(4) Make sure that the the ground safety locks are installed on the landing gear (Ref. TASK 32-00-00-481-001).
Subtask 27-54-49-860-064
B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Extend the flaps fully (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap/slat control lever in the cockpit.
(3)
Extend the No. 1 to No. 5 spoilers (Ref. TASK 27-60-00-866-002).
(4)
Make sure that a COLLAR-SAFETY, SPOILER is on the piston rod of each servo-control.
Subtask 27-54-49-865-068
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
Subtask 27-54-49-010-063
D. Get Access
(1)
Open the applicable MLG door (Ref. TASK 32-12-00-010-001).
(2)
Put the access platforms in position below the applicable access panels.
(3)
Remove the applicable access panels:
-
for the left wing, remove 193AB, 193BB, 573AB, 573BB, 573CB, 575AB, 575BB, 575CB, 575DB, 575EB, 575FB, 575GB
-
for the right wing, remove 194AB, 194BB, 673AB, 673BB, 673CB, 675AB, 675BB, 675CB, 675DB, 675EB, 675FB, 675GB.
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4. Procedure
_________
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
EDGE:
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Subtask 27-54-49-740-068
A. Do a Check of the Position Pick-Off Units (PPUs) on the Centralized Fault Display System (CFDS)
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Get access to the SYSTEM REPORT/TEST (F/CTL) page on the Multipurpose Control Display Unit (MCDU) (Ref. TASK 31-32-00-860-006).
(3)
Do a check of the flap PPU angles (deg) at the slat/flap control lever position FULL on the MCDU as follows:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU: On the MCDU:
-push (in) the line key < SFCC - the MCDU shows the SFCC 1 menu.
1.
2.
Push (in) the NEXT PAGE button. - the MCDU shows the next page of the SFCC 1 menu.
3.
Push (in) the line key SYSTEM - the MCDU shows the SFCC 1 FLAP DATA FLP >. SYSTEM DATA menu.
4.
Push (in) the line key < PPU. - the MCDU shows the PPU DATA page(s): Refer to Table 1.
NOTE : The APPU and the FPPU synchro
____ angles must agree within 1.3 deg. The LH APPU and the RH APPU synchro angles must agree within
0.45 deg.
R 1EFF : ALL 1 27-54-49Page 404 1 1 Aug 01/02 1 1 1CES 1
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
5. Write down the APPU and the FPPU angles (deg) shown on the display or push (in) the line key PRINT > to get a print-out of the screen.
NOTE : These angles, shown at
____
removal, will be used as a
datum. They will let you
compare the APPU and the
FPPU angles after the
installation of the
actuators (Ref. TASK 27-54-49-400-001), (Ref. TASK
27-54-49-400-002), (Ref.
TASK 27-54-49-400-003),
(Ref. TASK 27-54-49-400-004).
6.
Push the line key < RETURN frequently until the CFDS menu page is shown.
7.
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(97)
