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Flexjet Praetor 500 > Landing Gear and Brakes > Flashcards

Landing Gear and Brakes Flashcards

1
Q

What does pulling the LANDING GEAR FREE FALL LEVER do?

A

Relieves the hydraulic pressure in the landing gear lines and mechanically releases the uplock hooks for all the landing gear. AOM 9-13-30

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2
Q

What does it mean when the LANDING GEAR POSITION INDICATIONS turn to red icons?

A

That more than 20 seconds has passed since a discrepancy has been detected between the landing gear lever position and the actual landing gear position. AOM 9-13-30

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3
Q

If the parking brake is not fully released on the ground, what CAS message will be displayed?

A

Either a white PARKING BRAKE ON CAS or a cyan CHECK PARKING BRAKE CAS message. AOM 9-13-30

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4
Q

If the parking brake is not fully released in flight, what CAS message will be displayed?

A

An amber PARK BRAKE NOT REL CAS message. AOM 9-13-30

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5
Q

Where can the emergency/park brake accumulator pressure and the brake temperature indications be seen?

A

On the STATUS synoptic page. AOM 9-13-30

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6
Q

How long can the light on the STEERING button and the STEERING DISC CAS message take to go off after the first engagement of the nose wheel steering?

A

Up to two seconds. AOM 9-13-30

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7
Q

Which steering switch has priority for safe operation on the ground?

A

The external STEERING DISENGAGE switch. AOM 9-13-30

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8
Q

When will the green TOWING ALLOWED light in the external steering panel illuminate?

A

When the external STEERING DISENGAGE switch is in the DISENGAGE position and the parking brake in not applied. AOM 9-13-30

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9
Q

How far should the airplane be towed slowly in a straight line before turning?

A

10 feet. AOM 3-01-75

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10
Q

When should the DN LCK REL (down lock release) button be used?

A

Only in the event of a landing gear control lever failure or when it is necessary to clear obstacles. AOM 9-13-50

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11
Q

What type of brake system is on the aircraft?

A

Brake-by-wire. AOM 9-13-60

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12
Q

During normal operations, what does the Brake Control Unit (BCU) provide?

A

Locked wheel protection, anti-skid protection, gear retract braking, touchdown protection, a gear extension test, brake temperature monitoring and auto brake (optional). AOM 9-13-60

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13
Q

Where can the Brake Temperature Monitoring System (BTMS) information be found an what does it provide?

A

On the STATUS synoptic page, brake temperature status on the synoptic page and brake overheat warning on the EICAS. AOM 9-13-60

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14
Q

Where must the brake temperature indication be prior to takeoff?

A

In the green range. AOM 3-15

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15
Q

What are the two different modes of AUTOBRAKE control?

A

Landing mode (LO, MED, HI) and rejected takeoff (RTO). AOM 9-13-60

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16
Q

What kind of pressure will autobrake in the RTO mode apply?

A

A brake pressure equivalent to the maximum manual braking. AOM 9-13-60

17
Q

When will autobrake applications begin on landing?

A

Autobrake application will start one second after WOW indicates ground and thrust levers signal at idle. AOM 9-13-60

18
Q

Is antiskid protection available while braking with the emergency /parking brake?

A

No. AOM 9-13-60

19
Q

What handle position is used when using the emergency/parking brake as a parking brake?

A

The handle must be pulled until it locks at the full up position. AOM 9-13-60

20
Q

Where can the emergency/parking brake handle be set to as a reference for emergency braking?

A

To the intermediate position (first detent). AOM 9-13-60

21
Q

How can the emergency /parking brake be modulated?

A

By keeping the release button pressed. AOM 9-13-60

22
Q

How many full applications/how many hours of parking do the emergency/parking brake accumulators provide?

A

6 full or 16 hours. AOM 9-13-60

23
Q

When the airplane is airborne, is the steering system engaged?

A

No, it will automatically be disengaged. AOM 9-13-70

24
Q

What is the maximum range that the nose wheel can turn in free wheel steering mode?

A

+/- 170°. AOM 9-13-70

25
Q

List the steering angles and associated speed with nose wheel steering engaged:

A

Steering angle varies from +/- 62° up to 10 kts, decreasing laterally to +/- 8° at 25 kts and then to +/- 3° at 68 kts. AOM 9-13-70

26
Q

What airspeed is Vlo?

A

250 kts. AOM 2-10

27
Q

What airspeed is Vle?

A

250 kts. AOM 2-10

28
Q

When must AUTOBRAKE be set to OFF?

A

For emergency and abnormal procedures. AOM 2-49

Flexjet Praetor 500 (25 decks)

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