Flight Control Computers (ELAC / SEC / FAC) & Hydraulics
Click to toggle fault/pressurization
ECAM Status & Reconfiguration Assessment
ELEV: SEC1/SEC2 | ROLL: AIL+SPOIL
ELAC 1 & 2 offline triggers automatic reconfiguration to Alternate Law 2 without pitch/bank envelope protection; pitch elevator command transfers seamlessly to SEC 1 & 2, while roll transitions to ailerons and roll spoilers with direct stick proportionality.
Flight Envelope Protections
AIRBUS 320 SPECS
| Protection Feature | Status | Mode |
|---|
Control Surface Deflection Telemetry
LIVE ANGLES
Left Elevator
0.0°
Right Elevator
0.0°
Left Aileron
0.0°
Right Aileron
0.0°
Rudder Yaw
0.0°
THS Pitch Trim
0.0°
Side-Stick Dynamic Control Test
DRAG / TOUCH
PITCH DEMAND (Y) / ROLL DEMAND (X)
Stick X: +0.60
Stick Y: -0.45