(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 484 1 1 May 01/04R 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------Refer to Table 1.
NOTE : The APPU and the FPPU synhro
____ angle must agree within 1.3 deg. The LH APPU and the RH APPU synchro angles must agree within
0.45 deg.
-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
actuator (Ref. TASK 27-54-49-400-003).
-push the line key < RETURN
frequently until the CFDS menu
page is shown.
1EFF : ALL 1 27-54-49Page 485 1 1 May 01/04R 1 1 1CES 1
SFCC 1
PPU DATE (DEG)
DATE:XXX XX UTC:XXXX
LH APPU FPPU RH APPU
***.* ***.* ***.*
***HEX ***HEX ***HEX ***
OTHER SFCC LH APPU FPPU RH APPU ***.* ***.* ***.* *** ***HEX ***HEX ***HEX
<RETURN PRINT>
Table 1 PPU DATA (DEG) displayed on the MCDU at the flap position FULL
(4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 27-54-49-020-060
R C. Preparation for Removal of the Flap Track 3 Actuator
(1) Hold the trailing edge of the flap on supports.
R (2) Use the clamp to hold the carriage in position.
NOTE : This will make sure that the carriage does not move.
____
(3) Remove the applicable torque shafts (2) and (4) and the universal joint (3):
-
FOR 6221CM remove FIN 6222CM (Ref. TASK 27-54-45-000-010) and FIN 6220CM (Ref. TASK 27-54-45-000-007)
-
FOR 6271CM remove FIN 6272CM (Ref. TASK 27-54-45-000-010) and FIN 6270CM (Ref. TASK 27-54-45-000-007).
**ON A/C 001-049, 051-061, 101-105, 201-203,
Subtask 27-54-49-020-055
D. Removal of the Flap Track 3 Actuator 6221CM (6271CM) CAUTION : SUPPORT THE ACTUATOR, WHICH CAN WEIGH UP TO 10.5kg (23.2lbs).
_______ THIS WILL PREVENT DAMAGE TO THE RELATED STRUCTURE AND EQUIPMENT.
(1) Remove the nuts (9), the washer(s) (10), the bolts (7) and the countersunk washers (6).
NOTE : There can be one or two washers (10). Make a note of how many
____ you remove. You can subsequently install the correct number.
(2) Remove the actuator assembly from the structure interface and the flap drive lever.
(3) Prevent damage to the component interface and the adjacent area. R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
Subtask 27-54-49-020-055-A
D. Removal of the Flap Track 3 Actuator 6221CM (6271CM) CAUTION : SUPPORT THE ACTUATOR, WHICH CAN WEIGH UP TO 10.5kg (23.2lbs).
_______ THIS WILL PREVENT DAMAGE TO THE RELATED STRUCTURE AND EQUIPMENT.
(1)
Remove the nuts (8), the washers (9), the bolts (7) and the countersunk washers (6).
(2)
Remove the actuator assembly from the structure interface and the flap drive lever.
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵5(119)
