Flight Controls & Stall Protection Flashcards

(68 cards)

1
Q

What will happen if pitch trim is outside the green when the takeoff configuration button is pressed?

A

“NO TAKEOFF, TRIM”

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2
Q

How long are electric and hydraulic PBIT tests valid for?

A

50 hours

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3
Q

When does electric PBIT begin?

A

AC power is established

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4
Q

How long does the electric PBIT take to perform the test?

A

3 minutes

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5
Q

What mode are higher level flight control functions active?

A

Normal

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6
Q

When does hydraulic PBIT begin?

A

When all three hydraulic systems are pressurized

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7
Q

How long does the hydraulic PBIT test take?

A

1 minute

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8
Q

What flight control is NOT fly-by-wire?

A

Ailerons

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9
Q

Which trim is not automatically accomplished when the auto pilot is on?

A

Yaw trim

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10
Q

What is the max speed for flaps/slats 1?

A

230 KIAS

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11
Q

What system provides higher level functions to the flight controls?

A

FCM

Flight Control Module

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12
Q

When is the stick shaker activated?

A

When pitched to Pitch Limit Indicator (PLI)

Airspeed indicates in the Low Speed Awareness (LSA red region)

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13
Q

How is stall protection accomplished?

A

Stick shaker and AOA limiting

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14
Q

How can you interrupt hydraulic PBIT?

A

Move a flight control surface

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15
Q

Can you deploy ground spoilers manually?

A

No, they are deployed automatically after landing

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16
Q

When will speed brakes automatically stow in flight?

A

Thrust levers near TOGA
Flap 2 or greater
Airspeed is slower than 180 KIAS

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17
Q

How can you interrupt electric PBIT?

A

Turning on a hydraulic pump

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18
Q

What is the alternate mode for flight control if normal mode fails?

A

Direct mode.

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19
Q

What does direct mode bypass?

A

FCM

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20
Q

What are the primary flight controls?

A
Slats
Flaps
Spoilers (ground and multi function)
Ailerons
Stabilizer
Elevator
Rudder
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21
Q

What are the various ACEs?

A

P-ACE
SF-ACE
HS-ACE
S-ACE

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22
Q

What does P-ACE control?

A

Primary ACE

Elevator and rudder?

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23
Q

What does SF-ACE control?

A

Slats/Flaps

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24
Q

What does the S-ACE control?

A

Spoiler

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25
Do we have aerodynamic trim?
No the hydraulics hold the flight controls in a neutral position
26
What flight controls are electric?
Slats and horizontal stab
27
What are the Higher Level Functions provided by the FCM?
``` Elevator control laws Auto-thrust compensation AOA limiting Rudder airspeed gain and stoke limit YD and TC via AFCS Rudder flight authority Roll spoiler scheduling with speed-breaks Configuration change compensation ```
28
What higher level functions are available in direct mode?
None
29
What are the trim priorities?
Back up controls Captain yoke FO yoke FCM
30
How long are trim inputs limited to?
3 seconds
31
How can you lock out the trim switches?
Hold only 1 of the split switches for 7 seconds
32
When will the E-PBIT run?
When AC power is established?
33
How long does the E-PBIT take to complete the test
3 minutes
34
What will interrupt the E-PBIT?
Moving flight controls Interruption of AC power Flight control mode switches (normal - direct)
35
How long are the PBITs valid?
50 hrs
36
When does the H-PBIT start?
When all hydraulics are pressurized?
37
How long does the H-PBIT test take?
1 minute
38
What will interrupt the H-PBIT?
Flight control surface movement
39
What is the recommend temperature for the hydraulic reservoir for the P-BIT test?
12 C
40
What is the limit for the hydraulic reservoir temperature for the PBIT test?
-18 C
41
When are you required to warm up the hydraulic reservoir for the PBIT test?
Below -18 C Recommend below 10 C
42
What is the procedure if you inadvertently interrupt the H-PBIT and it is expired?
Follow the SOPM procedure
43
If the elevator is in direct mode, what higher level function is lost?
AOA limiting
44
“FLT CTRL TEST IN PROG” on EICAS after engine starts indicates what?
Hydraulic flight control components are being tested
45
When will the ground spoilers deploy?
Weight on wheels Above 45 kts wheel speed or above 60 KIAS Thrust lever angle below 26 degrees
46
When will the ground spoilers automatically retract?
When the wheel speed is below 45 kts for 5 seconds or | Thrust levers are moved beyond 35 degrees
47
What does flight control direct mode do?
Bypasses the FCM
48
When do we push shaker cutout 1(2)?
QRH directed
49
What will make the speed brakes automatically retract?
Less than 180 KIAS flaps greater than 1 Greater than 70 degrees TLA
50
What will we get if the airplane puts the brakes away | automatically?
SPEED BRAKE LEVER DISAG EICAS message
51
Which trim functions have memory items?
Pitch trim and roll trim
52
What are the trim priorities?
Back up, CA, FO, AFCM
53
What happens when we hold the switch for 3 seconds?
Aural “TRIM” and stops moving the trim
54
What happens when we hold 1 trim switch for 7 seconds?
Hard disconnect MX must resolve
55
What flap settings can we use for takeoff?
Flaps 1, 2, or 4
56
What flaps setting can we use for landing?
Flaps 5 or FULL
57
What are GA flap settings?
Flaps 2 or 4
58
What’s the difference between flaps 4 and 5?
Flaps 4 is for takeoff and flaps 5 is for landing | There is no angular difference
59
When do we have to be fully configured for a stable approach?
1000’ RA
60
What does our airspeed have to be at 500’?
Confines of the speed bug
61
What happens if you cannot maintain a stable airspeed at 500 ft?
Go around
62
What kind of procedure requires pulling the flight control disconnect?
Memory item
63
When do we pull the flight control disconnect handle?
Jammed flight controls
64
What does the TCS button do on the yoke?
Pauses the auto pilot
65
What happens to FD when TCS is pushed?
Follows flight path
66
Can we use TCS to respond to an RA?
No
67
Can we use TCS to break away from an PRM ILS?
Yes
68
What does the AP disconnect button do on the yoke?
1 press to disconnect 2 to stop the aural warning