IN101

Question 1

Why is it important to manage the EFIS displays?

Answer 1

To optimize flight information

Question 2

The standby airspeed indicator is operated by the ______.

Answer 2

secondary pitot/static system

Question 3

Once all electrical power to the standby attitude indicator is lost, it will continue to operate
indefinitely.

Answer 3

False. Operates for 9 mins.

Question 4

If the standby turn and bank indicator loses electrical power, the turn needle will continue to operate.

Answer 4

False

Question 5

How long will the standby attitude indicator continue to provide reliable attitude information if it
loses electrical power?

Answer 5

9 minutes

Question 6

The standby instruments operate independently of the primary flight instruments.

Answer 6

True

Question 7

The relationship between attitude and power in instrument flying should result in ______.

Answer 7

desired aircraft performance

Question 8

Which performance instruments lag

Answer 8

Altimeter and VSI

Question 9

The hub and spoke method is the only cross-check method used and is not modified for any maneuver
in instrument flight.

Answer 9

False

Question 10

The recommended way to achieve smooth and precise aircraft control in flight is to trim in this order
______

Answer 10

rudder, elevator, ailerons

Question 11

The approximate power setting in level flight at 150 KIAS at 15,000 feet with clean configuration is
______%

Answer 11

35

Question 12

To maintain level flight on final approach at 110 KIAS with gear and flaps set at T.O., set
approximately _____% power

Answer 12

35

Question 13

The EFIS system is composed of ______

Answer 13

two displays and a control panel

Question 14

When the EADI fails, the only mode that still functions is the ______.

a. unusual attitude mode
b. roll attitude
c. pitch attitude
d. none of the above

Answer 14

None of the above

Question 15

Without power, the standby attitude indicator will provide up to 9 minutes of attitude information and
may have as much as ______ of error

Answer 15

6°

Question 16

Which of the following statements about primary and standby instruments is correct?
a. Both primary and standby instruments operate off the secondary pitot/static system and their
indications should match.
b. All the standby instruments operate off the primary pitot/static system and their indications will
match the primary instruments.
c. The primary and standby instruments operate off different pitot static systems and their
indications should closely match.
d. None of the primary and standby instrument indications should match.

Answer 16

C

Question 17

The concept of flying an aircraft in instrument conditions centers on controlling ______

Answer 17

attitude and power

Question 18

The two control instruments are ______.

Answer 18

EADI and primary engine data display

Question 19

Which of the following are performance instruments?

a. Altimeter and airspeed indicator
b. VSI and EHSI
c. AOA indicator and turn and bank indicator
d. All of the above

Answer 19

D. All of the above

Question 20

What cross-check method is the base for all instrument cross-checks?

Answer 20

Hub and spoke method

Question 21

When setting the local altimeter, it should be within ______ of the field elevation.

Answer 21

75 feet

Question 22

The approximate power setting at 110 KIAS for a non-precision final approach with gear and flaps set at T.O. and 1000 fpm descent is ______%.

Answer 22

16

Question 23

The primary purpose of the EADI is to______.

Answer 23

act as the source for primary attitude information