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Spirit > Flight Controls & Flight Control Laws (Rev. 5) > Flashcards

Flight Controls & Flight Control Laws (Rev. 5) Flashcards

1
Q

What type of flight control system does the A320 aircraft family utilize?

A

Fly-by-wire system

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2
Q

Describe how the flight controls are controlled and activated

A

Electrically controlled and hydraulically activated

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3
Q

How is NORMAL LAW indicated on the PFD?

A
  • Green “=“ for pitch, bank, and over speed limits

- Amber / black (ALPHA PROT) airspeed tape

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4
Q

How is ALTERNATE LAW indicated on the PFD?

A

Amber Xs (indicating lack of NORMAL LAW protections)

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5
Q

How is DIRECT LAW indicated on the PFD?

A
  • Amber “USE MANUAL PITCH TRIM”

- Amber Xs indicating lack of NORMAL LAW protections

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6
Q

How is MECHANICAL BACKUP indicated on the PFD?

A
  • Red “MAN PITCH TRIM ONLY”

- Amber Xs indicating lack of NORMAL LAW protections

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7
Q

When operating in NORMAL LAW in flight mode, what does the side stick command for pitch and roll?

A

Pitch - G load

Bank - roll rate

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8
Q

What is the significance of the Side Stick Priority (Red Arrow) light?

A

The other pilot has gained side stick authority

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9
Q

Name the Flight Control Computers and the number of each

A
  • ELAC - elevator aileron computer (2)
  • SEC - spoiler elevator computer (3)
  • FAC - flight augmentation computer (2)
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10
Q

What does SEC 3 control?

A

Spoiler Control - one flight spoiler and one ground spoiler on each wing

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11
Q

What should happen to the THS after landing?

A

Reset to zero

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12
Q

Describe some of the protections a pilot will have in NORMAL LAW

A
  • Bank angle protection (67°) (roll)
  • Speed protection (high speed 6 kts above Vmo)
  • Load factor limitation +2.5G / -1.0G (+2.0G / 0.0G with flaps/slats)
  • AOA (Alpha)
  • Pitch attitude protections (30° UP / 15° DN)
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13
Q

Describe high speed protection

A

If Vmo/Mmo plus a predetermined factor is exceeded, the system induces a pitch-up input to limit A/C speed

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14
Q

What, if anything, can a pilot do to override high-speed protection?

A

It is not possible to override a protection while still in NORMAL LAW. In this case, the A/C would need to be forced into ALTERNATE LAW (for example by turning 2 ADRs off).

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15
Q

What is ALPHA MAX?

A

The maximum angle of attack allowed in NORMAL LAW, indicated by the top of the red strip on the airspeed scale

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16
Q

How does High AOA Protection operate?

A

When the AOA exceeds ALPHA PROT, nose up pitch trim ceases and AOA is now proportional to side stick deflection, not to exceed ALPHA MAX even with full aft side stick deflection

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17
Q

What protections and stabilities, if any, does a pilot have in ALTERNATE LAW?

A
  • Load factor
  • High speed stability
  • Low speed stability
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18
Q

What protections, if any, does a pilot have in DIRECT LAW?

A

None

19
Q

When, if at all, does FLARE mode activate in ALTERNATE LAW? Describe the entire process.

A

There is no FLARE mode if operating in ALTERNATE LAW. The A/C proceeds directly from ALTERNATE LAW to DIRECT LAW when the gear is selected down, and FLARE mode will not be available.

20
Q

If in ALTERNATE LAW, when will the A/C revert to DIRECT LAW?

A

If the controls downgrade to ALTERNATE LAW for any reason other than recovery from abnormal attitude, DIRECT LAW automatically becomes active with gear extension and autopilots not engaged. In this case, full use of autopilot is recommended until it must be disconnected.

21
Q

When is there a direct relationship between side stick and flight control surface deflection?

A
  • When in DIRECT LAW

- On the ground (ground mode)

22
Q

It’s common Airbus philosophy that the Airbus cannot stall in NORMAL LAW. However, there are conditions in which it can. Describe how this can happen.

A

A good pilot will operate under the philosophy that anything can happen. Preventative systems such as ALPHA PROT, ALPHA MAX, etc. could interpret bad data as valid data and subsequently fail to recognize the actual AOA or flight path of the A/C. Therefore, it is hard to point to exact scenarios when the Airbus can stall in NORMAL LAW. We need to understand anything is possible and we should recognize stall indications and recover regardless of the active control law.

23
Q

How would the A/C enter ABNORMAL ATTITUDE LAW?

A

By exceeding approx. double the NORMAL LAW limits

24
Q

What is the purpose of ABNORMAL ATTITUDE LAW?

A

Allows the A/C to be recovered from an unusual attitude

25
Q

If the flight crew is flying at 300 kts and they happen to pull full back on the side stick, how high would the A/C pitch up?

