PSA Airlines Canadair Regional Jet Systems (PSA-CRJ) Practice Exam

What triggers the bungee breakout mechanism to transfer control of multifunction spoilers?

1. When landing gear is in motion

2. When detecting a PCU runaway

3. When one engine fails

4. When cruising altitude is reached

The correct answer is: When detecting a PCU runaway

The bungee breakout mechanism is specifically designed to transfer control of the multifunction spoilers in response to a recognition of a power control unit (PCU) runaway. When a runaway is detected, the bungee mechanism engages to ensure that the aircraft maintains optimal control and stability by reallocating the functionality of the spoilers. This helps in preventing potential issues that could arise from a malfunctioning PCU, ensuring a safer and more controlled flight environment. The other scenarios presented do not directly initiate the bungee breakout mechanism. The motion of the landing gear, an engine failure, or reaching cruising altitude do not inherently involve the control dynamics of the multifunction spoilers or the need for a safety-switching mechanism like the bungee system. Therefore, recognizing a PCU runaway is the critical condition that prompts the correct response of transferring spoiler control to maintain aircraft performance.