121-140 Flashcards

1
Q

Are you able to re-stow the fire handle after you have pulled it?

A

You can restow it. Can’t find answer about it resetting SOVs

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2
Q

Why are we required to push the cargo smoke button an additional time to discharge the low rate bottle on the ground?

A

Low rate won’t automatically discharge on the ground because it assumes there will be outside fire assistance and we don’t want it to discharge for 75 minutes

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3
Q

According to the SOPM, how long should we delay APU start before pushback?

A

10 minutes prior to push

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4
Q

What is the minimum temperature to start the APU?

A

-54 C

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5
Q

When shutting down the APU, what is the difference between pushing the EMERG STOP button and turning the APU switch to OFF?

A

EMER STOP button closes APU fuel shutoff valve with no cool down period. OFF initiates normal APU shutdown.

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6
Q

If performance requires ECS OFF, what operational considerations exist with respect to the APU?

A

ECS off = APU on for pressurization and air conditioning.

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7
Q

How long can the aircraft be unattended while the APU is running?

A

No more than 5 minutes (SOPM 02-04.4)

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8
Q

What is the maximum speed for the windshield wipers?

A

250 kts

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9
Q

Do the wipers operate together or independently?

A

Independently

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10
Q

When should taxi lights be on? Off?

A

On: Movement on ground through 10,000, 18,000 ft descent check.

Off: Stationary on ground, or pulling into gate.

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11
Q

When does the SOPM require the NAV lights to be switched on?

A

When electrical power is applied to the aircraft (SOPM 04-01.8)

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12
Q

How do you initiate a hydraulic PBIT?

A

H-PBIT begins when all 3 hydraulic systems are pressured and reservoir temp is at least +10C (SOPM 04-01.11)

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13
Q

List the ways in which a hydraulic PBIT can be interrupted?

A

Interrupted when any flight control surface is moved. (SOPM 04-01.11)

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14
Q

What temperature will inhibit the HPBIT from running? Why?

A

Less than 10 degrees C. Because it’s too cold to properly move and could cause a flt cntrl no dsptch

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15
Q

When is a hydraulic warm up required?

A

Reservoir temperature below -18C prior to engine start

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16
Q

What is the purpose of the PTU?

A

The PTU assists the landing gear retraction or extension, should a right engine or right EDP failure occur.

17
Q

What is the EICAS message associated with the hydraulic PBIT?

A

FLIGHT CONTROL TEST IN PROG

18
Q

How is normal hydraulic pressure, temp, and quantity determined during the originating checklist?

A

CA originating flow, hydraulic synoptic page

19
Q

When must a hydraulic PBIT be completed without interruption?

A

When the test is expired or will expire

20
Q

How is landing elevation set?

A

By setting the destination airport in the MCDU the plane will automatically set LFE