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Boeing 737-600 - Subtask 24-31-11-420-001-001; Subtask 24-31-11-860-055-001; Subtask 24-31-11-710-001-001

Boeing 737-600
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G. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
H. Battery Installation
SUBTASK 24-31-11-420-001-001
(1) Install the battery [1] as follows:
(a) Put the skid plate, equipment, SPL-1633 in position as shown in (Figure 401).
ILF 707-710
CAUTION
DO NOT LET THE BATTERY TOUCH THE CAPSTRIP IMMEDIATELY
BELOW THE BATTERY-MOUNTING-RACK. IF THE BATTERY TOUCHES
THE CAPSTRIP, THEN IT CAN SCRATCH IT. THIS CAN CAUSE SEAL
DAMAGE THAT FORMS WHEN YOU INSTALL THE CLOSE-OUT PANEL.
(b) Have two persons hold each of the battery handles and lift the battery onto the skid plate.
Slide the battery into position.
NOTE: Make sure the terminals point aft.
ILF 562, 588, 592-596, 686, 833, 834, 854-856, 861-863, 871-874
CAUTION
DO NOT LET THE BATTERY TOUCH THE CAPSTRIP IMMEDIATELY
BELOW THE BATTERY-MOUNTING-RACK. IF THE BATTERY TOUCHES
THE CAPSTRIP, THEN IT CAN SCRATCH IT. THIS CAN CAUSE SEAL
DAMAGE THAT FORMS WHEN YOU INSTALL THE CLOSE-OUT PANEL.
(c) Have two persons hold each of the battery handles and lift the battery onto the skid plate.
Slide the battery into position.
NOTE: Make sure the terminals point left.
ILF 562, 588, 592-596, 686, 707-710, 833, 834, 854-856, 861-863, 871-874
(d) Remove the skid plate.
NOTE: You may have to tilt the battery back some to remove the skid plate.
(e) Install the six bolts [2] and washers [3] on the battery mounting brackets.
(f) Connect the electrical connector to the battery.
(g) Connect the battery connector to the battery.
1) Safetywire the battery connector with a 0.020 inch (0.5080 mm) diameter
MS20995CY20 lockwire, G02479, (TASK 20-30-51-910-801).
SUBTASK 24-31-11-860-055-001
(2) Remove the safety tag and close this circuit breaker:
Standby Power Control Unit, M01720
Row Col Number Name
B 1 C01410 SPCU NORMAL
I. Battery Installation Test
ILF 707-710
SUBTASK 24-31-11-710-001-001
(1) Test the battery per the steps that follow:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-31-11
Config 1
Page 409
D633A101-ILF Oct 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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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