Failure to close the engine bleed valves on the ___________ side of the manifold could cause damage to the airplane wing components due to escaping bleed air

Answer: malfunctioning

Application of hydraulic pressure to the main gear during manual extension may result in ___________

Answer: injury to operator

If the source of the leakage in the system cannot be determined, the hydraulic fluid quantity gauge for the affected system should be monitored during and after actuation of the crossover valve lever. If a fluid loss of the unaffected system is observed, return the _______ to _________

Answer: crossover; normal

It is safe to use the crossover valve after loss of fluid from either hydraulic system, provided pressure can be ________ and ________ in the affected system with the appropriate hydraulic pressure and aux pump switches on. When the LH system is affected, set the inboard spoiler switch to cut-off. When the RH system is affected set the CIPS generator switch to EMER and turn the rudder power switch to OFF

Answer: built up; maintained

Given: the left hydraulic pressure gauge indicates 1,800 psi with no other indications. You have determined that the accumulator preload is low and have repressurized the system. To check the actual system pressure, read the ____________ gauge by cycling the pilot's brakes

Answer: reserve brake

Given: the right hydraulic system pressure gauge indicates a sustained pressure of 3,550 psi with no indication of fluid loss or overhear. Immediately __________ the ______ system.

Answer: depressurize; right

Given: Loss of fluid in the right hydraulic system with no other indications, immediately depressurize the ________ system.

Answer: Right