The Static Bypass Switch for the PILOT'S/NO. 2 static system is located on which panel?

The Static Bypass Switch for the PILOT'S/NO. 2 static system is located on which panel?

• A. Avionics Rack Panel
• B. Center Console Panel
• C. Pilot's Switch Panel
• D. Electrical Panel

Answer: (A)

The main idea here is where the air data/avionics wiring for the PILOT’S and No. 2 static systems is managed, and where a switch that bypasses that pathway would logically be placed. The Static Bypass Switch for these static sources is located on the Avionics Rack Panel because that panel houses the air data/avionics hardware it controls. Having the switch on the Avionics Rack Panel provides direct access to the static pressure sources and their associated avionics circuitry, allowing quick isolation or bypass when faults are detected or during testing. The other panels serve different functions (controls and displays, or power/electrical distribution), so they aren’t the appropriate locations for this specific switch.

The main idea here is where the air data/avionics wiring for the PILOT’S and No. 2 static systems is managed, and where a switch that bypasses that pathway would logically be placed. The Static Bypass Switch for these static sources is located on the Avionics Rack Panel because that panel houses the air data/avionics hardware it controls. Having the switch on the Avionics Rack Panel provides direct access to the static pressure sources and their associated avionics circuitry, allowing quick isolation or bypass when faults are detected or during testing. The other panels serve different functions (controls and displays, or power/electrical distribution), so they aren’t the appropriate locations for this specific switch.