encompassing:
Failure to use caution when testing/troubleshooting electrical systems or components, hazards associated with connecting or disconnecting external power, hazards associated with performing maintenance on energized circuits/systems, failure to use caution when performing maintenance in areas containing aircraft wiring, improperly routing and securing wires and wire bundles, failure to use the correct size wire in an electrical circuit, hazards created by incorrect selection or installation of wire terminals, hazards associated with soldering, and failure to observe safety precautions and practices when soldering.
Demonstrates ability to:
Inspect aircraft wiring to verify installation and routing, perform wire terminating and splicing, assemble an aircraft electrical connector, use a wiring circuit diagram to identify components, solder aircraft wiring, troubleshoot an airframe electrical circuit, install airframe electrical wiring, switches, or protective devices, secure wire bundles, determine an electrical load in a given aircraft system, install bonding jumpers, check output voltage of a DC generator, check the resistance of an electrical system component, inspect generator brush serviceability and brush spring tension, inspect and check anti-collision, position, and/or landing lights for proper operation. Inspect components in an electrical system, troubleshoot a DC electrical system supplied by an AC electrical system, identify components in an electrical schematic where AC is rectified to a DC voltage, perform a continuity test to verify the condition of a conductor, perform a test on a conductor for a short to ground, perform a test on a conductor for a short to other conductors, and troubleshoot an electric fault.
Week 2:
Continued from Week 1
Week 3:
Continued from Week 2
Week 4:
Continued from Week 3
Week 5:
Continued from Week 4
Week 6:
Continued from Week 5
Week 7:
Demonstrates understanding of:
Annunciator indicating systems and the meaning of warning, caution, and advisory lights, magnetic compass operation, magnetic compass swinging procedures, pressure indicating instruments, temperature indicating instruments, position indication sensors and instruments, gyroscopic instruments, direction indicating instruments, instrument pneumatic systems, pitot static system, fuel quantity indicating systems, instruments range markings, electronic displays, electrostatic sensitive devices, built in test equipment, electronic flight instrument system, engine indication and crew altering system, heads-up guidance system,14 CFR parts 43 and/or 91 requirements for static system leak checks, instrument limitations and conditions, transponder/encoder system, angle of attack and stall warning systems, takeoff and landing gear configuration warning systems, and aircraft bonding and protection.
Ability to identify, assess, and mitigate risks, encompassing:
Misuse of pressurized air and/or water during maintenance or cleaning of aircraft instrument systems, inappropriate or no action in response to a reported intermittent warning or caution annunciator light illumination, failure to observe safety precautions when performing maintenance on equipment identified as electrostatic sensitive, mishandling of mechanical gyros or instruments containing mechanical, and failure to observe precautions when performing pitot/static systems test to prevent instrument damage.
Demonstrates ability to:
Perform a static system leak test, remove and install an instrument, install range marks on an instrument glass, determine barometric pressure using an altimeter, check for proper range markings on an instrument, inspect a magnetic compass, locate the procedures for troubleshooting a vacuum operated instrument system, select proper altimeter for installation on a given aircraft, identify exhaust gas temperature system components, inspect a vacuum system filter for serviceability, adjust gyro/instrument air pressure/vacuum, inspect an aircraft’s alternate air (static) source, locate the adjustment procedures for a stall warning system, and inspect outside air temperature gauge for condition and operation
Fall Break October 13-17 (2025)
Week 8:
Continued from Week 7
Week 9:
Demonstrates understanding of:
Annunciator indicating systems and the meaning of warning, caution, and advisory lights, magnetic compass operation, magnetic compass swinging procedures, pressure indicating instruments, temperature indicating instruments, position indication sensors and instruments, gyroscopic instruments, direction indicating instruments, instrument pneumatic systems, pitot static system, fuel quantity indicating systems, instruments range markings, electronic displays, electrostatic sensitive devices, built in test equipment, electronic flight instrument system, engine indication and crew altering system, heads-up guidance system,14 CFR parts 43 and/or 91 requirements for static system leak checks, instrument limitations and conditions, transponder/encoder system, angle of attack and stall warning systems, takeoff and landing gear configuration warning systems, and aircraft bonding and protection.
Ability to identify, assess, and mitigate risks, encompassing:
Misuse of pressurized air and/or water during maintenance or cleaning of aircraft instrument systems, inappropriate or no action in response to a reported intermittent warning or caution annunciator light illumination, failure to observe safety precautions when performing maintenance on equipment identified as electrostatic sensitive, mishandling of mechanical gyros or instruments containing mechanical, and failure to observe precautions when performing pitot/static systems test to prevent instrument damage.
Demonstrates ability to:
Perform a static system leak test, remove and install an instrument, install range marks on an instrument glass, determine barometric pressure using an altimeter, check for proper range markings on an instrument, inspect a magnetic compass, locate the procedures for troubleshooting a vacuum operated instrument system, select appropriate altimeter for installation on a given aircraft, identify exhaust gas temperature system components, inspect a vacuum system filter for serviceability, adjust gyro/instrument air pressure/vacuum, inspect an aircraft’s alternate air (static) source, locate the adjustment procedures for a stall warning system, and inspect outside air temperature gauge for condition and operation.
Week 10:
Continued from Week 9
Week 11:
Continued from Week 10
Week 12:
Continued from Week 11
Week 13:
Continued from Week 12
Week 14: Finals Week (Note: there is no finals week during the Summer Semester, and the exam will be moved up)