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6) Make sure the lights on the test box, SPL-1685 agree with the Table 508 below:
NOTE: Ignore the lights on the AUTOPILOT STABILIZER TRIM side of the test box
(right side).
Table 508/27-41-00-993-814
LIGHT STATUS
POWER ON
MAIN MOTOR ON
MAIN CLUTCH OFF
MAIN MOTOR CUTOUT ON
MAIN CLUTCH CUTOUT OFF
7) Move the captain’s control column more than 4 degrees forward of the neutral position.
8) Make sure the lights on the test box, SPL-1685 agree with the Table 509 below:
NOTE: Ignore the lights on the AUTOPILOT STABILIZER TRIM side of the test box
(right side).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-00
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Table 509/27-41-00-993-815
LIGHT STATUS
POWER ON
MAIN MOTOR OFF
MAIN CLUTCH OFF
MAIN MOTOR CUTOUT ON
MAIN CLUTCH CUTOUT OFF
9) Set the control column to the neutral position.
(g) Set the POWER and MAIN MOTOR CUTOUT switches on the test box, SPL-1685 to the OFF
position.
(h) Disconnect the test box connectors from the captain’s cutout switch connectors.
(i) Connect the electrical connector D12156 to the captain’s cutout switch.
(j) Remove the test box, SPL-1685 from the captain’s control column.
(k) Remove the control column assembly protractor, SPL-1680 from the captain’s control
column.
SUBTASK 27-41-00-730-002
(3) Do the test of the first officer’s column cutout switch:
(a) Install the control column assembly protractor, SPL-1680 on the first officer’s control
column.
(b) Install the test box, SPL-1685 on the first officer’s control column.
(c) Disconnect the electrical connectors D3124 and D2257 from the first officer’s column cutout
switch.
(d) Install the test box, SPL-1685:
1) Connect the test box, SPL-1685 to the first officer’s column cutout switch.
2) Connect the input jack on the test box, SPL-1685 to 28V DC power.
(e) Set the POWER, MAIN CLUTCH CUTOUT, AUTOPILOT MOTOR CUTOUT switches on the
test box, SPL-1685 to the ON position.
1) Move the first officer’s control column to the neutral position, which is 6.9 ±0.8 degrees
forward of the vertical position.
2) Make sure the lights on the test box, SPL-1685 agree with the Table 510 below:
Table 510/27-41-00-993-816
LIGHT STATUS
POWER ON
MAIN MOTOR OFF
MAIN CLUTCH ON
MAIN MOTOR CUTOUT OFF
MAIN CLUTCH CUTOUT ON
AUTOPILOT MOTOR ON
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-00
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D633A101-GUN
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(Continued)
LIGHT STATUS
AUTOPILOT CLUTCH OFF
AUTOPILOT MOTOR CUTOUT ON
AUTOPILOT CLUTCH CUTOUT OFF
3) Move the first officer’s control column more than 6 degrees aft of the neutral position.
4) Make sure the lights on the test box, SPL-1685 agree with the Table 511 below:
Table 511/27-41-00-993-817
LIGHT STATUS
POWER ON
MAIN MOTOR OFF
MAIN CLUTCH OFF
MAIN MOTOR CUTOUT OFF
MAIN CLUTCH CUTOUT ON
AUTOPILOT MOTOR OFF
AUTOPILOT CLUTCH OFF
AUTOPILOT MOTOR CUTOUT ON
AUTOPILOT CLUTCH CUTOUT OFF
5) Move the first officer’s control column to the neutral position.
6) Make sure the lights on the test box, SPL-1685 agree with the Table 512 below:
Table 512/27-41-00-993-818
LIGHT STATUS
POWER ON
MAIN MOTOR OFF
MAIN CLUTCH ON
MAIN MOTOR CUTOUT OFF
MAIN CLUTCH CUTOUT ON
AUTOPILOT MOTOR ON
AUTOPILOT CLUTCH OFF
AUTOPILOT MOTOR CUTOUT ON
AUTOPILOT CLUTCH CUTOUT OFF
7) Move the first officer’s control column more than 4 degrees forward of the neutral
position.
8) Make sure the lights on the test box, SPL-1685 agree with the Table 513 below:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-00
Page 549
Feb 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Table 513/27-41-00-993-819
LIGHT STATUS
POWER ON
MAIN MOTOR OFF
MAIN CLUTCH OFF
MAIN MOTOR CUTOUT OFF
MAIN CLUTCH CUTOUT ON
AUTOPILOT MOTOR OFF
AUTOPILOT CLUTCH OFF
AUTOPILOT MOTOR CUTOUT ON
AUTOPILOT CLUTCH CUTOUT OFF
(f) Set the POWER, MAIN CLUTCH CUTOUT, and AUTOPILOT MOTOR CUTOUT switches on
the test box, SPL-1685 to the OFF position.
(g) Set the POWER, MAIN MOTOR CUTOUT, and AUTOPILOT CLUTCH CUTOUT switches on
　
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