81-100

Question 1

Recite PITCH TRIM RUNAWAY MI. Is this emergency addressed by the QRC? What section of the QRH is it?

Answer 1

AP / TRIM DISC Button - Press and hold
PITCH TRIM SYS 1 & 2 CUTOUT BUTTONS - push

It is an emergency- Non annunciated section of the QRH

Question 2

How would you alleviate excessive pitch up tendencies with a PITCH TRIM RUNAWAY?

Answer 2

Continuous banks up to 30 degrees

Question 3

Recite Roll (YAW) TRIM RUNAWAY MI.

Answer 3

AP / TRIM DISC Button
- Press and hold

Question 4

Recite STEERING RUNAWAY MI

Answer 4

STEER DISC SWITCH- Press
Steer the airplane using the differential braking and rudder

Question 5

When performing the SAFETY AND POWER UP CHECKLIST, which display units should be powered?

Answer 5

Screens 2, 3, and IESS

Question 6

What information is displayed on Display unit 2 when you first power up the aircraft?

Answer 6

Status page

Question 7

Why must battery voltage be checked before applying AC power?

Answer 7

So we can identity if our batteries have sufficient charge to handle an electrical emergency

Question 8

If Batt 1 is 22.5v and Batt 2 is 21.4v, what action must you take?

Answer 8

Recharge the batteries using the procedure in the SOPM. (SOPM 04-01.7)

Question 9

What is the battery charging procedure?

Answer 9

Recharge batteries using any AC power source. The time it takes to recharge is based on Batt Temp. This procedure can only be used when the Batt voltage is between 21.0 and 22.5. If less than 21.0 call MX.
(SOPM 04-01.7)

Question 10

What is the purpose of charging the batteries prior to takeoff?

Answer 10

In an electrical emergency, while the RAT is not deployed the batteries can provided 10 minutes of power. (AOM 14-05-15)

Question 11

What should the pilot check prior to conducting a fire panel test?

Answer 11

Verify no fire protection fail messages on the EICAS. (SOPM 04-01.8)

Question 12

Describe what comes with the fire panel test.

Answer 12

6 lights on overhead: Both fire handles, Cargo smoke FWD/AFT, APU button, upper half of APU EMER STOP
5 EICAS messages: CARGO FWD(AFT) SMOKE, APU FIRE, ENG 1(2) FIRE 2 FIRE indications inside ITT
2 Master warning lights
2 Aural warnings: Triple chime and fire bell
(SOPM 04-01.8)

Question 13

How do you determine if the AC power supplied by the GPU is within proper limits?

Answer 13

If the GPU button AVAIL light is illuminated the power is within proper limits. The plane checks for correct voltage/amperage/frequency automatically.
(AOM 14-05-10)

Question 14

Upon establishing AC power on the aircraft, what test should automatically start?

Answer 14

Electric P-BIT
(SOPM 04-01.11)

Question 15

When does the elec PBIT auto start? How long does it last? What can interrupt it?

Answer 15

E-PBIT automatically starts when an initial AC source is introduced.
It’s takes 3 minutes to complete
3 things interrupt it: any hydraulic pump is on, flight control modes switches are cycled, AC power is interrupted
(SOPM 04-01.11)

Question 16

Is the elec PBIt required to complete every flight?

Answer 16

No, only needs to be completed if it is about to expire or we have a FLT CRTL BIT EXPIRED EICAS msg is displayed. Means test is more than 50 hours old.

Question 17

What should the pilot do if AC ground power is suddenly lost?

Answer 17

Power the plane down using the Leaving the Airplane Checklist, wait one minute, power plane up using Safety and Power Up Checklist, let E-PIT run.
(SOPM 04-01.12)

Question 18

When do the amber IDG lights illuminate?

Answer 18

HOTLOP. If the IDG experiences HIGH OIL TEMP or LOW OIL PRESS the amber light illuminates. The QRH directs the pilots to disconnect the associated IDG. After disconnecting the light will extinguish.
(AOM 14-05-10)

Question 19

Generally speaking, can one IDG meet the needs of the entire elec system?

Answer 19

Yes, bus ties will automatically close to connect the electrical networks. (AOM 14-05-40)

Question 20

Why is the switch position for Batt 2 AUTO instead on ON?

Answer 20

Batt 2 is used to start the APU and it can be replaced by a DC GPU cart