Aircraft hydraulic systems rely on pressurized reservoirs to supply fluid continuously to flight control actuators. At high cruising altitudes, atmospheric pressure drops drastically, which can cause hydraulic pumps to cavitate—forming vapor bubbles that disrupt fluid flow—if reservoir pressure falls below a safe threshold. To prevent this hazard, maintenance protocols mandate routing compressed bleed air from the turbine engines into the reservoir tanks to maintain steady internal pressure throughout the flight.
Based on the passage, what is implied about the consequence of a failure in the bleed air pressurization system during high-altitude cruising?
- AMaintenance protocols would automatically adjust the threshold to restore normal fluid flow.
- The decreased external pressure would lead to vapor bubble formation inside the hydraulic pumps.Answer
- CThe hydraulic fluid would instantly freeze due to the loss of hot compressed engine air.
- DThe flight control actuators would route compressed bleed air directly into the turbine engines.
Answer
The decreased external pressure would lead to vapor bubble formation inside the hydraulic pumps.
The passage explains that low atmospheric pressure at high altitudes causes pump cavitation (the formation of vapor bubbles) unless engine bleed air keeps the reservoirs pressurized. Therefore, if the bleed air system fails at high cruising altitude, the lack of positive pressure will allow the low ambient pressure to cause vapor bubbles in the hydraulic pumps.
Step-by-Step Solution
Key Concept
Inferring unstated physical consequences from described system mechanisms
Estimated Time:1m 0s