Flap Rigging Pin Locations
Figure 403/TASK 27-54-49-991-005
R 1EFF : 001-049, 051-061, 101-103, 201-203, 1 27-54-49Page 425 1301-399, 1May 01/05 1 1 1CES 1R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
(Ref. Fig. 403A/TASK 27-54-49-991-005-A)
**ON A/C ALL
Subtask 27-54-49-941-050
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put the warning notice(s) in position to tell persons not to operate the flaps.
(3)
Put a warning notice in position to tell persons not to operate the landing gear doors.
Subtask 27-54-49-860-050
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 the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap/slat control lever in the cockpit.
Subtask 27-54-49-865-050
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
Flap Rigging Pin Locations
Figure 403A/TASK 27-54-49-991-005-A
R 1EFF : 062-099, 104-149, 151-199, 204-299, 1 27-54-49Page 427 1401-499, 1Aug 01/05 1 1 1CES 1 Subtask 27-54-49-010-050
D. Get Access
(1)
Open the applicable MLG door (Ref. TASK 32-12-00-010-001):
-
for FIN 6205CM open 734
-
for FIN 6255CM open 744.
(2)
Put the access platform in position below the applicable access panel.
(3)
Remove the applicable access panels: FOR 6205CM remove 193AB, 193BB remove 573AB, 573BB (Ref. TASK 57-51-37-000-002). FOR 6255CM remove 194AB, 194BB remove 673AB, 673BB (Ref. TASK 57-51-37-000-002).
4. Procedure
_________
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 402/TASK 27-54-49-991-001) R **ON A/C 062-099, 106-149, 151-199, 204-299, 401-499,
(Ref. Fig. 402A/TASK 27-54-49-991-001-B)
**ON A/C 104-105,
(Ref. Fig. 402B/TASK 27-54-49-991-001-A)
**ON A/C 301-399,
(Ref. Fig. 402C/TASK 27-54-49-991-001-C)
**ON A/C ALL
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 27-54-49-480-050
A. Installation of Support Equipment
(1) Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) on the applicable torque shaft (Ref. TASK 27-50-00-400-003).
Subtask 27-54-49-740-061
B. 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.
-
push (in) the NEXT PAGE button. - the MCDU shows the next page of the SFCC 1 menu.
-
push (in) the line key SYSTEM - the MCDU shows the SFCC 1 FLAP
DATA FLP >. SYSTEM DATA menu.
-
push (in) the line key < PPU. - the MCDU shows the PPU DATA page(s):
1EFF : ALL 1 27-54-49Page 429 1 1 May 01/04R 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱5(102)
