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(c) Connect the electrical connectors. SUBTASK 27-41-51-420-004 (4) Connect the rod assemblies [8] to the column cutout switch arms [3]: (a) Install the rig pin E-1 from the rig pin kit, SPL-1585 through the left forward control quadrant. (b) Install the rig pin ST-4 from the rig pin kit, SPL-1585 in the column cutout switch. (c) Remove the lockwires from the rod assembly [8]. (d) Turn the jamnuts [7] until you can easily install the bolt that connect the rod assembly [8] to the column cutout switch arm [3]. (e) Install the bolt [4], washer [5], and nut [6] to connect the rod assembly [8] to the column cutout switch arm [3]. (f) Tighten the jamnuts [7]. (g) Install the lockwire, G01048. (h) Remove the rig pin E-1 from the left forward control quadrant. (i) Remove the rig pin ST-4 from the control column switch. SUBTASK 27-41-51-860-002 (5) Remove the safety tags and close these circuit breakers: F/O Electrical System Panel, P6-2 Row Col Number Name B 10 C00207 FLIGHT CONTROL STAB TRIM CONT D 10 C00840 FLIGHT CONTROL STAB TRIM ACTUATOR SUBTASK 27-41-51-710-001 (6) Do this task: Column Cutout Switches Test, TASK 27-41-00-700-810. G. Put the Airplane Back to Its Usual Condition SUBTASK 27-41-51-410-001 (1) Close this access panel: Number Name/Location 112A Forward Access Door ------------------------- END OF TASK --------------------------- 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL EFFECTIVITY GUN ALL 27-41-51 Page 407 Oct 10/2006 D633A101-GUN BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details HORIZONTAL STABILIZER TRIM CONTROL WHEEL - REMOVAL/INSTALLATION 1. General A. This procedure has these tasks: (1) Stabilizer Trim Control Wheel Removal. (2) Stabilizer Trim Control Wheel Installation. TASK 27-41-61-010-801 2. Stabilizer Trim Control Wheel Removal (Figure 401) A. Location Zones Zone Area 212 Flight Compartment - Right B. Stabilizer Trim Control Wheel Removal SUBTASK 27-41-61-010-001 (1) Remove the stabilizer trim wheel [1] from the control stand [7]: (a) Remove the bolt [2] that attaches the stabilizer trim wheel [1] to the shaft. (b) Remove the stabilizer trim wheel [1] from the shaft. SUBTASK 27-41-61-010-002 (2) As necessary, remove the upper side cover [3] and lower side cover [5] from the right side of the control stand [7]: (a) Remove the screws [6] and the pocket assembly [8] from the lower side cover [5]. (b) Remove the screws [4] that attach the upper side cover [3] and the lower side cover [5] to the control stand [7]. (c) Remove the upper side cover [3] and the lower side cover [5] from the control stand [7]. ------------------------- END OF TASK --------------------------- 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL EFFECTIVITY GUN ALL 27-41-61 Page 401 Oct 10/2003 D633A101-GUN BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details Stabilizer Trim Control Wheel Installation Figure 401/27-41-61-990-801 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL EFFECTIVITY GUN ALL 27-41-61 Page 402 Oct 10/2003 D633A101-GUN BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details TASK 27-41-61-410-801 3. Stabilizer Trim Control Wheel Installation (Figure 401) A. Location Zones Zone Area 212 Flight Compartment - Right B. Stabilizer Trim Control Wheel Installation SUBTASK 27-41-61-410-002 (1) As necessary, install the upper side cover [3] and lower side cover [5] on the control stand [7]: (a) Install the upper side cover [3] and the lower side cover [5] on the control stand [7]. (b) Install the screws [4] that attach the upper side cover [3] and the lower side cover [5] to the control stand [7]. (c) Install the screws [6] in the pocket assembly [8] and the lower side cover [5]. SUBTASK 27-41-61-410-003 (2) Install the stabilizer trim wheel [1] on the control stand [7]: (a) Install the stabilizer trim wheel [1] on the shaft with the handle 90 +/- 15 degrees apart from the handle on the other stabilizer trim wheel. (b) Install the bolt [2] that attaches the stabilizer trim wheel [1] to the shaft. ------------------------- END OF TASK --------------------------- 737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL EFFECTIVITY GUN ALL 27-41-61 Page 403 Oct 10/2003 D633A101-GUN BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details STABILIZER TRIM MOTOR - REMOVAL/INSTALLATION 1. General A. This procedure has these tasks: www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册4
