(14)
Apply SEALANTS (Material No. 09-001) around the electrical backshell
(8) to seal it to the rear spar.
(15)
Connect the electrical connector (7) to the electrical backshell (8).
(16) Clean the electrical connector (7) with a MISCELLANEOUS (Material No. R 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(17)
Apply a continuous layer of STORAGE PRESERVATION (Material No. 15-008) to the electrical connector (7).
(18)
Identify the cable ends for the probes that follow and connect them to the correct terminals (Ref. TASK 28-42-15-400-005):
-FOR 57QT, 58QT 21QT1(21QT2) 54QT1(54QT2) 23QT1(23QT2) 25QT1(25QT2) 27QT1(27QT2) 29QT1(29QT2) 59QT1(59QT2) 61QT1(61QT2)
-FOR 63QT, 64QT R 54QT1(54QT2) 56QT1(56QT2) 26QT1(26QT2).
(19)
Identify the cable ends for the sensors that follow and connect them to the correct terminals (Ref. TASK 28-46-15-400-009) (Ref. TASK 28-46-17-400-001) (Ref. TASK 28-46-19-400-001):
-
FOR 57QT, 58QT 16QJ1(16QJ2) 29QJ1(29QJ2) 38QJ1(38QJ2) 39QJ1(39QJ2) 40QJ1(40QJ2) 17QJ1(17QJ2)
-
FOR 63QT, 64QT 23QJ1(23QJ2) 24QJ1(24QJ2) 56QJ1(56QJ2) 25QJ1(25QJ2) 26QJ1(26QJ2) 27QJ1(27QJ2) FOR 57QT, 63QT
(20)
Identify the cable ends for the dualcomp (53QT) and connect them to the correct terminals (Ref. TASK 28-42-46-400-001). FOR 58QT, 64QT
(21)
Identify the cable ends for the ultracomp (52QT) and connect them to the correct terminals (Ref. TASK 28-42-48-400-001).
(22)
Attach the wing tank harness to the aircraft structure as follows:
-
install the related loop-clamps (3) and the related bolts (2)
-
install the related cable-ties (1) inboard of RIB15
-
install the related cable-ties (1) outboard of RIB15.
(23)
Apply SEALANTS (Material No. 09-001) to the bolts (2) and their related anchor nuts.
1EFF : 301-302, 1 28-42-43Page A432 1 1 Feb 01/05 1 1 1CES 1 1EFF : 303-399, 1 28-42-43Page A433 1 1 Feb 01/05 1 1 1CES 1 1EFF : 303-399, 1 28-42-43Page A434 1 1 Feb 01/05 1 1 1CES 1R **ON A/C 301-399,
R **ON A/C 303-399,
R Subtask 28-42-43-420-091-A
R B. Installation of the Wing Tank Harness 57QT (58QT), 63QT (64QT)
R (1) Get access to the opening 540BB(640BB).
R (2) Identify and attach each piece of string to its applicable wing tank
R harness cable.
R (3) Attach the related connectors together at all the ends of the wing
R tank harness with adhesive tape.
R NOTE : This will help you move the wing tank harness through its____
R conduit.
R (4) Use the string to carefully pull the wing tank harness through its
R conduit. When you install the wing tank harness make sure that it
R does not catch.
R (5) Remove and discard the adhesive tape and the string from every end of
R the wing tank harness.
R (6) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-013) to the
R threads of the electrical backshell (8).
R (7) Install the new O-ring (4) on the electrical backshell (8).
R (8) Install the electrical backshell (8) in the rear spar.
R (9) Get access through the opening 574BB(674BB).
R (10) Install the washer (5) and the nut (6).
R (11) TORQUE the nut (6) to between 1.16 and 1.27 m.daN (102.65 and 112.38
R lbf.in).
R (12) Use a MISCELLANEOUS (Material No. 19-003) to remove unwanted adhesive
R from the electrical backshell (8) and the nut (6).
R (13) Safety the nut (6) to an adjacent tag with MISCELLANEOUS (Material
R No. 19-010).
R (14) Apply SEALANTS (Material No. 09-001) around the electrical backshell
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FUEL 燃油6(14)