A

30° UP

26
Q

If the pilot selects 100 kts on the speed knob, how slow would the A/C fly if the A/P and A/TH are engaged?

A

Vls

27
Q

Describe, in detail, what would happen if the pilot slowly pulled the thrust lever to idle in NORMAL LAW

A
  • As airspeed decays, the THS adjusts the pitch attitude to maintain altitude
  • If the AOA increases to a threshold value, known as ALPHA PROT, the pitch function of the side stick changes. Stick movement commands a specific AOA instead of G load change
  • Since nose up pitch trim ceases, the pilot must hold continuous back pressure in order to fly slower than the speed for ALPHA PROT
28
Q

If the flight crew continued to pull back on the side stick, how slow would the A/C go?

A
  • The speed corresponding to ALPHA MAX
  • With the side stick full aft, the elevators will adjust the pitch attitude to maintain a maximum safe AOA (ALPHA MAX). This maximum AOA, induced by the pilot, is slightly lower than the stall AOA; therefore, the A/C theoretically cannot be stalled in NORMAL LAW
29
Q

At some point during this demonstration the A/THR automatically applies TOGA power. What is this protection and how does it work?

A
  • ALPHA FLOOR is a function of A/THR. It will activate at any airspeed based on AOA and automatically apply TOGA thrust regardless of thrust lever position
  • ALPHA FLOOR is available if the A/THR is functional (it does not need to be active), an engine is running, and the A/C is in NORMAL LAW
  • AOA protection does not depend on ALPHA FLOOR to function
  • On NEO A/C, ALPHA FLOOR is inhibited above M .6
30
Q

Describe what would happen if a flight crew attempted to over stress the A/C while in NORMAL LAW

A
  • Maneuver protection prevents a pilot from over stressing the A/C by limiting flight control inputs
  • If G loads become greater than normal, they are displayed in amber on the lower ECAM above the digital clock
  • When the side stick is pushed forward, less than 1G is commanded. A given pitch input always results in the same pitch response regardless of airspeed
  • When the stick is returned to neutral, the new pitch is held constant regardless of airspeed changes
31
Q

What will happen if the pilot over speeds the A/C? Are there any protections that are available to the pilots?

A
  • An over speed causes the flight control computers to provide a nose up input to reduce A/C damage due to excess speed. This protection limits the maximum airspeed by increasing the pitch attitude even if full forward stick is held
  • The speed at which this protection activates is shown on the airspeed indicator as a green “=“ sign
  • An over speed warning is generated as Vmo is exceeded (specifically Vmo+4). This warning can only be silenced by the EMER CANCLE pb
  • If the stick is released, the speed will return to Vmo/Mmo. The protections will allow a momentary increase in airspeed up to Vmo+16 / Mmo+0.04 to permit any necessary maneuvering, but then the speed will again slow to the limit
  • Positive spiral static stability is introduced to 0° bank angle (instead of 33° in NORMAL LAW) so that with the side stick released the A/C always returns to 0° of bank. The bank angle limit is reduced from 67° to 40°
  • If high speed protection is active, positive spiral stability occurs at all bank angles, and control pressure is required to hold any bank angle greater than 0
  • It is possible to over speed the A/C. The computers merely limit the max attainable airspeed
32
Q

When a pilot rolls into a bank, what is provided by the flight control laws?

A
  • In “flight” mode of NORMAL LAW, roll control is a roll rate demand. Side stick inputs commands the ailerons, spoilers 2-5, and the rudder to achieve the commanded roll rate with bank angle protection, turn coordination, and Dutch roll damping
  • The roll rate demanded by the pilot is proportional to side stick deflection. When the side stick is neutral, the ailerons and spoilers are positioned to maintain the roll rate at 0° per second. This results in a constant bank angle
  • When the side stick is displaced laterally, increasing roll rates are commanded. At full deflection, a roll rate of 15° per second is commanded in NORMAL LAW. The ailerons and spoilers are positioned as necessary to achieve the commanded roll rate
  • The side stick position cannot be used as a reference to determine the actual positions of flight control surfaces
  • In normal turns (up to 33°) pitch trim is automatic and assists the pilot in maintaining altitude
  • If the bank is increased beyond 33° and the side stick is released, the A/C would return to 33° of bank. This is known as positive spiral stability
  • Positive spiral stability is a characteristic programmed into the flight control computers, which returns the A/C to a more stable condition (0° if high speed or AOA protection is active)
  • Beyond 33° of bank, positive spiral stability is active and automatic pitch trim is inhibited. To maintain a bank angle greater than 33°, continuous side stick pressure must be used. Also, continuous back pressure will be needed to maintain altitude since automatic pitch trim is inhibited
33
Q

The pilots find themselves in ALTERNATE LAW. Describe the indications and available protections, and flight control logic

