TASK 24-34-31-400-801-001
3. Static Inverter RCCB Installation
(Figure 401, Figure 402)
A. General
(1) The Static Inverter RCCB, C1341, is located on the J9 Battery Shield in the Main Equipment
Center.
B. References
Reference Title
24-22-00-860-813 Supply External Power (P/B 201)
24-31-21-710-801 Main Battery Charger Operational Test (P/B 501)
FIM 24-31 TASK 801 P5-13 ELEC Light Message BITE Procedure
SWPM 20-83-00 Standard Wiring Practices Manual
C. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
1 Static inverter RCCB 24-34-31-01-015 ILF 686, 707-710,
854-856, 862, 871-874
24-34-31-02-015 ILF 562, 588, 592-596,
833, 834
D. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
121 Forward Cargo Compartment - Left
122 Forward Cargo Compartment - Right
E. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
F. Procedure
SUBTASK 24-34-31-420-001-001
(1) Do these steps to install the static inverter RCCB [1]:
(a) Hold the RCCB in position.
(b) Install the two screws [5] that hold the RCCB.
(c) Install the wires on the RCCB terminal studs.
(d) Install the two nuts [2], lockwashers [3] and washers [4] on both terminal studs on the
Static Inverter RCCB.
(e) Tighten the nuts to 40-45 inch-pounds (4.5-5.1 Newton meters).
(f) Install the control wires into sockets on RCCB per the identification tags SWPM 20-83-00.
(g) Install the access cover on top of the J9 shield.
SUBTASK 24-34-31-420-002-001
(2) Install the battery connector per the steps that follow:
(a) Gain access to the forward cargo area.
(b) Install the battery connector on the battery.
(c) Install the forward bulkhead liner.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-34-31
Config 1
Page 409
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF 562, 588, 592-596, 686, 707-710, 833, 834,
854-856, 861-863, 871-874
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