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Temp Deg F (C) Nominal Lbs (Kg) Minimum Lbs (Kg) Maximum Lbs (Kg)
-35 (-37.2) 120 (54.4) 110 (49.9) 130 (59.0)
-36 (-37.8) 119 (54.0) 109 (49.4) 129 (58.5)
-37 (-38.3) 119 (54.0) 109 (49.4) 129 (58.5)
-38 (-38.9) 118 (53.5) 108 (49.0) 128 (58.0)
-39 (-39.4) 118 (53.5) 108 (49.0) 128 (58.0)
-40 (-40.0) 117 (53.1) 107 (48.5) 127 (57.6)
GUN 006-099, 101-122; GUN 001-005, 155-157, 201-999 POST SB 737-27-1253
(d) Make sure you can install these rig pins from the rig pin kit, SPL-1585 (Figure 501):
1) Rig pin R-3 in the captain’s rudder forward quadrant.
2) Rig pin R-4 in the first officer’s rudder forward quadrant.
(e) If you can not install the rig pins R-3 and R-4 freely, then do these steps:
1) Turn the turnbuckles to release the tension of the control cables RA and RB.
2) Remove the pin [5], nut [4], washer [3], spacer [2] and bolt [1] to disconnect one end of
the bus rod [6] from rudder forward quadrant. Discard the pin [5].
3) Install the rig pins R-3 in the captain’s rudder forward quadrant.
4) Install the rig pin R-4 in the first officer’s rudder forward quadrant.
5) Adjust the bus rod [6] until you can install the bolt [1] easily.
6) Install the bolt [1], spacer [2], washer [3], nut [4], and new pin [5] to connect the bus rod
[6] to the rudder forward quadrant.
GUN 101-122
7) Adjust the turnbuckles on the control cables RA and RB to get the correct tension as
given in (Table 501).
GUN 006-099; GUN 001-005, 155-157, 201-999 POST SB 737-27-1253
8) Adjust the turnbuckles on the control cables RA and RB to get the correct tension as
given in (Table 502).
GUN 006-099, 101-122; GUN 001-005, 155-157, 201-999 POST SB 737-27-1253
(f) Do these steps to adjust the captain’s and first officer’s pedals to the neutral adjustment
position:
NOTE: The middle position of the rudder pedals 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 number of turns forward.
(g) Install these rig pins from the rig pin kit, SPL-1585:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 006-099, 101-122; GUN 001-005, 155-157, 201-999
POST SB 737-27-1253
27-21-00
Config 2
Page 524
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
1) Rig pin R-1 on the captain’s rudder pedals.
2) Rig pin R-2 on the first officer’s rudder pedals.
(h) If you can not install the rig pin R-1 or R-2 freely, then do these steps:
1) Loosen the jamnuts [8] from the applicable rudder pedal tension rod [7].
NOTE: If you can not install rig pin R-1 then adjust the captain’s rudder pedal tension
rods. If you can not install the rig pin R-2 then adjust the first officer’s rudder
pedal tension rods. You are only required to adjust the applicable rudder
pedal tension rod that is out of rig.
2) Remove the nut [11], washer [10], bolt [9] from the forward end of the rudder pedal
tension rod [7].
3) Adjust the rudder pedal tension rod [7] until you can install the applicable rig pin freely.
a) Make sure that you keep the lube fitting on the rudder pedal tension rod [7] is in the
down direction.
4) Install the bolt [9], washer [10], nut [11].
5) Tighten the jamnuts [8].
(i) Do a check on the rudder forward quadrant bus rod [6] and the four rudder pedal tension
rods [7]:
1) Make sure the rod ends cover at least 50 percent of the inspection holes at two end of
the rods (10 locations).
(j) Remove the rig pin R-1, R-2, R-3, R-4, and R-5.
(k) Operate the rudder pedals through one full travel cycle.
GUN 101-122
1) Make sure the control cables RA and RB are at the correct tension as given in
(Table 501).
GUN 006-099; GUN 001-005, 155-157, 201-999 POST SB 737-27-1253
2) Make sure the control cables RA and RB are at the correct tension as given in
(Table 502).
GUN 006-099, 101-122; GUN 001-005, 155-157, 201-999 POST SB 737-27-1253
(l) Install the locking clips on the turnbuckles.
H. Put the Airplane Back To Its Usual Condition
SUBTASK 27-21-00-010-024-002
(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
324AL Vertical Fin, Aft Fin Access Door
737-600/700/800/900
　
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本文鏈接地址：737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊2(57)