REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R **ON A/C 106-149, 221-228, 231-299, 301-399, 401-499,
28-23-41-991-002-A Fig. 402A
**ON A/C ALL
3. Job Set-up
__________
Subtask 28-23-41-650-050
A. Defuel the wing and center tanks (Ref. TASK 28-25-00-650-001).
Subtask 28-23-41-861-050
B. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002). Subtask 28-23-41-869-050
C. On the panel 40VU, make sure that :
-the FUEL/X FEED pushbutton switch 4QE is not pushed in. (The ON and OPEN legends of the pushbutton switch are off).
Subtask 28-23-41-862-050
D. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 28-23-41-010-050
E. Get access to the Avionics Compartment
(1)
Put the access platform in position under the main door of the right main gear.
(2)
Open the main door of the right main gear (Ref. TASK 32-12-00-010-001).
(3)
Remove the manhole cover 148AZ (Ref. TASK 57-17-11-000-001).
(4)
Remove the crossfeed valve actuator 5QE (Ref. TASK 28-23-51-000-001).
1EFF : ALL 1 28-23-41Page 402 1 1 Aug 01/05 1 1 1CES 1 Subtask 28-23-41-941-051
F. You must obey the special fuel safety procedures when you work in the fuel tank (Ref. TASK 28-10-00-910-001) (Ref. TASK 28-10-00-910-002).
4. Procedure
_________ (Ref. Fig. 401/TASK 28-23-41-991-001) R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220, 229-230,
(Ref. Fig. 402/TASK 28-23-41-991-002) R **ON A/C 106-149, 221-228, 231-299, 301-399, 401-499,
(Ref. Fig. 402A/TASK 28-23-41-991-002-A) R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220, 229-230,
Subtask 28-23-41-020-050
A. Removal of the Fuel Crossfeed Valve (10QM)
(1)
Put a container 1USgal (4l) below the valve (3), the pump (19) and the connections between the lines (6) and (7). (Ref. Fig. 401/TASK 28-23-41-991-001, 402/TASK 28-23-41-991-002)
(2)
Remove the nuts (12), the washers (13) and the bolts (14) and disconnect the bonding strips (11).
(3)
Remove the nut (23), the bolt (25) and disconnect the bonding strip (24).
(4)
Loosen the nut (27) and disconnect the line (26).
(5)
Remove the screws (22) and the washers (21).
(6)
Loosen the nuts (28) (Ref. Detail E).
(7)
Remove the cross-union (5) together with the lines (4) and (6). NOTE : Play at the connections between the line (4) and the
____ cross-union (5), and, the line (6) and the cross-union (5) will help you release the lines.
1EFF : ALL 1 28-23-41Page 403 1 1 Aug 01/05 1 1 1CES 1
Component location
Figure 401/TASK 28-23-41-991-001
1EFF : ALL 1 28-23-41 Page 404
1 1 Feb 01/98
1 1
1CES 1
Crossfeed Valve
Figure 402/TASK 28-23-41-991-002
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 28-23-41Page 405 1201-220, 229-230, 1Aug 01/05 1 1 1CES 1
Crossfeed Valve Figure 402A/TASK 28-23-41-991-002-A
R 1EFF : 106-149, 221-228, 231-299, 301-399, 1 28-23-41Page 406 1401-499, 1Aug 01/05 1 1 1CES 1
(8)
Remove and discard the O-ring (20).
(9)
Remove the screws (17).
(10) Remove the valve (3), and remove and discard the O-ring (15). NOTE : Play at the connections between the lines (1) and (2) will
____
help you release the valve (3).
(11) Remove and discard the O-rings (18) and (29). R **ON A/C 106-149, 221-228, 231-299, 301-399, 401-499,
Subtask 28-23-41-020-050-A
A. Removal of the Fuel Crossfeed Valve (10QM)
(1)
Put a container 1USgal (4l) below the valve (3), the pump (19) and the connections between the lines (6) and (7). (Ref. Fig. 401/TASK 28-23-41-991-001, 402A/TASK 28-23-41-991-002-A)
(2)
Remove the nuts (12), the washers (13) and the bolts (14) and disconnect the bonding strips (11).
(3)
Remove the nut (23), the bolt (25) and disconnect the bonding strip (24).
(4)
Loosen the nut (27) and disconnect the line (26).
(5)
Remove the screws (22) and the washers (21).
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUEL 燃油3(138)
