Embraer 190 - Flight Controls
FLIGHT CONTROLS QUESTIONS MADE FROM AOM VOL. 2GOOD LUCK!SANTIAGO STOCKER.
- 1.The Flight Control System is comprised of the ...
- A.
Primary and the secondary flight control systems and their associated system components.
- B.
Primary flight control systems and their associated system components.
- 2.The primary flight control system consists of: (Check all correct options) lklk (C
- A.
Horizontal stabilizer
- B.
Ailerons and the multi function roll spoilers for roll axis control.
- C.
Rudder for yaw axis control.
- D.
Flaps and Slats
- E.
Elevators for pitch axis control.
- F.
The multi-function spoiler (when used as speed brakes or groundspoilers).
- G.
Dedicated ground spoilers
- 3.The secondary flight control system consists of: (Check all correct options) lklk (C
- A.
Horizontal stabilizer
- B.
Ailerons and the multi function roll spoilers for roll axis control.
- C.
Rudder for yaw axis control.
- D.
Flaps and Slats
- E.
Elevators for pitch axis control.
- F.
The multi-function spoiler (when used as speed brakes or groundspoilers).
- G.
Dedicated ground spoilers
- 4.Hydraulic actuators control the respective flight control surfaces. These are referred to as ____________________ (PCUs).
- 5.The ailerons are ...
- A.
Commanded by conventional control cables that run from each control wheel back to a pair of hydro-mechanical actuators.
- B.
Controlled electronically using Fly-by-Wire (FBW) technology.
- 6.Elevators, rudders, roll spoilers as well as all secondary flight control systems, including the horizontal stabilizer, flaps and slats, ground spoilers and speed brakes, are ...
- A.
Commanded by conventional control cables that run from each control wheel back to a pair of hydro-mechanical actuators.
- B.
Controlled electronically using Fly-by-Wire (FBW) technology.
- 7.The primary flight control electronics include ...
- A.
One part:• The Primary Actuator Control Electronics (P-ACE).
- B.
Two complementary parts:• The Primary Actuator Control Electronics (P-ACE).• The Flight Control Module (FCM).
- 8.Primary Actuator Control Electronics (P-ACE) and/or Flight Control Modules (FCM) are employed to operate the respective ...
- A.
Electro-hydraulic or electro-mechanical actuators.
- B.
Electro-hydraulic.
- 9.The EMBRAER FBW system is composed of a set of ...
- A.
Four Actuator Control Electronics (ACEs) and nine Flight Control Modules (FCMs):
- B.
Nine Actuator Control Electronics (ACEs) and four Flight Control Modules (FCMs):
- 10.______ Primary-ACEs (P-ACE).
- A.
One
- B.
Two
- C.
Three
- 11.______ Slat/Flap ACEs (SF-ACE).
- A.
One
- B.
Two
- C.
Three
- 12.______ Horizontal Stabilizer ACE (HS-ACE).
- A.
One
- B.
Two
- C.
Three
- 13.______ Spoiler ACEs (S-ACE).
- A.
One
- B.
Two
- C.
Three
- 14.______ Flight Control Modules (FCM).
- A.
Two
- B.
Four
- C.
Six
- 15.What does ACE mean?
- 16.The ACE units connect the control column ______________ to the respective control surface, providing direct analog control of the surface.
- A.
Electronically
- B.
Mechanically
- 17.There are ______ different ACE units:
- A.
Four
- B.
Six
- 18.The P-ACE units control the ...
- A.
Rudder and the elevator surfaces.
- B.
Slat and flaps surface.
- C.
Horizontal stabilizer surface.
- D.
Multifunction spoilers. Each FCM controls one pair of multi-function spoiler.
- 19.There are three P-ACE units, two installed in the forward electronics bay and one installed in the aft electronics bay. Each P-ACE has ...
- A.
One active channel.
- B.
Two channels one is the active and the other is the standby.
- 20.The SF-ACE units control the ...
- A.
Rudder and the elevator surfaces.
- B.
Slat and flaps surface.
- C.
Horizontal stabilizer surface.
- D.
Multifunction spoilers. Each FCM controls one pair of multi-function spoiler.
- 21.There are two SF-ACE units installed in the middle electronics bay. Each SF-ACE has two channels ...
- A.
One channel for flap and one channel for slat.
- B.
One is the active and the other is the standby.
- 22.The HS-ACE unit controls the ...
- A.
Rudder and the elevator surfaces.
- B.
Slat and flaps surface.
- C.
Horizontal stabilizer surface.
- D.
Multifunction spoilers. Each FCM controls one pair of multi-function spoiler.
- 23.The Horizontal Stabilizer ACE (HS-ACE) is installed in the aft electronics bay. The HS-ACE has ...
- A.
One active channel.
- B.
Two channels one is the active and the other is the standby.
- 24.The S-ACE resides within the FCMs and is used to control the ...
- A.
Rudder and the elevator surfaces.
- B.
Slat and flaps surface.
- C.
Horizontal stabilizer surface.
- D.
Multifunction spoilers. Each FCM controls one pair of multi-function spoiler.
- 25.FCM #1, FCM #3 and FCM #4 have wiring to control spoilers. FCM #2 does not control any spoiler pair.
- A.
True
- B.
False
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