Flight controls Flashcards
What flight controls do we have on each wing?
5 x slats
5 x spoilers
2 x flaps
1 x aileron (at the end of the wing)
How are the flight controls - controlled and then actuated?
Fly by wire
“All flight controls are ELECTRONICALLY CONTROLLED and HYDRAULICALLY activated”
How does the flight control system work
(Caution - check answer)
- Demand made by pilot
- Goes to F/CTR computer
- Signal sent to actuator
- Actuator moves surface
- Response feedback back to F/CTR computer
Note: in normal law the computers prevent excessive manoeuvres and keeps us inside the flight envelope in the pitch and roll axis
Flight control - side stick
Are the FO AND CAPT side sticks mechanically linked?
No - they are not mechanically linked
Side stick - what is the SOP for disconnecting autopilot in flight?
Side stick red push button.
Why? Because this prevents an ECAM warning (albeit you still get the cavalry noise)
Side stick - Dual Inputs
They are algebraically added. Therefore:
- Half side deflection from CAPT plus half side stick deflection from FO (in same direction) = full deflection
- Full bank left from CAPT and full bank right from FO = no deflection
When doing flight control check (during taxi) - remember to look at the ECAM display (not the PFD)
Side stick - Priority
What is shown if Capt takes priority from the PF?
- Red arrow appears in front of the person that lost control (FO) and points to the person that has control (Capt)
- A green “CAPT” light illuminates (I.e says who now has control)
Side Stick - how do you take control from copilot?
Press and hold red pb for 40 seconds (this then semi locks out the co-pilot)
Does not fully lock because the co-pilot could request control back again
Rudder Trim Switch. What is the impact of autopilot on?
Autopilot on - turning the trim knob on the pedestal has no impact
What are the Cockpit THS controls? What happens if you manually control them in cockpit
2 x THS Hand wheels
If grab, you override the automatic computer and are directly controlling the electric motors which in turn move THS
What flight control computers does the a320 have?
Caution - not sure if below is 100% correct yet
- 2 x ELAC [Elevator and Aileron Computer]
- 3 x SEC [Spoiler and Elevator Computer] (note: also controls the standby elevators and stab control)
- 2 x FAC [Flight Augmentation Computer]
Not a computer as such but there are also:
2 x FCDC [Flight Computer Data Concentrators]
Elevators. Basic components of the system?
Each elevator is:
- Driven by 2 x electrically controlled hydraulic servo jacks
- Only 1 servo jack active at a time (the other is in damping mode)
- Left Elevator (Green Hyd). Right Elevator (Yellow Hyd) [Instructor advised don’t need memorise colours]
Elevators - how do they work in normal conditions?
There are 2 servojacks per elevator
A) 1 x servojack does all of the work; and
B) 1 x servo-Jack “relaxes” and simply follows what the other is doing (“Damping mode”) [instructor likened it to floating around)
Elevators - how do they work in abnormal (neither hydraulic Jack being controlled electrically)?
Reverts to “Central Mode” (elevator locks at the central / neutral position)
Elevators. What modes do the servojacks have?
- Active (the servojack is electronically controlled)
- Damping (the jack follows the surface movement)
- Centering (elevator locks at center/neutral)