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SUBTASK 27-61-41-020-012
(3) Examine the parts of the spoiler control quadrant for worn areas:
(a) Remove the parts to be checked.
(b) Measure the parts as necessary with a micrometer (0-1 Inch, readable to 1/1000 Inch),
STD-1096 or a readable to 1/1000 inch vernier 0 - 6 inch caliper, STD-1097.
(c) Compare the dimensions you measured with the permitted wear dimensions that follow.
(d) If the parts are not in the tolerance, replace the part as required.
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Table 601/27-61-41-993-801
NAME OF THE PARTS
THAT ARE IN CONTACT
DIM.
DIAMETER DESIGN LIMITS WEAR LIMITS
MINIMUM
inches/mm
MAXIMUM
inches/mm
PERMITTED
MAXIMUM I.D./
MINIMUM O.D. OF
WORN PART
MAXIMUM
SERVICE
DIAMETRIC
CLEARANCE
#1 BEARING*[1] I.D. 0.2497 in 0.2500 in 0.2500 in
0.0019 in
0.05 mm
6.34 mm 6.35 mm 6.35 mm
#1 BOLT O.D. 0.2485 in 0.2495 in 0.2481 in
6.31 mm 6.34 mm 6.30 mm
*[1] Maximum permitted radial play of the bearing is 0.0020 inch.
SUBTASK 27-61-41-020-013
(4) Connect the aileron spring cartridge to the aileron input crank.
------------------------- END OF TASK ---------------------------
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Spoiler Control Quadrant Wear Limits
Figure 601 (Sheet 1 of 2)/27-61-41-990-802
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Spoiler Control Quadrant Wear Limits
Figure 601 (Sheet 2 of 2)/27-61-41-990-802
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SPOILER CONTROL QUADRANT - REPAIRS
1. General
A. There is one task in this procedure, a repair of the spoiler control quadrant. The repair includes the
replacement of the rivets that attach the aileron input crank to the spoiler control quadrant shaft.
B. This task does not remove or install the spoiler control quadrant, refer to the Spoiler Control
Quadrant - Removal/Installation for procedures to remove and install the spoiler control quadrant.
TASK 27-61-41-200-801
2. Spoiler Control Quadrant Repairs
A. References
Reference Title
27-61-41-000-801 Spoiler Control Quadrant Removal (P/B 401)
27-61-41-400-801 Spoiler Control Quadrant Installation (P/B 401)
B. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
C. Procedure
SUBTASK 27-61-41-020-008
(1) Remove the spoiler control quadrant shaft. To remove it, do this task: Spoiler Control Quadrant
Removal, TASK 27-61-41-000-801.
SUBTASK 27-61-41-350-001
(2) Repair the quadrant shaft:
(a) Remove the broken parts of the rivets from the holes in the aileron input crank and the
quadrant shaft.
(b) Install the new rivets.
(c) Examine the aluminum foil marker on the quadrant shaft.
1) Replace the marker if it is damaged or not there.
SUBTASK 27-61-41-020-009
(3) Examine the parts of the spoiler control quadrant for worn areas. Repair or replace worn parts,
as necessary.
SUBTASK 27-61-41-020-014
(4) Install the spoiler control quadrant shaft. To install it, do this task: Spoiler Control Quadrant
Installation, TASK 27-61-41-400-801.
------------------------- END OF TASK ---------------------------
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FLIGHT SPOILER ACTUATOR - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the flight spoiler actuator.
(2) An installation of the flight spoiler actuator.
B. In this procedure the flight spoiler actuator is referred to as the "actuator".
TASK 27-61-51-000-801
2. Flight Spoiler Actuator Removal
(Figure 401)
A. References
Reference Title
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737-600-700-800-900 飞机维护手册6 AIRCRAFT MAINTENANCE MANUA(48)
