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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Aileron Clearance and Mismatch Requirements
Figure 403 (Sheet 1 of 3)/27-11-11-990-804
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AIRCRAFT MAINTENANCE MANUAL
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GUN ALL 27-11-11
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Aileron Clearance and Mismatch Requirements
Figure 403 (Sheet 2 of 3)/27-11-11-990-804
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Aileron Clearance and Mismatch Requirements
Figure 403 (Sheet 3 of 3)/27-11-11-990-804
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AILERON - INSPECTION/CHECK
1. General
A. This procedure contains the task to do a check of the aileron hinge.
TASK 27-11-11-200-801
2. Aileron Inspection
(Figure 601)
A. General
(1) This task gives wear limits and repair data for the aileron hinge inspection.
B. References
Reference Title
27-11-11-000-801 Aileron Removal (P/B 401)
27-11-11-400-801 Aileron Installation (P/B 401)
C. Tools/Equipment
Reference Description
STD-1096 Micrometer - Depth, 0-1 Inch, Readable to 1/1000 Inch
STD-1097 Caliper - Vernier, 0-6 Inch, Readable to 1/1000 Inch
D. Location Zones
Zone Area
572 Left Wing - Aileron
672 Right Wing - Aileron
E. Procedure
SUBTASK 27-11-11-020-003
(1) Do this task: Aileron Removal, TASK 27-11-11-000-801.
SUBTASK 27-11-11-020-004
(2) Use these tools to do a check for wear on the parts of the aileron hinge:
(a) micrometer (0-1 Inch, readable to 1/1000 Inch), STD-1096
(b) readable to 1/1000 inch vernier 0 - 6 inch caliper, STD-1097.
SUBTASK 27-11-11-020-005
(3) Examine the parts of the aileron PCU linkage for worn areas:
(a) Remove the parts you want to check.
(b) Measure the parts 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.
(d) If the parts are out of tolerance, replace or repair the parts if it is necessary.
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Table 601/27-11-11-993-801
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 BUSHING I.D. 0.2500 in 0.2505 in 0.2525 in
6.3500 mm 6.3627 mm 6.4135 mm 0.0005 in
#1 BOLT O.D. 0.2585 in 0.2595 in 0.2475 in 0.0127 mm
6.5659 mm 6.5913 mm 6.2865 mm
#2 BUSHING I.D. 0.3750 in
9.5250 mm
0.3756 in
9.5402 mm
0.3773 in
9.5834 mm
0.0005 in
#2 BUSHING O.D. 0.3740 in
9.4996 mm
0.3745 in
9.5123 mm
0.3728 in
9.4691 mm
0.0127 mm
#3 BUSHING I.D. 0.2500 in
6.3500 mm
0.2505 in
6.3627 mm
0.2525 in
6.4135 mm
0.0005 in
#3 BOLT O.D. 0.2485 in
6.3119 mm
0.2495 in
6.3373 mm
0.2475 in
6.2865 mm
0.0127 mm
#4 BEARING I.D. 0.2495 in
6.3373 mm
0.2500 in
6.3500 mm
0.2520 in
6.4008 mm
0.0000 in
#4 BOLT O.D. 0.2485 in
6.3119 mm
0.2495 in
6.3373 mm
0.2475 in
6.2865 mm
0.0000 mm
#5 BUSHING I.D. 0.3750 in 0.3756 in 0.3778 in
9.5250 mm 9.5402 mm 9.5961 mm 0.0005 in
#5 BOLT O.D. 0.3735 in 0.3745 in 0.3723 in 0.0127 mm
9.4869 mm 9.5123 mm 9.4564 mm
#6 BUSHING I.D. 0.5620 in
14.2748 mm
0.5627 in
14.2926 mm
0.5645 in
14.3383 mm
0.0005 in
#6 BUSHING O.D. 0.5610 in
14.2494 mm
0.5615 in
14.2621 mm
0.5595 in
14.2113 mm
0.0127 mm
#7 BUSHING I.D. 0.3750 in
9.5250 mm
0.3755 in
9.5377 mm
0.3777 in
9.5936 mm
0.0005 in
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册1(141)
