Section II - Normal Procedures

Question 1

Asterisk (*) items:

Answer 1

Need not be accomplished on subsequent flights by the same crew flying the same aircraft on the same day.

Question 2

What must be removed before removing the control lock?

Answer 2

External gust locks

Question 3

Repeated tests will invalidate the AHRS BATT TEST indication since battery power is reduced each time the TEST switch is pressed (T/F)?

Answer 3

True

Question 4

Battery voltage must be?

Answer 4

22 to 24 volts

Question 5

After presure refueling the aircraft, an indicated +- ___ lbs is considered acceptable.

Answer 5

50

Question 6

What should you do when changing an electrical source?

Answer 6

Advise the crew

Question 7

During the battery feed test what should you check for?

Answer 7

FDR FAIL/STBY PWR ON annunciators, Uncage/Check stby attitude indicator, left ITT, stby instruments and RTU 1 powered.

Question 8

During the battery feed test with the battery switch in EMER check for?

Answer 8

Flood lights, AC BUS SHED annunciator, left N1, left N2, RTU 1, BATT CUT OFF, INV 1 FAIL, AOA indexer, ldg gear position indicators, copilots clock.

Question 9

Whenever power is applied to the aircraft:

Answer 9

One crewmember must be onboard at all times.

Question 10

What must you have to use auxiliary heating and cooling?

Answer 10

GPU power

Question 11

What must you do before operating aux cool?

Answer 11

Ensure environmental scoop plug is removed.

Question 12

Will the exterior crew entry door handle stow by activating the interior handle?

Answer 12

No (Failure to stow the handle can result in damage to the door during flight)

Question 13

Can you operate windshield wipers on a dry windshield?

Answer 13

No (will cause scratching)

Question 14

Typical Nose LDG strut extension is approximately?

Answer 14

3.5 inches

Question 15

Main LDG minimum strut extension is?

Answer 15

1.1 inches

Question 16

What must you do if opening the main LDG door by the manual system?

Answer 16

Support the gear door so it does not strike the ground.

Question 17

Ensure both main tires are?

Answer 17

The same brand.

Question 18

How many static wicks may be missing for flight?

Answer 18

0

Question 19

What should be set on the cabin pressure controller?

Answer 19

The higher of 1,000’ above cruise altitude or 500’ above field elevation. (set the rate of change to the 10 o’clock position)

Question 20

Turning the manual pressure controller past its normal range could do what?

Answer 20

Damage the threads or needle valve seat.

Question 21

When ACM off takeoff is planned set the manual pressure controller to?

Answer 21

Full decrease.

Question 22

At temperatures below 17 degress fahrenheit, it is allowable for the pneumatic pressure to fall within the yellow arc on the pressure gage? (T/F)

Answer 22

True

Question 23

At 0 degrees fahrenheit the pneumatic pressure can be as low as 1305 pSI with a fully serviced system? (T/F)

Answer 23

True

Question 24

For a battery start set the generator reset switches to?

Answer 24

NORM

Question 25

For a GPU start set the generator reset switches to?

Answer 25

OFF

Question 26

How do you know the door is closed and locked?

Answer 26

eight door locking pins show white

Question 27

When you test the emergency lights how many lights illuminate?

Answer 27

4

Question 28

What lights do not illuminate when testing the indicator lights?

Answer 28

red landing gear unlocked indicator (press to test), GND COMM, ENG START buttons (2), starter disengage button, ELT ON annunciator.

Question 29

How many seconds does it take for the trim warning horn to sound?

Answer 29

5

Question 30

What could happen if you fully deflect the rudder during flight control checks?

Answer 30

Damage to the linkage

Question 31

An external power unit is required for engine start at ambient temps below?

Answer 31

5 deg F

Question 32

Continue at Starting Engines

Answer 32

..