The system bypass valve is: A) Spring-loaded closed. B) Spring-loaded open. C) Energized closed. D) Both B and C.
Depressing an ENG FIRE switch light: A) Shuts off hydraulic fluid to the pump B) Trips the generator field relay C) Arms the fire-extinguishing system. D) All of the above.
Closing of a hydraulic firewall shutoff valve is indicated by: A) A warning horn. B) Illumination of the applicable F/W SHUTOFF annunciator if the fuel shutoff valve also closes. C) Illumination of the HYD PRESS annunciator. D) None of the above.
If electrical power is lost, the system by-pass valve: A) Spring-loads to the closed position B) Is not affected. C) Spring-loads to the open position. D) None of the above.
The main hydraulic system provides pressure to operate the: A) Landing gear, speedbrakes, and thrust reversers. B) Landing gear and speedbrakes only (all airplanes) C) Antiskid brakes, landing gear, and flaps. D) Speedbrakes, landing gear, and wheel brakes.
The reservoir quantity indicator is located: A) In the right forward baggage compartment. B) On the copilot´s instrument panel. C) On the right engine near of the oil filter. D) In the tail cone area.
Reservoir fluid level below 0.2 gallon is indicated by illumination of the: A) L or R LO HYD LEVEL annunciator. B) HYD PRESS annunciator. C) LO HYD LEVEL annunciator. D) L or R LO HYD FLOW annunciator.
Hydraulic system operation is indicated by illumination of the: A) LO HYD LEVEL annunciator. B) HYD PRESS annunciator. C) L or R LO HYD LEVEL annunciator. D) L or R LO HYD FLOW annunciator.
Of the followings statements concerning the hydraulic system, the correct one is: A) The HYD PRESS annunciator illuminates any time the engine-driven pumps are operating. B) A HYD PRESS annunciator illuminating while the gear is extending may indicate a failed hydraulic pump. C) The LO HYD LEVEL annunciator illuminates whenever reservoir fluid level is 0,5 gallons. D) A LO HYD FLOW annunciator illuminating may indicate a failed hydraulic pump.
The thrust reversers: A) May be deployed only when the throttles are in IDLE. B) Must have both emergency stow switches in EMER for takeoffs to guard against inadvertent deployment during the critical phase of flight. C) May be left in idle reverse until the airplane is brought to a full stop. D) Both A and C.
When normal deployment of the thrust reverses is obtained, the following annunciator lights should be illuminated: A) ARM, UNLOCK, DEPLOY. B) DOOR NOT LOCKED, ARM, UNLOCK, DEPLOY. C) HYD PRESS, ARM, UNLOCK, DEPLOY. D) DOOR NOT LOCKED, HYD PRESS, DEPLOY.
The incorrect statement regarding the use of thrust reversers is: A) The may be used in flight to slow the airplane. B) They should not be used on touch and go landings. C) The reversers must be in idle reverse by 60 KIAS. D) Thrust reverser airplanes have two squat switches.
The MASTER WARNING lights: A) Have nothing to do with the reverser system. B) Will illuminate if an ARM light illuminates while in flight. C) Will illuminate if the HYD PRESS light remains illuminated after the DEPLOY lights is illuminated. D) Will illuminate if a DEPLOY light illuminates in flight.
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