Last 50 Qs Flashcards
(40 cards)
When is body steering activated?
AOM VOL II CH 14
Steering must exceed 20° and ground speed must be decreasing through 15 kts
When is RTO activated on a rejected takeoff if selected?
AOM VOL II CH. 14
Ground speed above 85 kts
All thrust levers closed
The brake source light is monitoring which system?
AOM VOL II CH 14
The active brake hydraulic source (system 4, 1 or 2).
What is the highest brake temp number on the GEAR synoptic page?
QRH VOL II CH 14 (?)
9
Do we have to write up a > BREAK TEMP EICAS message?
QRH CH 14
Yes
What will cause the autobrakes to disarm?
See a previous question
With the autobrakes, armed brake application begins when?
AOM VOL II CH 14
All thrust levers closed
Ground mode is sensed
Wheels have spun up
Body gear steering operates when nose wheel steering angle exceeds how many degrees?
AOM VOL II CH 14
20°
What must you have to get auto brakes?
AOM VOL II CH 14
The normal brake system, HYD system 4
How is predictive windshear system different from the reactive windshear system?
How should you react to either warning?
AOM VOL II CH 15
Predictive windshaer increases alerting time over reactive windshear by using Doppler weather radar to detect low altitude, horizontal wind, flow below 2300’ RA .
Auto pilot: disconnect
Push: TOGA
Thrust: maximum (apply aggressively)
Pitch attitude: rotate to 15° and roll wings level
Follow flight Director guidance
You may leave the AP on after TOGA, but be prepared to take over .
When is the STATS cue inhibited?
AOM VOL II CH 15
After engine start until 30 minutes after lift off
A vertical motion arrow on the ND traffic display indicates the traffic is climbing or descending at what rate?
AOM VOL II CH 15
Indicates a climb or descent of 500 ft./min. or greater
When is the MCP selected altitude alert inhibited?
AOM VOL II CH 15
Glideslope captured
Landing flaps selected and gear down and locked
Predictive windshear system operates only below what altitude?
AOM VOL II CH 15
2300’ RA
The Event Record switch will record how many events?
AOM VOL II CH 15
5 EICAS events
what is the purpose of the EIUs?
AOM VOL II CH 10
Supply information to the PFD, ND and EICAS.
The predictive wind system(PWS) is active when?
Are there any restrictions?
AOM VOL II CH 15
On the ground:
When WXR selected on EFIS control panel W/radar in any mode other than TEST
Automatically at 60% to 70% N1
In flight: automatically below 2300’ RA
What conditions trigger an EICAS altitude alert?
AOM VOL II CH 15
Depart more than 300’ from your selected altitude
Terrain displays (TAWS) are either solid or dotted, green, amber or red. What are the differences?
AOM VOL II CH 15
Dotted green: terrain 2000’ below to 500’ below (250’ W/GD)
Dotted Amber: terrain 500’ below 2000’ above (250’ W/GD)
Dotted red: terrain > 2000’ above
Solid amber: look ahead, terrain, caution
Solid red: look ahead, terrain, warning
When are the MCP altitude alerts inhibited?
See a previous question
During engine start all EICAS caution and advisory messages are inhibited, except;
AOM VOL II CH 15
Bleed
ENG autostart
ENG fuel valve
ENG shutdown
ENG start VLV
Starter cutout
What 2 Conditions Would Dr. the magenta command, air speed bug(CAB) to the bottom of the over speed indication?
FCTM CH 4, 4-3
At heavy weights or high-cost index .
When directed by the QRH pushing the ground proximity flap override switch inhibits what?
AOM VOL II CH 15
inhibits TOO LOW flaps alert
What is monitored by the takeoff warning system?
AOM VOL II CH 15
Engine 2 or 3 intake of thrust (N1 is 70% or more):
Flaps not in takeoff
Speed brake lever not in down detent
Stabilizer not in takeoff range
Parking brake set
Body gear not centered
