True or False: Pressure for the anti-G system is supplied by the electrically driven pump.

True or False: Pressure for the anti-G system is supplied by the electrically driven pump.

• A. True
• B. False
• C. Only during high-G maneuvers
• D. Depends on hydraulic status

Answer: (B)

The correct assertion is that pressure for the anti-G system is not supplied by an electrically driven pump. In the context of the T-6 aircraft, the anti-G system is powered by hydraulic pressure, which is generated by the aircraft's hydraulic systems rather than relying solely on an electrically driven pump. This hydraulic system is crucial for providing the necessary pressure to operate the anti-G garments that help maintain blood flow to the brain during high-G maneuvers, thereby preventing G-induced Loss Of Consciousness (GLOC). The design of the T-6 ensures that it uses the structural hydraulic system for such critical functions rather than an additional system that would depend on electrical input, which may be less reliable during certain operational scenarios. Understanding this aspect is important for comprehending the overall function and reliability of anti-G systems during flight operations.

The correct assertion is that pressure for the anti-G system is not supplied by an electrically driven pump. In the context of the T-6 aircraft, the anti-G system is powered by hydraulic pressure, which is generated by the aircraft's hydraulic systems rather than relying solely on an electrically driven pump. This hydraulic system is crucial for providing the necessary pressure to operate the anti-G garments that help maintain blood flow to the brain during high-G maneuvers, thereby preventing G-induced Loss Of Consciousness (GLOC).

The design of the T-6 ensures that it uses the structural hydraulic system for such critical functions rather than an additional system that would depend on electrical input, which may be less reliable during certain operational scenarios. Understanding this aspect is important for comprehending the overall function and reliability of anti-G systems during flight operations.