IN101 Flashcards
(23 cards)
Why is it important to manage the EFIS displays?
To optimize flight information
The standby airspeed indicator is operated by the ______.
secondary pitot/static system
Once all electrical power to the standby attitude indicator is lost, it will continue to operate
indefinitely.
False. Operates for 9 mins.
If the standby turn and bank indicator loses electrical power, the turn needle will continue to operate.
False
How long will the standby attitude indicator continue to provide reliable attitude information if it
loses electrical power?
9 minutes
The standby instruments operate independently of the primary flight instruments.
True
The relationship between attitude and power in instrument flying should result in ______.
desired aircraft performance
Which performance instruments lag
Altimeter and VSI
The hub and spoke method is the only cross-check method used and is not modified for any maneuver
in instrument flight.
False
The recommended way to achieve smooth and precise aircraft control in flight is to trim in this order
______
rudder, elevator, ailerons
The approximate power setting in level flight at 150 KIAS at 15,000 feet with clean configuration is
______%
35
To maintain level flight on final approach at 110 KIAS with gear and flaps set at T.O., set
approximately _____% power
35
The EFIS system is composed of ______
two displays and a control panel
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
None of the above
Without power, the standby attitude indicator will provide up to 9 minutes of attitude information and
may have as much as ______ of error
6°
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.
C
The concept of flying an aircraft in instrument conditions centers on controlling ______
attitude and power
The two control instruments are ______.
EADI and primary engine data display
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
D. All of the above
What cross-check method is the base for all instrument cross-checks?
Hub and spoke method
When setting the local altimeter, it should be within ______ of the field elevation.
75 feet
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 ______%.
16
The primary purpose of the EADI is to______.
act as the source for primary attitude information
