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that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
D. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
211 Flight Compartment - Left
212 Flight Compartment - Right
E. Access Panels
Number Name/Location
112A Forward Access Door
113AW Forward Nose Wheel Well Panel
113BW Forward Nose Wheel Well Panel
114AW Forward Nose Wheel Well Panel
114BW Forward Nose Wheel Well Panel
324CL Vertical Fin, Access
F. Prepare for the Test
SUBTASK 27-21-00-860-072-001
(1) Do this task: Remove Pressure from the Rudder Hydraulic Systems A, B, and Standby,
TASK 27-21-00-800-802.
SUBTASK 27-21-00-010-020-001
(2) Open these access doors:
Number Name/Location
112A Forward Access Door
324CL Vertical Fin, Access
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 509
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-21-00-010-021-001
(3) Open 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
G. Procedure
SUBTASK 27-21-00-710-071-001
(1) Do the rudder pedals adjustment:
(a) Install the rig pin R-5 from the rig pin kit, SPL-1585 in the rudder feel and centering unit.
(Figure 502)
(b) Install the rig pin R-3 from the rig pin kit, SPL-1585 in the captain’s rudder forward quadrant.
(Figure 501)
(c) Install the rig pin R-4 from the rig pin kit, SPL-1585 in the first officer’s rudder forward
quadrant.
(d) Do these steps to set the jackshaft yoke to the middle position:
NOTE: The middle position of the jackshaft yoke is where the number of turns of the shaft
from the full forward and full aft adjustment are the same.
1) Turn the rudder pedal adjustment crank to move the rudder pedals full forward.
2) Turn the rudder pedal adjustment crank to move the rudder pedals full aft. Record the
number of turns.
3) Turn the rudder pedal adjustment crank half the recorded number of turns forward.
(e) Make sure that you can install these rig pins from the rig pin kit, SPL-1585:
1) Rig pin R-1 on the captain’s rudder pedals.
2) Rig pin R-2 on the first officer’s rudder pedals.
(f) If you can not install the rig pins R-1 and R-2 freely, then do these steps:
1) Determine which pedal arm is out-of-line with the rigging pin hole.
a) If you have problem with installing rig pin R-1, then adjust the captain’s side.
b) If you have problem with installing rig pin R-2, then adjust the first officer’s side.
c) If you have problem with installing both rig pins R-1 and R-2, then adjust both sides.
2) Loosen both jamnuts [8] on the rudder pedal tension rods [7].
3) Remove the bolts [9], washers [10], and nuts [11] to disconnect the rudder pedal
tension rods [7] at the forward end.
4) Adjust the length of rudder pedal tension rods [7] until you can install rig pin R-1 or R-2
easily.
a) Turn the rod end or rod body of the rudder pedal tension rod [7] as necessary to
adjust the length.
b) Keep the lube fitting on the rudder pedal tension rod [7] down.
5) Install the bolts [9], washers [10], and nuts [11] to connect the rudder pedal tension rods
[7].
6) Tighten the jamnuts [8].
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 510
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
7) Make sure you can see the threads through the holes on the rudder pedal tension rods
[7].
(g) Remove the rig pins R-1, R-2, R-3, R-4, and R-5.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-21-00-410-011-001
(1) 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 27-21-00-940-002-001
(2) Close these doors:
Number Name/Location
112A Forward Access Door
324CL Vertical Fin, Access
SUBTASK 27-21-00-860-073-001
(3) Do this task: Put the Rudder Systems A, B, and Standby Back to the Condition Before the
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(23)
