2.
On the MCDU:
-
push the line key adjacent to the <LGCIU 1 or the <LGCIU 2 indication. (You can use LGCIU 1 or LGCIU 2 system).
-
push the NEXT PAGE P/BSW.
-
push the line key adjacent to the <LANDING GEAR SIMULATION indication.
-
push the line key adjacent to the <NOSE + LH + RH indication.
-
push the line key adjacent to the <EXTENDED indication.
3.
On the panel 400VU:
-set the landing-gear control-lever 6GA to the UP position.
The MCDU shows the SYSTEMREPORT/TEST/L/G page.
On the MCDU:
-
the applicable LGCIU menu page comesinto view.
-
the applicable LGCIU menu page 2 comes into view.
-
the LANDING GEAR SIMULATION pagecomes into view.
-
the NOSE + LH + RH simulation pagecomes into view.
-
the applicable < goes off.
On the panel 402VU:
-
the landing gear unlock indicatorsshow UNLK (red).
NOTE : The downlock indicators show
____ green when the landing gear is downlocked. The unlock indicators show red when the landing gear is downlocked and the landing-gear control-lever is set to the UP position.
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ACTION RESULT -------------------------------------------------------------------------------
4. On the MCDU:
-push the line key adjacent to the <RETURN indication.
5. On the panel 400VU:
-set the landing gear control lever to the DOWN position.
6. On the MCDU:
-push the line key adjacent to the <RETURN indication 3 times.
-put the BRT switch to off.
5. Close-up
________ Subtask 32-31-00-860-090On the MCDU:
-
the LANDING GEAR SIMULATION pagecomes into view.
On the aircraft:
-
the landing gear doors open correctly.
On the aircraft:
-
the landing gear doors closecorrectly.
On the MCDU:
-you exit the simulation mode.
-the SYSTEM REPORT/TEST/L/G page comes into view.
A. Aircraft Maintenance Configuration
R (1) On the panel 20VU, put the applicable ADIRS IR1/IR2/IR3 switch to the
R OFF position.
(2) Depressurize the Green hydraulic system
(Ref. TASK 29-10-00-864-001).
R (3) If you have energized the aircraft electrical circuits from an
R external source, do the procedure (Ref. TASK 24-41-00-862-002).
R (4) If you have energized the aircraft electrical circuits from the APU,
R do the steps that follow:
R (a) Set the ADIRU 1 or 3 to OFF.
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R R R (b) De-energize the aircraft electrical circuits supplied from the APU (Ref. TASK 24-41-00-862-002).
Subtask 32-31-00-869-108
B. Flight Configuration Precautions
(1) Put the aircraft back to the ground configuration (Ref. TASK 32-00-00-860-002).
Subtask 32-31-00-942-086
C. Removal of Equipment
(1) Remove the safety barriers.
(2) Make sure that the work area is clean and clear of tool(s) and other items.
(3) Remove the warning notice(s).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Functional Test of the Normal Extension and Retraction of the Nose Landing Gear
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific rod (not metal) No specific safety barriers No specific warning notice 98F32304000000 4 FALSE TARGET
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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