曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
(Opt Part #: C27007-21, Supplier: 81205, A/P Effectivity: 737-300, -400,
-500)
(Opt Part #: C27007-26, Supplier: 81205, A/P Effectivity: 737-300, -400,
-500, -600, -700, -700C, -700ER, -700QC, -800, -BBJ)
C. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-00
Page 544
Feb 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
D. Access Panels
Number Name/Location
112A Forward Access Door
E. Procedure
SUBTASK 27-41-00-010-006
(1) Open this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 27-41-00-730-001
(2) Do the test of the captain’s column cutout switch:
(a) Install the control column assembly protractor, SPL-1680 on the captain’s control column.
(b) Disconnect the electrical connector D12156 from the captain’s column cutout switch.
(c) Install the test box, SPL-1685:
1) Connect the test box, SPL-1685 connector to the captain’s column cutout switch.
2) Connect the input jack on the test box, SPL-1685 to 28V DC power.
3) Set the stabilizer to 4 units of trim (B dimension equals to 39.89 in. (1013.2 mm).
(d) Set the POWER and MAIN CLUTCH CUTOUT switches on the test box, SPL-1685 to the ON
position.
1) Move the captain’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 agree with the Table 502 below:
NOTE: Ignore the lights on the AUTOPILOT STABILIZER TRIM side of the test box
(right side).
Table 502/27-41-00-993-808
LIGHT STATUS
POWER ON
MAIN MOTOR OFF
MAIN CLUTCH ON
MAIN MOTOR CUTOUT OFF
MAIN CLUTCH CUTOUT ON
3) Move the captain’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 503 below:
NOTE: Ignore the lights on the AUTOPILOT STABILIZER TRIM side of the test box
(right side).
Table 503/27-41-00-993-809
LIGHT STATUS
POWER ON
MAIN MOTOR OFF
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-00
Page 545
Feb 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
LIGHT STATUS
MAIN CLUTCH OFF
MAIN MOTOR CUTOUT OFF
MAIN CLUTCH CUTOUT ON
5) Move the captain’s control column to the neutral position,
6) Make sure the lights on the test box, SPL-1685 agree with the Table 504 below:
NOTE: Ignore the lights on the AUTOPILOT STABILIZER TRIM side of the test box
(right side).
Table 504/27-41-00-993-810
LIGHT STATUS
POWER ON
MAIN MOTOR OFF
MAIN CLUTCH ON
MAIN MOTOR CUTOUT OFF
MAIN CLUTCH CUTOUT ON
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 505 below:
NOTE: Ignore the lights on the AUTOPILOT STABILIZER TRIM side of the test box
(right side).
Table 505/27-41-00-993-811
LIGHT STATUS
POWER ON
MAIN MOTOR OFF
MAIN CLUTCH OFF
MAIN MOTOR CUTOUT OFF
MAIN CLUTCH CUTOUT ON
(e) Set the POWER and MAIN CLUTCH CUTOUT switches on the test box, SPL-1685 to the OFF
position.
(f) Set the POWER and MAIN MOTOR CUTOUT switches on the test box, SPL-1685 to the ON
position.
1) Move the captain’s control column to the neutral position.
2) Make sure the lights on the test box, SPL-1685 agree with the Table 506 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
Page 546
Feb 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Table 506/27-41-00-993-812
LIGHT STATUS
POWER ON
MAIN MOTOR ON
MAIN CLUTCH OFF
MAIN MOTOR CUTOUT ON
MAIN CLUTCH CUTOUT OFF
3) Move the captain’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 507 below:
NOTE: Ignore the lights on the AUTOPILOT STABILIZER TRIM side of the test box
(right side).
Table 507/27-41-00-993-813
LIGHT STATUS
POWER ON
MAIN MOTOR OFF
MAIN CLUTCH OFF
MAIN MOTOR CUTOUT ON
MAIN CLUTCH CUTOUT OFF
5) Move the captain’s control column to the neutral position,
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(121)
