EasyManua.ls Logo

Boeing 737-600 - Subtask 76-11-01-020-015-F00; Subtask 76-11-01-420-007-F00; Subtask 76-11-01-420-006-F00; Subtask 76-11-01-410-002-F00

Boeing 737-600
2300 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
(f) Install the nut [65] and the washer [63].
SUBTASK 76-11-01-020-015-F00
(11) Install the control shaft components as follows (Figure 402):
(a) Install the clamp up bushing [36] and the long bushing [37] on the stabilizer trim
shaft [31].
NOTE: Put the clamp up bushing on the end with the longest splines.
(b) Put the bearing [41] into the inside end of the short shaft.
(c) Move the stabilizer trim shaft [31] into the control stand from the left side.
NOTE: Put the end of the shaft with the longest splines in first.
(d) Move the sprocket [40] and the chain [39] up from the bottom of the control stand.
(e) Put the sprocket [40] on the splined end of the stabilizer trim shaft [31].
1) Move the control shaft thru the chain sprocket.
(f) Put the bushing [35] on the splined end of the stabilizer trim shaft [31].
1) Move the shaft through the bushing [35].
(g) Move the shaft through the bearing [41] until the end is moved out through the short
shaft [42].
(h) Install the bearing [38] on the left side of the stabilizer trim shaft [31].
(i) Install the clamp up bushing [33] on the right side of the stabilizer trim shaft [31].
(j) Install the bearing [34] on the right side of the stabilizer trim shaft [31].
(k) Lightly tap the stabilizer trim shaft [31] from the left side.
NOTE: Do this task to make sure that the assembled parts are tight and in the correct
position.
SUBTASK 76-11-01-420-007-F00
(12) Connect the stabilizer trim indicator as follows:
(a) Put the link assembly [13] to the arm.
(b) Install the nut [16], the washer [15], and the bolt [17].
SUBTASK 76-11-01-420-006-F00
(13) Activate and adjust the stabilizer trim assembly as follows:
(a) Remove the temporary wire tie from the chain [39] and the sprocket [40].
(b) Adjust the stabilizer control chain (TASK 27-41-00-820-801).
SUBTASK 76-11-01-410-002-F00
(14) Connect the flap lever synchro assembly as follows (Figure 401):
(a) Put the link assembly [12] in the clevis for the flap lever position synchro assembly.
(b) Install the nut [18] and the bolt [19].
(c) Test the flap control lever position sensor system (Flap Control Lever Position Sensor
System Test, TASK 27-51-06-730-802).
SUBTASK 76-11-01-040-007-F00
(15) Activate the speed brake lever as follows:
(a) Go into the access area under the forward flight compartment floor.
(b) Remove the rig pin from the rigging pin kit, SPL-1585 from the forward drum of the speed
break assembly (Speed Brake Control Lever Adjustment, TASK 27-62-00-820-801).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
CFM56 ENGINES (CFM56-7)
76-11-01
Page 430
D633A101-ILF Jun 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

Table of Contents

Related product manuals