CALLS

• MECH: Provides call facility between the cockpit and the ground mechanic.
• EMER:
  • ON: CALL PRIO CAPT message appears at ' ALL ' Attendent Indication Panels.
  • ON Light: Illuminates White in case of cockpit Emergency Call.
  • Call Light: Illuminates Amber in case of cockpit or cabin Emergency Call.
• ALL: CAPTAIN CALL message appears at ' ALL ' Attendant Indication Panels.
• FLT REST: CAPTAIN CALL message appears at corresponding Attendant Indication Panel.
• CAB REST: CAPTAIN CALL message appears at corresponding Attendant Indication Panel.
• FWD: CAPTAIN CALL message appears at corresponding Attendant Indication Panel.
• MID: CAPTAIN CALL message appears at corresponding Attendant Indication Panel.
• EXIT: CAPTAIN CALL message appears at corresponding Attendant Indication Panel.
• AFT: CAPTAIN CALL message appears at corresponding Attendant Indication Panel.

Capt & XXX
 

Horn Shutoff
 

Command
 

Crew

• ON: The valve is opened, low pressure Oxygen is supplied to the Masks.
• OFF: The valve is closed. The illuminates WHITE.

Passengers SYS ON Light
Illuminates WHITE when the control of the Oxygen Mask doors is activated, it remains on until TMR RESET pb is activated.

Oxygen Mask MAN ON

• AUTO: Mask doors open automatically when cabin altitude exceeds 14000 ft.
• Pressed: Mask doors open.

GPWS Flap Mode

• OFF: Flap Mode is inhibited ( Mode 4 ).

GPWS G/S Mode

• OFF: Glide Slop Mode is inhibited ( Mode 5 ).

GPWS SYS

• OFF: All warnings are inhibited.
• Fault Light: Illuminates AMBER associated with ECAM caution when a malfunction of the GPWS is detected.

ATTND ADV pb

• ON: Used to inform cabin crew for imminent takeoff or landing.

Wiper Selector
Each rotary selector controls its Wiper at either low or high speed.

Rain RPLNT
Controls the application of Rain Repellent fluid to the respective front windshield.

MAN ON Pushbutton ( Guarded )

• AUTO: In flight, in case of normal AC supply loss, the emergency generator is Automatically started.
• When Pressed: The emergency generator runs and is connected to the aircraft network.

EMER GEN Fault Light
The lights comes on RED when the Emergency Generator is not supplying and normal AC supply is lost in flight.

Land Recovery Pushbutton Switch
When Pressed: The AC Land Recovery and the DC Land Recovery bus are recovered and the following equipment is restored, LGCIU 1, SFCC 1, ILS 1.

EMER ELEC PWR Test Button
When Pressed: The Emergency Generator runs and supplies the DC ESS BUS and the AC ESS BUS.

Jettison Active

• OFF: Guarded position. The Jettison system is not active.
• ON: The Jettison system is activated provided the ARM pushbutton is selected ON.
• Open: Illuminates when the Jettison valves are open.

Jettison Arm

• OFF: Guarded position. The Jeffison system is disarmed.
• ON: The Jettison is armed and can be activated through the ACTIVE pushbutton.

Fuel Inner Tank Split ( L / R )

• OFF: The SPLIT valve is open. The Inner Tank is used as a single Tank.
• ON: The valve closes and the Inner Tank is Split in two parts. The forward part is feeding the inboard engine. The aft part is feeding the outboard engine and will receive any fuel transferred to Inner Tank from center, outer or trim Tank. The light illuminates AMBER.
• SHUT: Illuminates BLUE when the valve is Shut.

Flight Control

• PRIM 1: Control the flight control Primary computers ( FCPC ).
  • ON: The following functions are provided by each computer: Normal pitch, Normal Lateral, MLA Speed Brakes, Pitch Alternate, Pitch Direct, Roll Direct, Yaw Alternate, Ailerons Droop, Abnormal Attitude Law, Autopilot Order Acquisition
  • OFF: The corresponding computer is not active.
  • FAULT: Illuminates AMBER accompanied by ECAM caution activation when a failure is detected.
• SEC 1: Control the flight control Secondary computer ( FCSC ).
  • ON: The following functions are provided by each computer: Pitch Direct, Roll Direct, Yaw Alternate, Rudder Trim, Rudder Travel.
  • OFF: The corresponding computer is not active.
  • FAULT: Illuminates AMBER accompanied by ECAM caution activation when a failure is detected.