-x- Flight Controls -x- Flashcards

1
Q

What are the indications that alpha lock is triggered?

A

A-LOCK pulses on EWD (just above the slats on the slat/flap position indicator)

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2
Q

What are the characteristics of abnormal attitude law?

A

Operates like normal law with no stabilities, and auto pitch trim is also lost

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3
Q

What does low speed stability do in alternate law? Can this be overridden?

A

Introduces a progressive nose down input, which can be overridden by pilot input

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4
Q

In mechanical backup, what can be used to control the aircraft?

A

THS, rudder and differential thrust

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5
Q

What does high speed stability do in alternate law? Can this be overridden?

A

Introduces a nose up demand when above VMO/MMO which can be overridden by pilot input

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6
Q

What are the flap limiting speeds for A319 and A320 in config 1

A

230kts

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7
Q

When do you get an overspeed warning?

A

VMO +4
MMO +0.006

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8
Q

At what point does AP disconnect in slow speed?

A

Valpha prot + 1 degree

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9
Q

What are the flap limiting speeds for A319 and A320 in config 3

A

185kts

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10
Q

What does FAC stand for? What does it do?

A

Flight Augmentation Computer.

It has several main functions, including:
Rudder trim
Rudder travel limits
Yaw damping inputs
Alternate law
Flight envelope and speed computations
Wind shear detection

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11
Q

At what angle of bank does the AP disconnect?

A

45 degrees

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12
Q

In what conditions might you need to reset autothrust on approach?

A

In A319 only, if changing configuration with speed brakes extended, A/THR may settle 10kts above applicable speed target. This can be reset by recycling the A/THR button on FCU

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13
Q

When is abnormal attitude law triggered?

A

When normal law envelope is exceeded by external forces (eg wake turbulence encounter)

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14
Q

What happens once recovered from abnormal attitude law?

A

Auto pitch trim is regained, and aircraft will be in alternate law for the remainder of the flight. The aircraft lands in alternate law

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15
Q

With sustained sidestick input, what will speed decay until?

A

ValphaMax

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16
Q

At what angle of bank do the FDs disappear?

A

45 degrees

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17
Q

Which spoilers deploy for speed brakes?

A

Middle 3

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18
Q

When does AP disconnect in overspeed?

A

VMO +15
MMO +0.04

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19
Q

What is the purpose of abnormal attitude law?

A

Prevents normal law from impeding recovery

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20
Q

With A/THR engaged, what lowest speed will you decrease towards?

A

VLS +/-2kt

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21
Q

When does the aircraft revert to direct law?

A

When in alternate law, gear down, AP off for landing

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22
Q

What is the high AoA protection bank angle limit?

A

45 degrees

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23
Q

What triggers alpha lock?

A

Activated by SFCCs when flap lever moved from position 1 to 0 and either:
Alpha above 8.5 degrees or
Speed below 148kts

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24
Q

How can you identify that you are in mechanical backup?

A

MAN PITCH TRIM ONLY in red on PFD

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25
Q

What is VLS?

A

Lowest selectable speed

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26
Q

Are hydraulics required in mechanical backup to manoeuvre the aircraft?

A

Yes, either the green or the yellow system needed

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27
Q

How many slats per wing?

A

5

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28
Q

Which control surfaces have mechanical controls?

A

Rudder and THS. The rest are electronically controlled and hydraulically activated

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29
Q

What is VMO/MMO?

A

350kt/M0.82

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30
Q

Below alpha prot, what does sidestick command?

A

Alpha, instead of load factor

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31
Q

Do we keep protections and stabilities in direct law?

A

No, but overspeed and stall warnings still remain available

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32
Q

How can you tell you are in direct law?

A

USE MAN PITCH TRIM in amber on the PFD

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33
Q

What are the four modes of operation?

A

Ground mode, flight mode, flare mode and rotation mode (NEO only)

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34
Q

Will AP disconnect in alternate law for high speed or bank?

A

Yes for both. Speed if above VMO/MMO, bank if above 45 degrees

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35
Q

What are the main protections in normal law?

A

Load factor
Pitch attitude
Bank angle
High speed
High AoA

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36
Q

When do speed brakes autoretract?

A

Config full (or CONF 3 in A321)

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37
Q

Which spoilers deploy for roll?

A

Outer 4

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38
Q

Do you get full speed brake deflection with AP engaged?

A

Yes, in an A319 or A321. In an A320 only half speed brake deflection is available

39
Q

What are the load factor limitations in normal law?

A

Clean -1g to +2.5g
Configured 0g to +2g

40
Q

What does the low speed regime in normal law provide?

A

Low energy aural alert “SPEED”
Alpha floor protection

Neither of these are flight control protections

41
Q

What replaces the low speed alpha indications?

A

VSW

42
Q

What happens if an SFCC channel is lost?

A

Slats and flaps operate at half speed

43
Q

What is the maximum bank angle for auto pitch trim and bank hold?

A

33 degrees

44
Q

How many flaps per wing?

A

2

45
Q

In alternate law, and if available, at what speed is low speed stability active?

A

5-10kt above VSW

46
Q

What are the pitch attitude limitations in normal law?

A

Nose up 30 degrees (CONF 0-3) and 25 degrees CONF FULL. Progressively reduced by 5 degrees at low speeds.
Nose down 15 degrees in all cases

47
Q

In direct law, what config is needed for landing and what speed adjustment if any?

A

CONF 3 and VREF + 10kt for landing unless otherwise specified

48
Q

When moving flap lever from 0 to 1, what causes aircraft to go to config 1+F?

A

Speed less than or equal to 100kts

49
Q

What is an easy way to identify if you are in alternate law?

A

Amber crosses

50
Q

In high speed, when is nose down authority zero?