A
  • In most cases, a single system component failure will not cause a flight control degradation (except jammed stabilizer causes degradation)
  • Indications would be amber Xs and an EW/D message. The ECAM states PROT LOST, but maneuver protection is still available
  • AP availability in ALTERNATE LAW depends on the failures that caused the degradation. Generally speaking, if the failures DO NOT affect a primary flight control surface, the AP should be available
  • Pitch is the same as NORMAL LAW, roll is direct (not roll rate demand), and yaw loses turn coordination
  • Attitude, high speed and AOA protections are lost. They are replaced by high speed stability and low speed stability respectively
  • High speed stability activates just prior to the over speed warning. Nose down trim is inhibited
  • Low speed stability activates just prior to the stall warning. Nose up trim is inhibited
  • The pilot can override the stabilities and over speed or stall the A/C
  • In ALTERNATE LAW, turn coordination is always lost regardless of FAC status. Yaw damping, rudder trim and rudder limiting is available if a FAC is operational
  • Instead of commanding a specific roll rate, there is a direct relationship between side stick position and control surface position. As a result, roll sensitivity now changes with A/C speed and amount of side stick deflection
  • Bank angle protection is not available in ALTERNATE LAW. Roll commands are carried out directly without modification
  • Depending on the failure combination, the maximum roll rate may be as much as twice what it was in NORMAL LAW
  • Attitude protection is lost and the green “=“ signs on the PFD are replaced with amber Xs. There are now no limits on how far a pilot can pitch or roll the A/C. The A/C can roll beyond the amber Xs. Positive spiral stability is also lost.
34
Q

The pilots finde themselves in DIRECT LAW. Describe the indications, protections, and flight control logic

A
  • When in ALTERNATE LAW, there is no landing mode that would provide consistent control during landing for all possible failure combinations. Consequently, the flight controls transition to DIRECT LAW when the landing gear is extended and AP is off
  • DIRECT LAW is very unlikely in flight. It usually results from lowering the gear while in ALTERNATE LAW
  • An ECAM message is generated and says “PROT LOST”. Unlike in ALTERNATE LAW, this is now true. There are no protections or stabilities available in DIRECT LAW
  • The message “USE MAN PITCH TRIM” in amber is displayed on the FMA because automatic pitch trim is lost
  • Pitch control is direct. Load factor demand is lost. Pitch sensitivity or control is a factor of airspeed and the amount of flight control deflection. Roll control is the same as ALTERNATE LAW (direct relationship with no protections)
35
Q

The pilots find themselves in MECHANICAL BACKUP. What functions are available?

A
  • MECHANICAL BACKUP control is provided for the rudder and THS in the event of a complete loss of flight control computers or electrical power, provided that there is hydraulic pressure
  • Although the A/C can be flown indefinitely in this condition, it is intended to be used only as long as it takes to restore the computers
  • Note the EW/D warning message and red “MAN PITCH TRIM ONLY” indication on the FMA. There isn’t a specific mechanical backup ECAM message
  • The side stick are inoperative. Pitch is controlled with the trim wheel via the mechanical connection to the pitch system
  • Roll and yaw are controlled through the rudder pedals and the mechanical connection to the rudder
  • In reality, the failure of only 4 flight control computers may result in mechanical backup: both ELACs and SEC 1 and 2 fail, all computerized pitch control is lost. In this case, because SEC 3 is still available, the side sticks can control roll using one spoiler on each wing, but pitch control is mechanical
36
Q

FAC Functions

A

Yaw Control (turn coordination, rudder travel limiter, rudder trim, yaw damper)
Airspeed protection computations (alpha PROT, hi/lo)
Windshear protection
Low energy warning
THS

37
Q

SEC Functions

A 
Spoilers
Abnormal Attitude
Direct Roll
Direct Pitch
Alternate Pitch
Normal Roll
38
Q

ELAC Functions

A 
Normal Elevator, Aileron, Pitch and Roll
Aileron droop
Direct pitch & roll
Alternate pitch
Abnormal attitude
Autopilot orders
39
Q

What happens when Alpha Prot engages?

A

Alpha is commanded instead of load factor
Speed brake is retracted
AP disengages
Pitch trim is inhibited

40
Q

Normal Law Protection

A 
Bank Angle Protection
Speed Protection
Load factor protection
AOA protection
Pitch angle protection
41
Q

Low Energy Warning Inhibited when

A 
Normal law not active
Flaps 1 or 0
Alpha floor
TOGA
RA failure
Altitude above 2000 RA or below 100 RA
GPWS alert
42
Q

Wing Tip brakes engage when

A

Runaway
Over speed
Asymmetry
Movement uncommanded

43
Q

Ditching pb closes

A 
Cargo isol valve
Ram air inlet valve
Avionics inlet and extract valve
Pack flow control valves
Outflow valve

Spirit (49 decks)

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