Table 404/76-11-10-993-804-F00 (Continued)
CIRCUIT SETTINGS
Connector
(Switch) Connector Pin Numbers
Circuit Condition
(Switch Settings)
D11292P (S91) 11 and 13 More than 1 megohm
D11292P (S1028) 15 and 5 Less than 1 ohm
D11292P (S1028) 15 and 4 More than 1 megohm
D11292P (S596) 9 and 8 Less than 1 ohm
D11292P (S596) 9 and 7 More than 1 megohm
(e) If you find that the measured circuits are as shown, do the electrical connector installation
steps.
SUBTASK 76-11-10-420-001-F00
(6) Connect the electrical harness for the start brake assembly (engine 1) [71] as follows.
(a) Install the electrical connector [23] (D11286P).
(b) Install the electrical connector [22] (D11288P).
(c) Attach the three clamps [21].
SUBTASK 76-11-10-020-007-F00
(7) Connect the electrical harness for the start brake assembly (engine 2) [72] as follows:
(a) Install the electrical connector [42] (D11292P).
(b) Install the electrical connector [43] (D11290P).
(c) Attach the three clamps [41].
SUBTASK 76-11-10-010-003-F00
(8) Install the access covers on to the control stand as follows:
(a) Install the left upper side panel [1].
1) Attach with four screws [2].
(b) Install the left lower side panel [5].
1) Attach with five screws [2].
(c) Install the right upper side panel [3].
1) Attach with four screws [2]].
(d) Install the right lower side panel [4].
1) Attach with four screws [2].
G. Put the Airplane Back to Its Usual Condition
SUBTASK 76-11-10-860-011-F00
(1) Remove the safety tags and close these circuit breakers:
CAPT Electrical System Panel, P18-1
Row Col Number Name
E 1 C00721 AUTOTHROTTLE DC 1
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-10
Page 415
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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