6.
Push the line key adjacent to the the LGCIU1 page comes into view.
LGCIU1 indication.
7.
Push the NEXT PAGE key. the LGCIU1 page comes into view.
8.
Push the line key adjacent to the On the MCDU 1(2): LANDING GEAR SIMULATION - the LGCIU1 LANDING GEAR SIMULATION indication. page comes into view.
9.
Push the line key adjacent to the On the MCDU 1(2):
NOSE + LH + RH indication. - the LGCIU1 NOSE + LH + RH page comes into view.
10.
Push the line key adjacent to On the MCDU 1(2):
1EFF : ALL 1 31-10-00Page 219 1 1 Feb 01/03 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------the UP LOCKED indication - the LGCIU1 NOSE + LH + RH page comes into view.
On the panel 402VU:
-
the three UNLK legends come on (red)
-
the three downlock symbols go off
11. Push the line key adjacent to On the MCDU 1(2):
the DOWN LOCKED indication. - the LGCIU1 NOSE + LH + RH page comes into view.
On the panel 402VU:
-
the three UNLK legends go off
-
the three downlock symbols come on (green).
12. Push the line key adjacent to
the RETURN indication until the
CFDS menu page comes into view.
(2)
Do the operational test of the anti-skid inhibition (Ref. TASK 32-42-00-710-003) .
(3)
Do the operational test of the autobrake deceleration rate arming (Ref. TASK 32-42-00-710-005).
(4)
Do the operational test of the GPWS ground self-test function (Ref. TASK 34-48-00-710-001).
Subtask 31-10-00-710-087
R AR. Test Program after Removal/Installation of the Panel 403VU
(1) Do the operational test of the GPWS ground self-test function (Ref. TASK 34-48-00-710-001).
1EFF : ALL 1 31-10-00Page 220 1 1 Feb 01/03 1 1 1CES 1 1EFF : ALL 1 31-10-00Page 221 1 1 May 01/04 1 1 1CES 1 1EFF : ALL 1 31-14-25Page 201 1 1 Aug 01/98 1 1 1CES 1 1EFF : ALL 1 31-14-25Page 202 1 1 Aug 01/98 1 1 1CES 1
Subtask 31-10-00-710-088
AS. Test Program after Removal/Installation of the Panel 500VU
(1) Do the operational test of the general illumination (Ref. TASK 33-12-00-710-001).
(2) Do the operational test of the Audio Management Unit (Ref. TASK 23-51-00-710-001).
(3) Do the brightness test of the EFIS/ECAM switching functions (Ref. TASK 31-60-00-710-002).
(4) Do the operational test of the PFD/ND/upper and lower ECAM Display Units (DU) (Ref. TASK 31-60-00-710-003).
(5) Do the operational test of the angle-of-attack warning (Ref. TASK 34-10-00-710-007).
(6) Do the operational test of the GPWS ground self-test function (Ref. TASK 34-48-00-710-001).
Subtask 31-10-00-710-092
AT. Test Program after Removal/Installation of the Panel 619VU
R R (1) Do the functional test of the remote ATC control box (Ref. TASK 34-52-00-720-009).
Subtask 31-10-00-710-093
AU. Test Program after Removal/Installation of the Panel 620VU
R R (1) Do the functional test of the remote ATC control box (Ref. TASK 34-52-00-720-009).
OVERHEAD CONTROL AND INDICATING PANEL (25VU) - MAINTENANCE PRACTICES____________________________________________________________________
R TASK 31-14-25-860-002
R Floor Path Emergency-Lighting Inhibition With Removal of the Overhead Panel
R 25VU
R 1. Reason for the Job__________________
R Self Explanatory
R 2. Job Set-up Information______________________
R A. Fixtures, Tools, Test and Support Equipment
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R No specific blanking caps
R B. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
R from the External Power
R 31-14-25-991-001 Fig. 201
R 3. Job Set-up__________
R Subtask 31-14-25-862-052
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本文链接地址：A320飞机维护手册 AMM 指示/记录系统INDICATING/RECORDING SYSTE(76)
