R 1EFF : 301-399, 1 27-54-49Page 447 1 1 May 01/04 1 1 1CES 1
R (8) Do an electrical bonding check between the flap track 1 and the
R applicable bolt (Ref. TASK 20-28-00-869-002):
R - FOR 6205CM
R in the LH wing bonding position
R - FOR 6255CM
R in the RH wing bonding position.
R (9) Seal the applicable bolt (5), the countersunk washer (6), the washer
R (7) and the nut (8) in the bonding position (Ref. TASK 20-28-00-912-
R 004):
R - FOR 6205CM
R in the LH wing bonding position
R - FOR 6255CM
R in the RH wing bonding position.
R (10) Apply a thin layer of STRUCTURE PAINTS (Material No. 16-021) when the
R sealant you applied before is cured.
R (11) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to the
R remaining bolts (5) the countersunk washers (6), the washers (7) and
R the nuts (8).
R (12) Install the plunging joint (2) and the universal joint (3) so that
R the flanges align with the torque shafts (1) and (4).
R (13) Install the torque shafts (1) and (4):
R - FOR 6205CM
R install 6206CM (Ref. TASK 27-54-45-400-003) and 6204CM (Ref. TASK
R 27-54-45-400-002)
R - FOR 6255CM
R install 6256CM (Ref. TASK 27-54-45-400-003) and 6254CM (Ref. TASK
R 27-54-45-400-002).
**ON A/C ALL
Subtask 27-54-49-080-050
R E. Removal of Support Equipment
(1) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT from
the applicable torque shaft (Ref. TASK 27-50-00-000-003).
R (2) Remove the clamp that holds the carriage in position.
(3) Remove the support from the flap trailing edge.
Subtask 27-54-49-740-063
F. 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:
-push (in) the line key < SFCC
1.
-
push (in) the NEXT PAGE button.
-
push (in) the line key SYSTEM DATA FLP >.
-
push (in) the line key < PPU.
-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.
-push the line key < RETURN frequently until the CFDS menu page is shown.
2. De-energize the electrical circuits (Ref. TASK 24-41-00-862-002).
On the MCDU:
-
the MCDU shows the SFCC 1 menu.
-
the MCDU shows the next page of the SFCC 1 menu.
-
the MCDU shows the SFCC 1 FLAPSYSTEM DATA menu.
-
the MCDU shows the PPU DATA page(s). Refer to Table 1.
1EFF : ALL 1 27-54-49Page 449 1 1 May 01/04R 1 1 1CES 1
Subtask 27-54-49-820-060
G. Adjustment After BITE Test
(1)
Compare the APPU and the FPPU angles (deg) with those that were written down (or printed) before the actuator was removed (Ref. TASK 27-54-49-000-001).
(2)
Make sure that the FPPU angle values agree with the values recorded before the actuators were removed (+/- 0.2 deg).
(3)
Make sure that the APPU angle values agree with the values recorded before the actuators were removed (+/- 0.2 deg).
(4)
Make sure that the APPU/FPPU angles (deg) agree (+/- 1.3 deg).
(5)
Make sure that the LH APPU and the RH APPU angles agree (+/- 0.45 deg).
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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(109)
