Landing Gear, Brakes, & Steering Flashcards

1
Q

What does a NWS LIMIT EXCEEDED(C) CAS indicate, and what action should be taken?

A

Nosewheel has been turned beyond 120 degrees. Check shear pins. If broken then the nose wheel has exceeded 123 degrees and possible damage has occured.

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2
Q

How much steering authority is available with the tiller?

A

65 degrees.

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3
Q

How much steering authority is available with the rudder pedals?

A

7 degrees.

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4
Q

The nose gear is actuated by which Hydraulic System?

A

Left Hydraulic System

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5
Q

What centers the nose gear during retraction?

A
  • Electrically by the Steering Control Unit

- Mechanically by cams on the top of the nose strut

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6
Q

Antiskid is available down to what speed?

A

10 knots

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7
Q

Why must we observe brake cooling times?

A

To ensure there is sufficient brake energy available to come to a complete stop within the charted distance if we reject a takeoff.

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8
Q

The landing gear is normally actuated by which hydraulic system?

A

Left Hydraulic System

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9
Q

Gear is held up by what?

A

Mechanical Uplocks

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10
Q

What do the brake accumulators provide us when loss of L and R hydraulic pressure?

A

1 continuous application to a complete stop

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11
Q

Parking brake accumulator has sufficient pressure for how many applications?

A

6

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12
Q

If a gear control or left hyd system failure occurs, how do we get the gear extended?

A

Alternate method through the checklist - pull the manual release handle “LG PULL”

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13
Q

What does the “LG PULL” handle do?

A
  • Manually releases the uplocks (Nose and Main Gear)

- Actuates the dump valves (ports fluid pressure to the return side of actuator)

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14
Q

When should the “LG PULL” handle be stowed?

A

After landing and the gear pins installed

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15
Q

What also assists the main gear to be fully extended? (down and locked)

A

Main landing gear down lock assist accumulator

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16
Q

Where do we read the Main Landing Gear Down Lock Assist Accumulator pressure?

A

Gauge is located in the battery compartment (purple band)

17
Q

How do we check the brake wear indicators?

A

With the parking brake set and the pins are not flush with the housing

18
Q

Where are the brake accumulator gauges located?

A

In the battery bay

19
Q

With a NORMAL BRAKES FAIL indication, how will we apply braking to stop the aircraft?

A

By pulling the Emer/Parking brake smoothly

20
Q

With a NORMAL BRAKES FAIL indication (pulling the Emer/Parking brake smoothly), will we have anti-skid or differential braking?

A

No

21
Q

When does the PTU operate in “AUTO”?

A
  • Left EDP failed
  • Right EDP producing pressure
  • Weight off Wheels (in air)
  • Gear not in the selected position
22
Q

What are the tire pressures?

A
  • Nose: 113 PSI

- Mains: 154 PSI

23
Q

What prevents the main tires from exploding in an overheat situation?

A

4 fuse plugs in each wheel assembly

24
Q

How many brake wear indicator pins are there on each brake assembly?

A

2 pins on each assembly - 1 top, 1 bottom

25
Q

What components of the landing gear are monitored by the Proximity Sensing System?

A

Main landing gear, nose gear, nose gear doors