(a) Apply one of the parting agents listed to the surface of the receptacle [1] that touches the
receptacle pan.
NOTE: Do not apply the parting agent to the structure or any surface that will have fillet
seal.
1) AC962-73C peelable parting agent, G50365
2) peelable parting agent, G50366
3) AZ 634-2 peelable parting agent, G50367
4) Rexco Partall Coverall Film peelable parting agent, G50368
5) temporary coating, G50369
(b) When the parting agent is dry to touch, apply sealant, A00247 to the surface of the
receptacle [1] that touches the receptacle pan to make a removable faying surface seal
(TASK 51-31-00-390-810).
(c) Put the receptacle [1] in its position on the receptacle pan.
(d) Apply sealant, A00247 to the four bolts [2].
(e) Put the shield [17] in its position.
(f) Install the bolts [2] washers [3], and washers [16] through receptacle [1], shield [17], and
receptacle pan.
(g) Install the nuts [15].
1) Tighten the nuts [15].
(h) Install the nuts [14].
1) Tighten the nut [14].
(i) Remove the excessive sealant, A00247.
(j) Apply sealant, A02315 to the edge of the receptacle [1] to make a fillet seal
(TASK 51-31-00-390-804).
SUBTASK 24-41-11-420-005-002
CAUTION
PUT AN IDENTIFIER ON THE WIRES ON EACH SIDE OF THE ELECTRICAL
CONNECTION BEFORE YOU DISCONNECT. IF YOU CONNECT THEM AT AN
INCORRECT LOCATION, DAMAGE TO THE COMPONENTS WILL OCCUR.
CAUTION
DO NOT INSTALL WASHERS BELOW THE ELECTRICAL LEAD TERMINAL
LUGS. THIS WILL CAUSE HEAT AND DAMAGE TO THE TERMINAL STUDS.
(2) Do these steps to connect the electrical leads to the receptacle [1]:
(a) Install the electrical leads onto receptacle studs.
(b) Install the washers [4], lockwashers [5], and nuts [6].
1) Tighten the nuts [6] to 21 ±1 in-lb (2.37 ±0.12 N·m).
(c) Install the washers [7], lockwashers [8], and nuts [9].
1) Tighten the nuts [9] to 122.5 ±2.5 in-lb (13.84 ±0.28 N·m).
(d) Remove the identification tags from the electrical leads.
(e) Install the washers [13].
(f) Put the cover assembly [10] in its position.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-41-11
Config 2
Page 407
D633A101-ILF Oct 15/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF 593-599, 601-603, 606, 607, 610-615, 620,
625-627, 691-699, 833-835, 838
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