(c) Remove the two nuts [2], lockwashers [3] and washers [4] from both terminal studs on
the Dual Battery RCCB [1].
(d) Remove the nut [2], lockwasher [3] and washer [4] from the top terminal stud on the
Static Inverter RCCB [1].
NOTE: This step must be done because the terminals are close together on the same
wire.
(e) Remove the wires from the terminal studs.
(f) Remove the control wires from the connector on the Dual Battery RCCB [1] SWPM
20-83-00.
NOTE: Be sure to install an identification tag on wire so that you can install the wire into
the correct socket later.
(g) Remove the two screws [5] that hold the Dual Battery RCCB [1] to the panel.
(h) Remove the Dual Battery RCCB [1].
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-31-41
Page 403
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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