Landing Gear and Brakes Flashcards

1
Q

How are the landing gear extension/retraction and braking functions powered and controlled?

A

Hydraulically assisted and electronically controlled and monitored

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2
Q

Which hydraulic system powers landing gear retraction and extension?

A

No 1 hydraulic system

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3
Q

How should the landing gear be lowered if the No.1 engine fails?

A

Using the normal landing gear handle

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4
Q

How should the landing gear be lowered if the No.1 hydraulic system fails?

A

Using the free fall handle

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5
Q

Where is the landing gear position indicated?

A

Primarily on the EICAS, but also on either RMU

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6
Q

What system backups are available in the event of normal extension failure?

A

The electric override serves as the primary extension backup, and the free fall system serves as a secondary backup

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7
Q

How many proximity switches does the landing gear use to detect when the aircraft is on the ground?

A

Four. The nose gear proximity switch is not used by the landing gear

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8
Q

Which system use the nose landing gear weight on weight signal?

A

Thrust reversers and nosewheel steering

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9
Q

How are the nose landing gear doors kept closed when the landing gear is fully retracted?

A

Hydraulic pressure

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9
Q

If any gear uplock is found in the up position during a pre flight walkaround, how can it be reset?

A

By activating the landing gear free fall lever

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10
Q

What color is the EICAS landing gear position indicator when the landing gear is in transit?

A

Yellow and black cross hatched

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11
Q

If the landing gear is not in the selected position after 20 sec, what color is the EICAS display?

A

Red and black cross hatched

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12
Q

Under what conditions is the landing gear warning message generated when the gear is not locked down?

A
  • RA below 1,200 ft flaps set below 22 degrees, one thrust lever below 59 degrees and the other below 45 degrees
  • Flaps set at 45 degrees
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13
Q

What does the brake control unit do as soon as the aircraft is airborne and the gear is selected up?

A

Automatically applies brake pressure to the main gear wheels

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14
Q

How are the nose gear tires braked upon gear retraction?

A

Mechanically, via stops located in the nosewheel well

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15
Q

What are the three levels of protection provided by the anti skid system?

A

-Touchdown protection
-Locked wheel protection
-Anti Skid protection

15
Q

How does the anti skid function operate?

A

It releases brake pressure on the wheel it senses is rotating slower

15
Q

At what speed is anti skid available?

A

Wheel speed above 10kt during deceleration

16
Q

At what speed is locked wheel protection available?

A

Above 30 kt

17
Q

What does touchdown protection do?

A

It inhibits brake actuation before the main wheels have accelerated. Braking is inhibited until 3 sec after landing or the wheels have spun up to at least 50 kt

18
Q

Which hydraulic system powers the emergency/parking brake?

A

The No.2 system

19
Q

How many complete emergency brake actuators or hours of parking brake actuation can be relied on from the No.2 system accumulator?

A

Six emergency brake actuations or 24 hour of parking brake

20
Q

Are any of the brake protection systems available when using the emergency brake?

21
Q

How is the nosewheel steering system controlled and operated?

A

It is electronically controlled and hydraulically operated

21
What are the two ways of disconnecting the nosewheel steering?
Either by a switch on the back side of either pilot's control wheel or by an external steering disengagement switch in a compartment on the left front of the fuselage. This external switch cannot be reset from inside the aircraft
22
Which indication is provided to the pilots that the steering is disconnected?
STEER INOP caution message on the EICAS
23
What safeguard is provided to preclude an inadvertent gear retraction command while on the ground?
The air-ground system provides a signal to a solenoid inside the landing gear lever which places a mechanical stop over it
24
The nosewheel steering system is operating by which hydraulic system?
No. 1
25
Where are the brake temperatures shown?
On the MFD hydraulic page
26
What is the limit of nosewheel steering provided by the rudder pedals?
5 degrees. A position sensor set to 7 degrees disengages the system if the nosewheel is rotated above this limit by using the rudder pedals
27
What is the meaning of the BRAKE DEGRADED EICAS message?
It indicates a total or partial loss of braking capability of one outboard wheel and/or one inboard wheel, or internal BCU failure
27
How many seperate hydraulic systems power the brakes?
The brakes are powered by two independent hydraulic systems