A

VMO +16
MMO +0.04

51
Q

At what angle of bank do the FDs reappear after overbanking?

A

40 degrees

52
Q

If ECAM states F/CTL ALTN LAW (PROT LOST), are protections lost?

A

Load factor protection is retained. High and low speed stabilities may be retained, but ECAM doesnt tell us

53
Q

In alternate law, is high speed stability available?

A

It might be, depending on the situation

54
Q

How many flight control computers are there?

A

7.
2 FACs
2 ELACs
3 SECs

55
Q

When are overspeed protections active?

A

VMO +6
MMO +0.01

Max 40 degrees AOB

If sidestick released, bank angle returns to 0

56
Q

In flight mode, what does the sidestick command?

A

In pitch, load factor demand, and in roll a roll rate demand

57
Q

What are SFCCs and how do they work?

A

Slat Flap Control Computers. They command two Power Control Units (PCUs) which operate the slats and flaps.

58
Q

With stick neutral, what will speed decay until?

A

ValphaProt

59
Q

In alternate law, what does the sidestick command?

A

In pitch it is normal - Load factor demand with auto pitch trim
In roll, it is a direct relationship. Maximum is 30 degrees per second clean or 25 degrees per second with flaps

60
Q

Which spoilers deploy for ground spoilers?

A

All 5

61
Q

What does SEC stand for? What does it do?

A

Spoiler Elevator Computer.

It has several main functions, including:
Normal roll via spoilers
Speed brakes and ground spoilers
Alternate pitch (SEC 1 and SEC 2 only)
Direct pitch (SEC 1 and SEC 2 only)
Alternate LAF (Load alleviation function)
Abnormal attitude
Direct roll

62
Q

What are the flap limiting speeds for A319 and A320 in config 1+F

A

215kts

63
Q

What happens if hydraulic input is lost to slats and flaps? Green? Yellow? Blue?

A

Surfaces operate at half speed. Yellow flaps. Blue slats. Green both

64
Q

Where on the speed tape is VSW?

A

Top of the barber pole

65
Q

At what attitude do FDs disappear in normal law? When are they recovered?

A

25 degrees up, 13 degrees down.

Recovered at 22 degrees up and 10 degrees down

66
Q

What is the high speed protection bank angle limit?

A

40 degrees

67
Q

What is the maximum bank angle?

A

67 degrees

68
Q

What are the flap limiting speeds for A319 and A320 in config 2

A

200kts

69
Q

What is shown at the low speed end of the speed tape in alternate law?

A

The barbers pole and the amber hockey stick only

70
Q

How many flight control laws are there?

A
  1. Normal law
  2. Alternate law
  3. Direct law
  4. Mechanical Backup
  5. Abnormal attitude
71
Q

What does ELAC stand for? What does it do?

A

Elevator Aileron Computer.

It has several main functions, including:
ELAC 1 controls ailerons
ELAC 2 controls elevators and horizontal stabilizer

Both control:
Normal pitch and roll
Normal LAF (load alleviation function)
Direct pitch and roll
Aileron droop
Abnormal attitude
Acquisition of autopilot orders

72
Q

In alternate law, is alpha floor available?

A

No

73
Q

What causes mechanical backup?

A

Loss of multiple flight control computers or flight control surfaces, or total but temporary electrical loss

74
Q

In direct law, what does the sidestick command?

A

Pitch - direct
Roll - direct

75
Q

What are the flap limiting speeds for A319 and A320 in config full

A

177kts

76
Q

What would you do on approach if selecting flaps 2 and the ECAM caution F/CTL FLAPS LOCKED - WING TIP BRAKE ON came on

A

Pull speed

DO NOT move the flap lever
Discontinue the approach
If below FCU altitude, it would need to be a go around, however because the flap lever can’t be moved, briefly confirm both pilots understand it will be a go around with no flap movement, then say something like “Go around maintain config”, and follow the missed approach. Aviator, Navigate, Communicate, then consider ECAM.

ECAM, then consult QRH landing with slats or flaps jammed

77
Q

Will you get the overspeed master warning and aurul warning in alternate law? If so, when?

A

Yes. VMO +4kt (MMO + 0.006)

78
Q

If at ValphaMax and sidestick released, what will speed go to?

A

ValphaProt

79
Q

What happens when sidestick released at bank angle greater than 33 degrees?

A

Bank angle returns to 33 degrees

80
Q

What is the maximum speed in alternate law?

A

320kt/M0.77

81
Q

What is alpha lock?

A

Inhibits slat retraction if low speed or high angle of attack

82
Q

What are the inputs to the FAC?

A

ELAC and rudder trim

83
Q

What are the outputs from the FAC?

A

Rudder

84
Q

What are the inputs to the ELAC?

A

Sidestick, pedals, FMGC

85
Q

What are the outputs from the ELAC?

A

FACs, SECs, Ailerons, Elevators, THS

86
Q

What are the inputs to the SEC?

A

ELAC, sidestick, Speed brake lever

87
Q

What are the outputs from the SEC?

A

Spoilers, Elevators

88
Q

What does FCDC stand for?

A

Flight Control Data Concentrator

89
Q

How many FCDCs are there?

A

2

90
Q

What are the inputs for the FCDC?

A

ELACs, SECs

91
Q

What are the outputs from the FCDC?

A

EIS, ECAM

92
Q

Which SEC is responsible for which spoiler?

A

S1 = SEC 3,
S2 = SEC 3,
S3 = SEC 1,
S4 = SEC 1,
S5 = SEC 2

93
Q

Which hydraulic system controls which spoiler?

A

S1 = G,
S2 = Y,
S3 = B,
S4 = Y,
S5 = G