Systems - Flight Controls Flashcards

1
Q

How is the elevator operated?

A

Mechanically with no hydraulic assist (cables and pulleys) with no hydraulic assist.

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2
Q

How is elevator assist provided at high wing loading?

A

2 tabs on each side; servo and spring.

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3
Q

Where are the Servo Tabs located and what is their primary purpose? Where are the spring tabs located and what is there primary purpose?

A

1) Servo Tabs - Outer tabs, primary purpose is to assist at slower speeds (primary control suface has to move first.
2) Spring Tabs - Inner tabs, primary purpose is to assit at higer speeds.

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4
Q

What is a general rule of control tabs?

A

They move in the opposite direction of the primary control system you want to move.

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5
Q

How is each pilot connected to the flight controls?

A

Directly to their on-side controls with a torque tube at the pilot seats.

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6
Q

What happens when you pull the elevator disconnect?

A

Pulls the cable to a disconnection device and separate one side from the other in case of a jammed elevator.

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7
Q

Once the elevator disconnect is pulled, which side flight controls will work and what kind of elevator control will they have?

A

The side that is not jammed will work but with only half control (applies to aileron as well).

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8
Q

What is a positive indication of an elevator or aileron disconnect?

A

The light will illuminate (not handle position).

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9
Q

Once pulled, can disconnect be reset by pilots?

A

No, only by MX.

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10
Q

How is pitch trim operated on the EMB-145?

A

electrically commanded and electrically operated with an all moving horizontal stabilizer (no trim tabs).

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11
Q

How many pitch trim channels are there?

A

Two - main and backup

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12
Q

How is the main pitch trim channel controlled?

A

Yolk thumb switches on both Capt and FO sides.

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13
Q

Which pitch trim thumb switch has priority?

A

Capt

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14
Q

Can both the main and backup trim motors be activated at the same time? Which has priority?

A

No, only one at a time. The priority is first come first serve.

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15
Q

What is the HSCU?

A

Horizontal Stabilzer Control Unit - brains of the trim system

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16
Q

What logic do all three pitch trim split switches follow?

A

1) If you hold them them split for more than 7 seconds, it will disable the switch
2) Accumulated trim inputs of 16 seconds or more without control surface movement will dis-able the channel.
3) Trim inputs are limited to 3 seconds at a time (to help stop runaway trim).

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17
Q

When is automatic trim activated?

A

1) Through the autopilot (pitch only)
2) With speed brake deployment (when slow).

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18
Q

Is pitch trim speed consistent?

A

No

  • If you are going slow, trim will be fast
  • If you are going fast, trim will be slow.
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19
Q

When you push the QD button, what trim controls are interrupted?

A

All of them (pitch, yaw and roll).

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20
Q

How can pitch trim be read externally and what are the indications?

A

Top of horizontal stabilizer. 10° up and 4° down.

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21
Q

How is the rudder operated?

A

Hydraulically assisted, cable operated.

22
Q

How is rudder trim accomplished?

A

Electrically trimmed, no tabs and moves the entire rudder system.

23
Q

Can the rudder system be shutoff manually, if this is done how are the rudders operated?

A

Yes, with the SYS shutoff switches. Mechanical control (cable) will still be available.

24
Q

When does rudder system 1 automatically shut off.

A

On takeoff, above 135 kts if system 2 is available.

25
Q

What happens if rudder system 1 does not shut off above 135 kts.

A

You will get a RUDDER OVERBOOST EICAS message and rudder system 1 will need to be disengaged manually.

26
Q

What is a Rudder Hardover

A

Hydraulic mis-command resulting in a full deflection of the rudder.

27
Q

What is rudder hardover protection and when will it activate?

A

Cuts out ALL Hyd assist to the rudder if:

1) Rudder is deflected 5° or more
2) Pedal Force > 130lbs of opposite deflection
3) Both engines are above 56%N2

28
Q

Which flight controls are locked by activating the gust lock? Why is this necessary

A

Elevator becuase it does not have hydraulic assist.

29
Q

What kind of flaps are on the EMB-145?

A

Double slotted fowler flaps with 2 panels per wing (4 total).

30
Q

How are the flaps operated

A

Electrically commanded and operated.

31
Q

How many flap motors are on the EMB-145 and will they engage at the same time?

A

2 electric motors and yes, they do engage at the same time.

32
Q

How will you know if a flap motor fails?

A

1) The flaps will run at 1/2 speed.
2) you will get an EICAS message.
3) EICAS display will also show the actual degree change while in transit (on two motors you will get dashes when flaps are in transit).

33
Q

How are the flaps driven

A

Motors run a flexible shaft.

34
Q

How are the flaps prevented from being extended assymetrically?

A

Velocity Sensors

35
Q

What are the three ways you can read the flap position?

A

1) EICAS
2) RMU
3) Externally from exit row window

36
Q

When can you reset frozen flaps?

A

On the ground

37
Q

When are speed brakes used and which panels will deploy when they are activated?

A

Used in flight with the speed brake handle and the outboard panels will deploy.

38
Q

When are spoilers used and which panels will deploy when they are activated?

A

On the ground and inboard and outboard panels will deploy.

39
Q

How are speedbrakes and spoilers operated

A

Electricly commanded and hydraulically operated.

40
Q

What conditions need to be met to delploy speed brakes in the air?

A

1) Flaps 0°-9°
2) Low Thrust Lever Angle (TLA)
3) Pull Handle

41
Q

What conditions need to be met to deploy ground spoilers (all four panels)

A

1) Weight on Wheels
2) Low T.L.A
3) Speed above 25kts.

42
Q

Which HYD system operates the speed brakes

A

System 2

43
Q

Which HYD system operates the Ground Spoilers (all 4 panels)

A

System 1 and 2

44
Q

How many ailerons do we have and how are they operated?

A

Two mechanically operated (cable) hydraulically assited

45
Q

Do the Ailerons have trim tabs? How does Aileron Trim work?

A

No trim tabs. Trim is electric and moves the entire ailerons.

46
Q

What happens if you lose the hydraulic assist on the Ailerons? What kind of control will you have?

A

Revert to mechanical operation and will be very heavy.

47
Q

Which Hydraulic systems feed the ailerons.

A

Both.

48
Q

How many hydraulic systems are required to give you full aileron authority?

A

One

49
Q

Which side cable runs have the AP?

A

Capt. Side

50
Q

What is an artificial feel unit and how many do we have on board?

A

We have 2 on board and they provide an artificial realistic load feel to the pilots to prevent over-controlling the aircraft

51
Q

on which side are the artificial feel units installed?

A

On the FO side

52
Q

How is roll (Aileron) trim operated

A

Electrically.