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When armed, the RTO mode of the Autobrake System: reduces brake pressure during the rejected take-off as other controls such as thrust reversers and spoilers contribute to total deceleration. operates above a groundspeed of 85 knots. operates if either Thrust Lever is retarded to idle during the take-off run. cannot be disarmed by manual braking.

Which hydraulic system is affected if selecting the reserve brake switch is needed?. Left. Center. Right & Center. None. Right & Left.

Do reserve brakes have the same capabilities as normal brakes?. No. Antiskid is inoperative - care must be taken on landing to avoid tyre blowout. No. Antiskid operates to paired wheels only. No. Brake pressure is reduced - full brake pressure is not available. Yes.

Which of the following statements is NOT true?. Normal brakes are powered by the Right hydraulic system. Alternate brakes are powered by the Center hydraulic system. Reserve brakes are powered by the Left hydraulic system. None of the above.

Antiskid operation is available using: both Normal and Alternate braking systems. both Normal and Reserve braking systems. the brake accumulator system. All of the above.

The ANTI SKID light indicates: a total failure of the antiskid system. a failure in the antiskid system - some antiskid protection may still be available. a system fault - only paired wheel protection is available. the antiskid system has not been armed for landing.

What action intiates normal landing gear extension?. Pulling the landing gear lever out and positioning to DN (DOWN). Pushing the landing gear lever in and positiong to DN (DOWN). Pushing the landing gear lever locked switch and placing the gear lever DN (DOWN).

The AutoBrake system will provide automatic braking down to ......... knots if not disarmed by the pilot. 0. 5. 10. 15.

When the Main and Nose gear have extended: Only main gear doors close. All gear doors close. Nose gear doors close.

How does the LOCK OVRD p/b override the landing gear lever lock?. Manually. Hidraulically. Electrically.

L HYD SYS PRESS + R HYD SYS PRESS on EICAS display. Will you have nose wheel steering after touchdown?. NO. YES.

Pressurization of the Alternate Brake system occurs automatically when the R HYD sys press is low. TRUE. FALSE.

The landing gear lock prevents movement of the landing gear lever to the up positon when any main gear is not tilted. TRUE. FALSE.

Which one of the following indicates the Auto Brake System is armed and operative. The Autobrake selector latches at the deceleration selection. The Autobrake ARMED light is on. The Autobrake EICAS msg is displayed.

How is the Alternate Gear Extension system actuated?. Crank operation. Handle operation. Toggle switch.

When does the Alternate brake system operate?. When RIGHT hydraulic pressure to normal brake is low. When the Antiskid controller detects a fault in normal brakes. When the Max Auto setting is selected for autobrakes.

When does the landing gear lever lock prevent movement of the landing gear lever to the UP position?. When the gear is not tilted. When the nosewheel steering is not centered. When the gear is tilted.

Moving the Autobrake selector from DISARM to OFF turns the Autobrake light OFF. TRUE. FALSE.

After a loss in the Center and Right Hyd systems, do you have antiskid braking?. YES, fully operational. NO. YES, paired wheels.

What is the function of the parking brake valve?. Prevents accumulator pressure to bleed off. Supplies accumulator pressure to the brakes. Supplies system pressure to the brakes.

What function occurs automatically during landing gear retraction?. Lever latch override. Nose gear Tilting. Wheel braking.

During Alternate Extension, MAIN gear doors remain open. TRUE. FALSE.

The amber "DOORS"light means either Main gear or Nose gear door is open when the NOSE gear is not extended. TRUE. FALSE.

What is accomplished by positioning the landing gear lever to OFF?. It provides a hydraulic pressure lock to the landing gear and doors. It stops operation of the brake cooling fans. It depressurizes the landing gear system.

There is a Speed / Drag limitation if the tailskid remains extended. TRUE, performance penalties apply. TRUE, no calculation needed since its not possible to determine tailskid position. FALSE.

How many degrees must the Nose Steering Tiller be rotated to obtain the maximum 65 degrees of steering?. 65 degrees. 360 degrees. 90 degrees. 180 degrees.

During Maximum braking what prevents the wheels from skidding?. Antiskid valves. Hydraulic valves. Autobrake valves.

