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[26] to airplane structure.
(g) Pull the lower crank [22] down and remove it from the torque tube [1].
(h) Remove the plate [42], retainer [41], lower bearing housing [26], and plate [40] from the
torque tube [1].
(i) Pull the torque tube [1] down through the upper crank [35] and center crank [30].
(j) Remove the torque tube [1], upper crank [35], and center crank [30] from the airplane.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-71
Config 1
Page 402
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Rudder Control Torque Tube Installation
Figure 401 (Sheet 1 of 3)/27-21-71-990-804-001
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-71
Config 1
Page 403
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Rudder Control Torque Tube Installation
Figure 401 (Sheet 2 of 3)/27-21-71-990-804-001
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-71
Config 1
Page 404
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Rudder Control Torque Tube Installation
Figure 401 (Sheet 3 of 3)/27-21-71-990-804-001
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-71
Config 1
Page 405
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-21-71-400-803-001
3. Rudder Control Torque Tube Installation
(Figure 401)
A. References
Reference Title
27-21-00-700-817-001 Rudder Travel Test (P/B 501)
27-21-00-700-818-001 Standby Rudder Power Control Unit Deadband Test (P/B 501)
27-21-00-820-809-001 Control Rod for Main Rudder Power Control Unit Adjustment
(P/B 501)
27-21-00-820-810-001 Control Rod for Standby Rudder Power Control Unit Adjustment
(P/B 501)
27-21-00-840-802 Put the Rudder Systems A, B, and Standby Back to the Condition
Before the Pressure Removal (P/B 201)
27-21-87-400-801 Rudder Trim Actuator Installation (P/B 401)
51-31-00-390-804 Fillet Seal Application (P/B 201)
B. 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
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)
C. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental - Chromate
Type
BMS5-95
C00308 Compound - Corrosion Preventive, Petrolatum Hot
Application
MIL-C-11796
D00015 Grease - Aircraft Bearing BMS3-24
G01048 Lockwire - Corrosion Resistant Steel (0.032 In. Dia.) NASM20995~
C32
D. Location Zones
Zone Area
324 Vertical Fin - Rear Spar To Trailing Edge
E. Access Panels
Number Name/Location
324BL Vertical Fin, Trailing Edge Access
324DL Trailing Edge Access
F. Torque Tube Installation
SUBTASK 27-21-71-420-012-001
(1) Install the torque tube [1]:
(a) Put the torque tube [1] through the structural cutouts, the upper bearing housing [4], upper
crank [35], and center crank [30].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-005, 155-157, 201-999 PRE SB 737-27-1253 27-21-71
Config 1
Page 406
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(b) Install the plate [40], lower bearing housing [26], retainer [41], and plate [42] to the torque
tube [1].
(c) Install the bolts [27], washers [28], and nuts [29] to attach the lower bearing housing [26] to
the structure.
(d) Install the washers [3] and bolts [2] to attach the upper bearing housing [4] to the structure.
1) Install the lockwire, G01048.
(e) Install the lower crank [22] on the torque tube [1]:
1) Apply corrosion preventive compound, C00308 to the bolts [23].
2) Put the lower crank [22] on the torque tube [1].
3) Install the bolts [23], washers [24], and nuts [25] to attach the lower crank [22] to the
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(101)
