Card 281
Question
There are two actuators on the rudder, an upper and a lower. Which one does the Captain control?
Answer
The upper actuator
E190 Other Questions
Discover E190 Other Questions: 325 flashcards with questions and answers.
- Subject
- No category / Others
- Language of creation
- English
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Cards in this set
Card 282
Question
Each SF-ACE is a dual channel unit with:
Answer
1 channel for flap control and 1 channel for slat control
Card 283
Question
After touchdown, the FCM will command all multifunction spoiler surfaces to the 40° fully extended position when the following occurs
Answer
WoW
Card 284
Question
When will the speed brakes automatically stow? (What flap setting, and which TLA)
Answer
Flap 2 selected and TLA above 40 degrees
Card 285
Question
The Elevator Thrust Compensation (ETC) function, stabilizing the aircraft around the pitch axis, will be available?
Answer
In normal mode only as it is computed in the FCM unit
Card 286
Question
The Pitch Trim Control switches have a ___ second time limitation when actuated separately.
Answer
7 second
Card 287
Question
Where are the SF-ACE units located?
Answer
Two in the middle electronics bay
Card 288
Question
In the event of a jam in one of the control columns the disconnect mechanism can be actuated by? (What lever or handle)
Answer
Using the disconnect handle in the cockpit
Card 289
Question
If extended during approach the speed brakes will automatically retract upon?
Answer
Selecting flap 2 or speed less than 180 kt
Card 290
Question
In normal operations how many modes do the MFS have?
Answer
Three
Card 291
Question
What is the maximum deflection of the speed brakes in the air?
Answer
30 degrees
Card 292
Question
Should the electronic and the hydraulic systems fail, the landing gear can still be lowered using the:
Answer
Alternate gear extension lever
Card 293
Question
How many seconds after a landing gear position discrepancy is detected will a disagreement indication be displayed?
Answer
20 seconds
Card 294
Question
Locked Wheel protection is active anytime on the ground and at wheel speeds above:
Answer
30 kts
Card 295
Question
Which landing gear systems are supplied by hydraulic system 1? (Brakes)
Answer
Outboard wheel normal braking and emergency/park brake
Card 296
Question
When will touchdown protection be deactivated?
Answer
WoW for 3 sec or wheel speed greater than 50kts
Card 297
Question
How many full brake applications are available from the emergency/parking brake system?
Answer
six
Card 298
Question
What is the maximum steering angle possible from the rudder pedals
Answer
+- 7 degrees
Card 299
Question
The Electric Override Switch bypasses the PSEM and commands gear extension using:
Answer
Electrical and hydraulic power
Card 300
Question
Touchdown protection prevents brake application until _____________ after aircraft touchdown.
Answer
Three seconds
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