Aircraft Configuration Flashcards
Aluminum panels are used in some locations for E3 protection while____has been bonded to composite material panels in other locations
Aluminum mesh
Which components are located in the avionics compartment?
Number one and number two slab
Number one and number two EGI
Number two FCC
Esis battery
How much ground clearance does the landing light in searchlight have when extended
Less than 1 ft
Why does storing items blow the seat? Increase the probability in severity of injury in the event of a crash
The seats are designed to stroke downward during a crash
The vlea can be adjusted. From___pounds to___pounds
130 to 250
What provides a means of manually selecting alternate data sources for the pilot and copilot mfds?
Reversionary switch panels
What is the purpose of the I-Event switch?
To capture and record intermittent event data
Where is the ESIS display located?
The upper center of the instrument panel
What is the purpose of the auxiliary fuel management panel
It contains all controls for operating the CEFS
How is the tail wheel locked in the trail position from the cockpit
By activating the unlock/lock switch on the parking brake/ tail wheel control panel
What are the three positions of the backup hydraulic pump switch?
On auto off
The___safeguards the battery system and the DC electrical system from shorts in the applicable bus
Battery circuit breaker panels
The ICS consists of___control panels located throughout the aircraft
5 ICS control panels
___Mode provides for hands off and foot off voice activated keying of the ICS intercom or the pvt intercom
VOX
Illumination of the___indicates that the digital link between the ICS panel and the ICU has been broken
ICU light
What are the four engine power control lever positions?
Off idle fly lockout
How is cockpit ventilation controlled
Vent blower switch
When either___is pulled DC power actuates the fire extinguisher logic module to select the compartment to which the fire extinguisher agent is to be directed
Engine fire T-handle
The two-stage main strut is designed to absorb a landing rate of up to ___ ft per second
39 fps (11 Gs)
For flights over 6 hours, the engine oil level should be___
Full
The___provides pneumatic power for main engine start and cabin heating and electrical power for ground operation and in-flight emergency
APU
The main transmission has a built-in___forward tilt
3 deg