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ACTION RESULT -------------------------------------------------------------------------------
2. On the ECAM CP:
-push (in) the EMER CANC P/BSW.
3. On the MCDU:
-push (in) the DOWNLOCKED P/BSW.
-you can hear the warning chime.
On the Landing-Gear Normal Control-Lever (6GA):
-
the red DOWN arrow light comes on.
The warning chime stops.
On the panels 130VU and 131VU:
-
the MASTER WARN lights go off. On 402VU:
-
the UNLK (red) indicator lights stay on.
On the ECAM upper DU:
-
the L/G GEAR NOT DOWN and L/G GEAR NOT DOWNLOCKED display goes out of view
-
the UNLK (red) indicator lights go out and the LKD (green) indicator lights come on.
On the Landing-Gear Normal Control-Lever (6GA):
-
the red DOWN arrow light goes off. On the ECAM lower DU:
-
the WHEELS page shows the wheels in the DOWN position.
NOTE : The amber crosses will stay on screen because the No 2 LGCIU circuit breaker is open.
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4.
Push (in) the RETURN P/BSW until - the CFDS menu page shows.
the CFDS menu page shows.
5.
Push in the MCDU MENU P/BSW.
5. Close-up
________
Subtask 32-61-00-865-050
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2GA.
Subtask 32-61-00-860-051
B. Aircraft Maintenance Configuration
(1)
Put the aircraft back to the ground configuration (Ref. TASK 32-00-00-860-002).
(2)
Fully retract the flaps (Ref. TASK 27-50-00-866-009).
(3) Cockpit Configuration R
R (a) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002). R (b) On the panel 50VU:
-push (in) the FADEC GND PWR 1 or 2 P/BSW. Make sure that the applicable P/BSW ON light goes off.
(4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 32-61-00-942-051
C. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
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(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
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LANDING GEAR - POSITION INFORMATION - DESCRIPTION AND OPERATION
_______________________________________________________________
1. General
_______
Two Landing Gear Control and Interface Units (LGCIUs) supply an interface between the landing gear (L/G) system and other systems which require L/G position information. Each LGCIU controls the position relays.
The L/G control lever supplies position information, this is done independently from the LGCIUs. The switch contacts operated by the control-lever (which are not used to control L/G operations), are used for this function.
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