Flight Controls Flashcards

1
Q

Which Flight Controls are NOT Fly by Wire?

A

Ailerons

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2
Q

How many Channels does a P-ACE have?

A

2 - Active/Standby

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3
Q

What is the maximum time manual pitch trim inputs are allowed?

A

3 Seconds

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4
Q

What are the Fly by Wire Components?

A

3 x P-ACEs (Primary)
2 x SF-ACEs (Slat/Flap)
1 x HS-ACE (Horizontal Stabiliser)
3 x S-ACE (Spoiler)
4 x FCMs (Flight Control Modules)

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5
Q

How many Channels does a SF-ACE have?

A

2 - Slats/Flaps

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6
Q

How many Channels does a SF-ACE have?

A

2 - Active/Standby, switching daily

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7
Q

What is the difference between NORMAL & Direct Mode?

A

FCM is removed from the the control loop and the control limits default to values set by hardware in the P-ACE when a channel failure is detected. High Level functions may not be available

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8
Q

How long do the Electric and Hydraulic PBITs take?

A

Electric - 3 minutes
Hydraulic - 1 minute

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9
Q

What is the Flight Control ODD-EVEN Day Engage Configuration?

A

Switches between the ODD & EVEN Channel, to reduce latency in the Flight Control System and to allow for even wear of the Flight Control System

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10
Q

How long does the Fly-by-wire Battery Last and what does it provide?

A

15 minutes - rudder and elevator actuators

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11
Q

How are the elevator surfaces actuated?

A

Hydraulically via the PCUs (Power Control Units)

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12
Q

What happens in the event of an Elevator Jam?

A

Respective elevator surface will remain fixed at the jammed position. Control can be achieved using the remaining elevator

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13
Q

Which Hydraulic Systems power the Elevator Actuators?

A

HYD SYS 1 - L OUTBOARD
HYD SYS 2 - L & R INBOARD
HYD SYS 3 - R OUTBOARD

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14
Q

What is TSA?

A

Tail Strike Avoidance System

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15
Q

Max Pitch Up with TSA Inoperative?

A

10° Pitch UP

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16
Q

What is the Stabiliser Trim priority Logic?

A

Backup
LH Pitch Trim Switch
RH Pitch rim Swithc
FCM AUTO Trim

17
Q

In the event of an electrical failure, followed by RAT deployment what happens to the Trim function?

A

It will operate at a low rate

18
Q

Which HS-ACE operates in the event of an electrical emergency?

A

HS-ACE 2 - At low rate

19
Q

Which Hydraulic Systems power the Ailerons?

A

HYD SYS 2 - Inboard Ailerons
HYD SYS 3 - Outboard Ailerons

20
Q

In the event of a RIGHT aileron Jam (FO) what happens?

A

Captain retains control of the LEFT aileron and Spoilers 5 WITH artificial feel

21
Q

In the event of a LEFT aileron Jam (CAPT) what happens?

A

FO retains control of the RIGHT aileron and Spoilers 4 WITHOUT artificial feel

22
Q

What happens in the event of a disconnection of 1 Aileron PCU?

A

Other PCU will operate normally but the force authority will be halved

23
Q

Which Spoilers are Multifunction Spoilers?

A

3-5 on each side

24
Q

What Hydraulic Systems power the rudder?

A

Hydraulic System 1 - UPPER
Hydraulic System 3 - LOWER

25
How many Slats/Flaps are there?
8 x Slats Leading Edge 4 x Flaps Training Edge
26
What is the priority order of SLAT/FLAP Retraction/Extension
Slats extended FIRST, Flaps Retracted FIRST
27
When might you see a SLAT(FLAP) FAIL EICAS?
Skew Protection - When the differential movement of a panel exceeds acceptable limits
28
What happens to the SLATS/FLAPS when the RAT is deployed?
Operate in half speed
29
What position must the FLAPS/SLATS be in for the RAT?
3 (Max)
30
How many Spoilers are there?
10 (6 are MFS)
31
What are the functions of the MFS?
Roll Control Speed Brakes Ground Spoilers Steep Approach
32
When are all 10 spoilers commanded?
ON GROUND Wheel Speed above 45kts or Airspeed above 60kts Thrust Levers below 26° MFS (Outboard) - 40° Ground Spoilers (Inboard) - 60°
33
When do all 10 spoilers retract?
When the speed is below 45kts for at least 5 seconds
34
What happens to all 10 Spoilers if the throttles are moved beyond 35° after landing?
Automatically retracted
35
Are Ground spoilers available in Direct Mode?
No
36
When will the speed brakes automatically be retracted?
Slaps/Flats Selected to Flap 2 or above Speed below 180kts When Thrust Levers advanced beyond 70° (to prevent inadvertent operation during a Go Around
37
How is Steep Approach Armed?
By pressing the Steep Approach Button
38
When is Steep Approach Disarmed?
ON GROUND TO/GA for a Go Around Stall Protection Activated Steep Approach Button Pressed Flaps removed from FULL Airspeed higher than VFE for Flap FULL
39
What is the Cyan Pointer on the Slat/Flap/Speedbrake indication on EICAS?
Commanded Slat/Flap Position