Instrument Displays and Cross-Check Flashcards
The function of the EADI is to ____.
act as the source for primary attitude information
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
True or false: Once all electrical power to the standby attitude indicator is lost, it will continue to operate indefinitely.
False
True or false: 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
True or false: 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
True or false: 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
Without power, the standby attitude indicator will provide up to 9 minutes of attitude information and may have as much as ______ of error.
6°
