(3)
Drain the remaining fuel form the center tank and the vent surge tank (Ref. TASK 28-25-00-650-003).
Subtask 28-11-00-860-061
C. Aircraft Maintenance Configuration
(1)
Fully extend the flaps (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the slat/flap control lever.
(3)
Extend the spoilers fully (Ref. TASK 27-60-00-866-002).
(4)
Make sure that the COLLAR-SAFETY, SPOILER is on each of the spoiler servo-controls.
**ON A/C 001-049, 051-061, 101-103, 201-203,
Subtask 28-11-00-010-057
D. Get Access
(1)
Put the access platform in position below the applicable zone 550 or
650.
(2)
Remove the applicable NACA vent intake 550AB, 650AB (Ref. TASK 28-12-47-000-001).
(3)
Open the MLG doors (Ref. TASK 32-12-00-010-001).
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(4)
Make sure that the GROUND LOCK SLEEVE is on the applicable MLG door actuator.
(5)
Put an access platform in the applicable MLG bay below the access panel 147AZ, 148AZ.
(6)
Remove the applicable access panel 147AZ, 148AZ (Ref. TASK 57-17-11-000-001).
(7)
Put an adjustable access platform below the applicable zone 521(621).
(8)
Put an adjustable access platform below the applicable zone 522(622).
(9)
Put an adjustable access platform in the applicable MLG bays below the Wing tank rear spar.
(10)
Put an adjustable access platform below the applicable zone 574(674).
(11)
Put an adjustable access platform below the applicable zone 575(675).
(12)
Remove the applicable leading-edge access-panels 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522HB, 522JB, 522KB, 522LB, 522NB, 522QB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB, 622HB, 622JB, 622KB, 622LB, 622NB, 622QB.
(13)
Remove the applicable trailing edge access panels 575AB, 575BB, 575CB, 575DB, 575EB, 575FB, 575GB, 575HB, 675AB, 675BB, 675CB, 675DB, 675EB, 675FB, 675GB, 675HB (Ref. TASK 57-51-37-000-004).
(14)
Open the applicable trailing edge panels 574AB, 574BB, 674AB, 674BB.
(15)
Remove the applicable dry-bay access-covers 521AZ, 521BZ, 621AZ, 621BZ (Ref. TASK 57-27-11-000-005).
R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
Subtask 28-11-00-010-057-A
D. Get Access
(1)
Put the access platform in position below the applicable zone 550 or
650.
(2)
Remove the applicable NACA vent intake 550AB, 650AB (Ref. TASK 28-12-47-000-001).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-11-00Page 512 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(3)
Open the MLG doors (Ref. TASK 32-12-00-010-001).
(4)
Make sure that the GROUND LOCK SLEEVE is on the applicable MLG door actuator.
(5)
Put an access platform in the applicable MLG bay below the access
panel 147AZ, 148AZ.
(6)
Remove the applicable access panel 147AZ, 148AZ (Ref. TASK 57-17-11-000-001).
(7)
Put an adjustable access platform below the applicable zone 521(621).
(8)
Put an adjustable access platform below the applicable zone 522(622).
(9)
Put an adjustable access platform in the applicable MLG bays below
the Wing tank rear spar.
(10)
Put an adjustable access platform below the applicable zone 574(674).
(11)
Put an adjustable access platform below the applicable zone 575(675).
(12)
Remove the applicable leading-edge access-panels 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522HB, 522JB, 522KB, 522LB, 522NB, 522QB, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB, 622HB, 622JB, 622KB, 622LB, 622NB, 622QB.
(13)
Remove the applicable trailing edge access panels 574AB, 574BB, 575AB, 575BB, 575CB, 575DB, 575EB, 575FB, 575GB, 575HB, 674AB, 674BB, 675AB, 675BB, 675CB, 675DB, 675EB, 675FB, 675GB, 675HB (Ref. TASK 57-51-37-000-004).
(14)
Remove the applicable dry-bay access-covers 521AZ, 521BZ, 621AZ, 621BZ (Ref. TASK 57-27-11-000-005).
R 1EFF : 062-099, 104-149, 151-199, 204-299, 1 28-11-00Page 513 1401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
4. Procedure 中國航空網 m.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1(107)
