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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-71
Page 407
Jun 10/2004
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Input Torque Tube Installation
Figure 402 (Sheet 3 of 8)/27-31-71-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-012, 155-157, 201-999 PRE SB 737-27A1271 27-31-71
Page 408
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Input Torque Tube Installation
Figure 402 (Sheet 4 of 8)/27-31-71-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 013-099, 101-122; GUN 001-012, 155-157, 201-999
POST SB 737-27A1271
27-31-71
Page 409
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Input Torque Tube Installation
Figure 402 (Sheet 5 of 8)/27-31-71-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-012, 155-157, 201-999 PRE SB 737-27A1271 27-31-71
Page 410
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Input Torque Tube Installation
Figure 402 (Sheet 6 of 8)/27-31-71-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 013-099, 101-122; GUN 001-012, 155-157, 201-999
POST SB 737-27A1271
27-31-71
Page 411
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Input Torque Tube Installation
Figure 402 (Sheet 7 of 8)/27-31-71-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-012, 155-157, 201-999 PRE SB 737-27A1271 27-31-71
Page 412
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Input Torque Tube Installation
Figure 402 (Sheet 8 of 8)/27-31-71-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 013-099, 101-122; GUN 001-012, 155-157, 201-999
POST SB 737-27A1271
27-31-71
Page 413
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-31-71-400-801
3. Elevator Input Torque Tube - Installation
(Figure 401, Figure 402)
A. References
Reference Title
27-31-00-700-809 Control Column Power Force - Test (P/B 501)
27-31-00-700-812 Feel Force System - Test (P/B 501)
27-31-00-820-801 Elevator Control Cables EA and EB and Pitch Force Transducers -
Adjustment (P/B 501)
27-31-00-820-802 Elevator Control Pushrods - Adjustment (P/B 501)
27-31-00-820-803 Input Rods of the Elevator Power Control Unit - Adjustment (P/B 501)
27-31-00-820-804 Input Rods of the Elevator Neutral Shift Mechanism and Output Rod
of the Feel and Centering Unit - Adjustment (P/B 501)
27-31-00-840-802 Put the Elevator Systems A and B Back to the Condition Before the
Pressure Removal (P/B 201)
53-53-00-400-801 Tailcone Installation (P/B 401)
B. Location Zones
Zone Area
315 APU Compartment - Left
316 APU Compartment - Right
C. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
D. Torque Tube Installation
SUBTASK 27-31-71-420-001
(1) Install the torque tube [18]:
(a) Hold the torque tube [18] in its position.
(b) Attach the torque tube [18] to the support structure:
1) Install the bushings [53], bolt assemblies [35], washers [34], washers [51], washers
[52], and nuts [50].
a) Tighten the nuts [50] to 90-105 pound-inches (10.2-11.9 newton-meters).
CAUTION: DO NOT TIGHTEN THE NUT [48] AGAIN AFTER YOU TIGHTEN THE NUT
[50]. YOU CAN CAUSE DAMAGE TO EQUIPMENT.
2) Install the washers [49] and nuts [50].
a) Tighten the nuts [50] to 30-35 pound-inches (3.4-3.9 newton-meters).
CAUTION: EXAMINE THE INNER AND THE OUTER RODS/BOLTS FOR DAMAGE BEFORE
YOU INSTALL THE ROD END BOLTS. DAMAGE TO EQUIPMENT CAN OCCUR.
(c) Connect the torque tube [18] to the two reaction links [37]:
1) Install the bushings [45], bolts [44], washers [46], and nuts [47].
NOTE: Install the left bolt (on the left assembly) with the bolt head inboard and the
right bolt (on the right assembly) with the bolt head outboard.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-71
Page 414
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN 013-099, 101-122; GUN 001-012, 155-157, 201-999 POST SB 737-27A1271
　
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