B757 Flight Controls Flashcards

1
Q

Why does the Yaw Damper become INOP?

A
  1. Fault
  2. switch off
  3. IRS not aligned
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2
Q

How many spoilers per wing?

A

6

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3
Q

SPEEDBRAKES

A
  1. Flaps are in the landing position

2. RA 800 feet or below

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4
Q

Which are the takeoff flap positions?

A

1, 5, 15 & 20

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5
Q

Alternate flaps switches do what?

A
  1. Arms the LE or TE flap alternate drive unit

2. Shuts off hydraulic power to both the flap and slat drive systems

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6
Q

AUTO BRAKES - DISARM

A
  1. Disengages the auto brake system

2. Releases brake pressure

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7
Q

Which hydraulic systems supply pressure to the Rudder?

A

All three

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8
Q

What does the Rudder Ratio System do?

A

Limits Rudder deflection at high speeds.

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9
Q

Which hydraulic system powers the Rudder Ratio Changer?

A

Left Hydraulic System

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10
Q

When will the speedbrakes deploy if they are not armed prior to landing?

A

On the ground when either thrust lever is moved to the reverse idle detent.

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11
Q

What happens to the Slats and Flaps @Flaps 1?

A
  1. Slats move to the midrange

2. Flaps extend to 1

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12
Q

What does the Auto Slat System do?

A

Automatically extends the slats from the midrange to fully extended landing position during a Stall Warning.

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13
Q

When do the Slats move to the landing position?

A

Flaps 25

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14
Q

Flaps Load Relief is armed when and does what?

A

Flaps are extended to 30 - armed
Airspeed placard Limit exceeded
Flaps retract to 25 position then back once exceedence

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15
Q

TRAILING

EDGE

A
  1. Flap Disagree commanded position
  2. Flap asymmetry
  3. Flap lever not in a detent for an extended period
  4. Flap Load Relief is INOP
    Hydraulic power shut off with disagree or asymmetry
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16
Q

LEADING

EDGE

A
  1. Slat disagree with commanded position
  2. Slat asymmetry
  3. Hydraulic power is shut off
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17
Q

What happens when either the ALTN LE or TE button is pushed?

A
  1. Arms the LE or TE alternate drive unit

2. Shuts off hydraulic power to both LE and TE drive units

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18
Q

Is any asymmetry or Load Relief protection available when using ALTN extension?

A

Only LE have asymmetry protection using ALTN

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19
Q

When do slats extend to landing position with ALTN extension?

A

Flaps 20 selected

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20
Q

How do you override a Jammed Control ?

A
  1. Sufficient forward pressure or
    Sufficient aft pressure
  2. Column disconnects
  3. Use free control column for pitch inputs
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21
Q

Stabilizer Trim Motors are powered?

A

Hydraulically

22
Q

At what rate will the autopilot trim the stabilizer?

A

1/2 rate using only one stabilizer Trim control module.

23
Q

Stabilizer Trim “OFF” flag?

A

Stabilizer Trim is INOP

24
Q

What do STAB TRIM CUTOUT switches do in the cutout position?

A

Removes hydraulic power to the respective Stabilizer Trim Control Module.

25
What happens if a control column input is made opposing the direction of the stabilizer trim?
Trim commands are interrupted.
26
How are the ailerons trimmed?
Dual aileron trim switches on the aft pedestal. Must be pushed together to command trim changes.
27
What type of trim will override the input of Electrical Trim switches on the control wheel?
1. Alternate Trim Lever | 2. ALTN STAB TRIM switch input
28
Which hydraulics power the stabilizer?
2 1. Center 2. Right
29
How many stabilizer Trim modules are there?
2 | One for each source
30
How many modes of stabilizer Trim control are there?
3 1. Electic 2. Alternate 3. Automatic
31
GND PROX SYS EICAS
FLAP OVRD selected for more than 60 | seconds airspeed greater than 250
32
GND PROX SYS EICAS
GEAR OVRD selected for more than 60 seconds airspeed greater than 290 Ko
33
ALTN STAB TRIM switches
* Electrically signal Stab movement | * neutralize all other stab trim commands
34
YAW DAMPER INOP
* fault * switch off * IRS not aligned
35
MACH | SPD TRIM
Mach/Speed Trim system is inoperative.
36
RUDDER | RATIO
1. Rudder Ratio System INOP | 2. left hydraulic system pressure low
37
SPEED | BRAKES
SPEEDBRAKES extended <800 ft RA with Flaps in landing position
38
What causes the the SPEED BRAKES light to illuminate?
2 conditions 1. Flaps in the landing position with speed brakes extended 2. RA 800 feet or below with speedbrakes extended
39
SPOILERS
One or more spoilers pairs are inop or not in the commanded position
40
STAB TRIM
Electric and alternate stabilizer trim is 1/2 the normal rate Use of alternate allows
41
UNSCHED | STAB TRIM
1. Uncommanded stab motion detected 2. Runaway stab motion with no pilot input 3. Wrong way Stab moves opposite of autopilot or Mach speed trim. 4. Use of alternate Trim with an autopilot engaged.
42
AUTO SPDBRK
Fault detected may result in loss of AUTO SPDBRK extension
43
Mach Speed Trim SYS
Controls stab when autopilot not engaged • Improves speed stability • electric, alternate or autopilot trimming overrides Mach speed trim
44
Aileron trimming w/autopilot
Changed neutral point without showing it on the scale.
45
How many spoilers per wing and their use?
6 Speedbrakes Supplementary roll control
46
What are the TO FLAP settings
1 5 15 20
47
LDG FLAP settings
20 - non normal 25 30
48
Flap gates
1 - inadvertent retraction of slats 20 - inadvertent retraction of flaps during a go around
49
Electric trimming with autopilot
1 autopilot - causes autopilot to disengage More than ONE AP- inhibited
50
Alternate trimming with AP
Does not cause disengagement