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stop. Add or subtract shims as needed to bring the clearance to zero.
(k) Remove the rig pin R-3.
(l) Move the first officer’s rudder forward quadrant until you can install the rig pin R-4 in the aft
rig pin hole.
(m) Make sure there is no clearance between the first officer’s forward quadrant and quadrant
stop. Add or subtract shims as needed to bring the clearance to zero.
(n) Remove the rig pin R-4.
(o) Connect the control rod [36] to the center crank [41].
1) Install the bolt assembly [42] with the bolt head end up and washer [43].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
Page 503
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
2) Tighten the outer bolt of the bolt assembly [42] to 70 in-lb (7.9 N
m) -- 85 in-lb (9.6 N
m).
3) Install the washers [44] and nut [45].
CAUTION: DO NOT TIGHTEN THE OUTER BOLT OF THE BOLT ASSEMBLY [42]
AFTER YOU TIGHTEN THE NUT [45]. THIS CAN CAUSE DAMAGE TO
EQUIPMENT.
4) Tighten the nut [45] to 25 in-lb (2.8 N
m) -- 30 in-lb (3.4 N
m).
(p) Install the bolt assembly [47] with the bolt head end up, washer [48] (under bolt), washer
[49] (under nut), and nut [50] to connect the control rod [34] to the upper crank [46].
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-21-00-820-006-001
(1) Do this task: Rudder Pedals Adjustment, TASK 27-21-00-820-807-001.
SUBTASK 27-21-00-820-007-001
(2) Do this task: Control Rod for Main Rudder Power Control Unit Adjustment,
TASK 27-21-00-820-809-001.
SUBTASK 27-21-00-410-010-001
(3) Close these access panels:
Number Name/Location
113AW Forward Nose Wheel Well Panel
113BW Forward Nose Wheel Well Panel
114AW Forward Nose Wheel Well Panel
114BW Forward Nose Wheel Well Panel
SUBTASK 27-21-00-010-019-001
(4) Close these access doors:
Number Name/Location
112A Forward Access Door
317AL Tail Cone Access Door
SUBTASK 27-21-00-860-071-001
(5) Do this task: Put the Rudder Systems A, B, and Standby Back to the Condition Before the
Pressure Removal, TASK 27-21-00-840-802.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
Page 504
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Rudder Control System Forward Components
Figure 501 (Sheet 1 of 4)/27-21-00-990-810-001
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
Page 505
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Rudder Control System Forward Components
Figure 501 (Sheet 2 of 4)/27-21-00-990-810-001
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
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Rudder Control System Forward Components
Figure 501 (Sheet 3 of 4)/27-21-00-990-810-001
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
Page 507
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Rudder Control System Forward Components
Figure 501 (Sheet 4 of 4)/27-21-00-990-810-001
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-00
Config 1
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TASK 27-21-00-820-807-001
3. Rudder Pedals Adjustment
(Figure 501)
A. General
(1) Use this task to adjust the rudder pedals to the center position.
B. References
Reference Title
27-21-00-800-802 Remove Pressure from the Rudder Hydraulic Systems A, B, and
Standby (P/B 201)
27-21-00-840-802 Put the Rudder Systems A, B, and Standby Back to the Condition
Before the Pressure Removal (P/B 201)
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
　
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