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208 0.94
258 0.91
308 0.87
358 0.82
408 0.77
458 0.71
3) Make sure the pedal force is no more than 18.0 lbf (80.1 N).
4) Push again on the adapter, SPL-1681 until the captain’s left rudder pedal is 3.60 in.
(91.4 mm) ±0.10 in. (2.5 mm) forward from the neutral position.
5) Multiply the compression gage value on the adapter, SPL-1681 by a multiplication
factor given in (Table 503).
NOTE: The angle from the horizontal value is also shown on the adapter, SPL-1681.
6) Make sure the pedal force is between 60.0 lbf (266.9 N) to 82.0 lbf (364.8 N).
7) Remove the adapter, SPL-1681 from the captain’s left pedal.
(d) Install adapter, SPL-1681 on the captain’s right rudder pedal.
1) Push on the adapter, SPL-1681 until the rudder starts to move.
2) Multiply the compression gage value on the adapter, SPL-1681 by a multiplication
factor given in (Table 503).
NOTE: The angle from the horizontal value is also shown on the adapter, SPL-1681.
3) Make sure the pedal force is no more than 18.0 lbf (80.1 N).
4) Push again on the adapter, SPL-1681 until the captain’s right rudder pedal is 3.60 in.
(91.4 mm) ±0.10 in. (2.5 mm) forward from the neutral position.
5) Multiply the compression gage value on the adapter, SPL-1681 by a multiplication
factor given in (Table 503).
NOTE: The angle from the horizontal value is also shown on the adapter, SPL-1681.
6) Make sure the pedal force is between 60.0 lbf (266.9 N) to 82.0 lbf (364.8 N).
7) Remove the adapter, SPL-1681 from the captain’s right pedal.
(e) Install adapter, SPL-1681 on the first officer’s left rudder pedal.
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 553
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
1) Push on the adapter, SPL-1681 until the rudder starts to move.
2) Multiply the compression gage value on the adapter, SPL-1681 by a multiplication
factor given in (Table 503).
NOTE: The angle from the horizontal value is also shown on the adapter, SPL-1681.
3) Make sure the pedal force is no more than 18.0 lbf (80.1 N).
4) Push again on the adapter, SPL-1681 until the first officer’s left rudder pedal is 3.60 in.
(91.4 mm) ±0.10 in. (2.5 mm) forward from the neutral position.
5) Multiply the compression gage value on the adapter, SPL-1681 by a multiplication
factor given in (Table 503).
NOTE: The angle from the horizontal value is also shown on the adapter, SPL-1681.
6) Make sure the pedal force is between 60.0 lbf (266.9 N) to 82.0 lbf (364.8 N).
7) Remove the adapter, SPL-1681 from the first officer’s left pedal.
(f) Install adapter, SPL-1681 on the first officer’s right rudder pedal.
1) Push on the adapter, SPL-1681 until the rudder starts to move.
2) Multiply the compression gage value on the adapter, SPL-1681 by a multiplication
factor given in (Table 503).
NOTE: The angle from the horizontal value is also shown on the adapter, SPL-1681.
3) Make sure the pedal force is no more than 18.0 lbf (80.1 N).
4) Push again on the adapter, SPL-1681 until the first officer’s right rudder pedal is 3.60 in.
(91.4 mm) ±0.10 in. (2.5 mm) forward from the neutral position.
5) Multiply the compression gage value on the adapter, SPL-1681 by a multiplication
factor given in (Table 503).
NOTE: The angle from the horizontal value is also shown on the adapter, SPL-1681.
6) Make sure the pedal force is between 60.0 lbf (266.9 N) to 82.0 lbf (364.8 N).
7) Remove the adapter, SPL-1681 from the first officer’s right pedal.
SUBTASK 27-21-00-860-111-002
(3) Do this task: Put the Rudder Hydraulic systems A, B, and Standby Back to the Condition
Before the Pressurization, TASK 27-21-00-840-801.
------------------------- END OF TASK ---------------------------
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 554
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Rudder Pedal Force Checking Tool
Figure 504/27-21-00-990-812-002
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 555
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
　
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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(68)