Which Hydraulic system powers the Alternate brake system?. Left. Right. Center.

Which one of the following will cause a take off configuration warning?. Parking brake set. Bleed valves not open. Nose wheel not aligned with runway. A cargo door unlocked.

Inflight, the Gear Not Down configuration warning occurs if. Aircraft flying below 800 ft, any gear not down and either thrust lever at idle. Speedbrakes and flaps are extended at the same time. Aircraft flying below 800 ft and flaps not in Landing position.

How is the parking brake released?. Apply pressure to brake pedals. Push down the parking brake handle. Pull up the parking brake handle. Rotate the Autobrake selector to OFF.

When will the Autobrake light be illuminated?. When the selector is in the OFF position. When the Autobrake system is operating. When the selector is in DISARM position.

Normal brakes are powered by. R HYD SYS. C HYD SYS. L HYD SYS.

In cruise phase, you loose complete electric power and battery power is now depleted. Can you extend the Landing Gear?. Yes, by normal & alternate extension. NO. Yes, by Alternate extension. Yes, by Normal extension.

Why is the Landing gear lever moved to OFF prior to Alternate gear extension?. To prevent the possibility of Hydraulic power interference. To open gear doors. To release gear up locks.

What is indicated with the ANTISKID message and ANTISKID light ON?. Hydroplane protection activated. Power loss or system malfunction. System normal.

When will the landing gear lever lock release?. When the main and nose gear struts extend. When the main gear struts are compressed. When main gear tilt.

What is the function of the landing gear lever lock?. Provides hydraulic pressure for tilting each main gear. Prevents moving the gear lever UP on the ground. Prevent moving the gear lever to DN on the ground.

What is the maximum alternate gear extension airspeed?. 290 kts - .82 mach. 250 kts - .75 mach. 320 kts - .82 mach. 270 kts - .75 mach.

Following touchdown with Autobrake armed, when will the Autobrake activate?. When the groundspeed is less than 85 kts. When both thrust levers are at idle. When both thrust leves are in reverse.

Which of the following disarms the Autobrake after landing?. Retracting the speedbrake. Manual braking. Both, Manual braking or speedbrake retraction.

Which one of the following provides the greatest deceleration rate?. Full manual braking. Autobrake selection 4. Autobrake selection MAX AUTO.

What is the maximum landing gear extension speed?. 250 kt - .75 Mach. 290 kt - .82 Mach. 270 kt - .82 Mach. 320 kt - .82 Mach.

Which Hydraulic system provides hydraulic pressure for Landing Gear alternate extension?. Left. Right. Center. None.

In normal operation the Landing Gear is powered by the Center Hydraulic system. TRUE. FALSE.

What holds the main landing gear doors in the closed position?. Overcenter struts. Gear door locks. Internal hydraulic actuators.

Autobrake is available in Normal and Reserve brake modes only. TRUE. FALSE.

What would be the position of the Autobrake selector if the pilot applies brake pedal pressure after an Autobrake landing?. OFF. DISARM. Previous braking selection.

What holds the main landing gear in the up position?. Overcenter struts. Locked main gear door structure. Main gear locks.

How many degrees can the nose wheel be turned with the rudder pedals in either direction?. 0 to 90. 0 to 65. 0 to 7. 0 to 360.

After take off, how does the Autobrake selector move from RTO to OFF?. Automatically. Manually. Remains in RTO.

Tilt sensors located in each main landing gear send signals to Air/Ground sensing system. TRUE. FALSE.

The Nose Landing gear sends signal to the Air/Ground sensing system, providing inputs for Stall warning and Caution / Warning system. TRUE. FALSE.

Landing gear Alternate extension only needs battery power to activate (HOT BAT BUS), it uses an electric motor to unlock gear and free fall extension to deploy the gear. In such case the Main landing gear doors will remain open. TRUE. FALSE.

When Antiskid is INOP, Take off is not permitted on contaminated runways, in wet runways is permitted but performance penalties apply. TRUE. FALSE.

Brake source light is illuminated, which braking system/s is/are not available?. Brake Accumulator. Reserve brake and Normal brake. Alternate brake and Normal brake. Normal brake. Alternate brake and Reserve brake.