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时间:2010-08-24 13:01来源:蓝天飞行翻译 作者:admin
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MAXIMUM
SERVICE
CLEARANCE
inches/mm
#1 BUSHING I.D. 0.8080 in 0.8175 in 0.8198 in
20.523 mm 20.764 mm 20.822 mm 0.0313 in
#1 FUSE PIN O.D. 0.7880 in 0.7885 in 0.7862 in 0.7950 mm
20.015 mm 20.028 mm 19.969 mm
#2 BUSHING I.D. 0.8080 in 0.8175 in 0.8198 in
20.523 mm 20.764 mm 20.822 mm 0.0313 in
#2 FUSE PIN O.D. 0.7880 in 0.7885 in 0.7862 in 0.7950 mm
20.015 mm 20.028 mm 19.969 mm
#3 BUSHING I.D. 0.5000 in 0.5050 in 0.5050 in
12.700 mm 12.827 mm 12.827 mm 0.0065 in
#3 BOLT O.D. 0.4985 in 0.4995 in 0.4985 in 0.1651 mm
12.662 mm 12.687 mm 12.662 mm
#4 BEARING I.D. 0.5620 in 0.5670 in 0.5670 in
14.275 mm 14.402 mm 14.402 mm 0.0065 in
#4 BOLT O.D. 0.5605 in 0.5615 in 0.5605 in 0.1651 mm
14.237 mm 14.262 mm 14.237 mm
#5 BUSHING I.D. 0.5620 in 0.5670 in 0.5695 in
14.275 mm 14.402 mm 14.465 mm 0.0080 in
#5 BOLT O.D. 0.5605 in 0.5615 in 0.5590 in 0.2032 mm
14.237 mm 14.262 mm 14.199 mm
#6 BUSHING I.D. 0.5620 in 0.5670 in 0.5695 in
14.275 mm 14.402 mm 14.464 mm 0.0700 in
#6 BOLT O.D. 0.4985 in 0.4995 in 0.4970 in 1.7780 mm
12.662 mm 12.687 mm 12.624 mm
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-51-15-420-012
(4) Do this task: Inboard Flap Outboard Track Installation, TASK 27-51-15-400-801.
------------------------- END OF TASK ---------------------------
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D633A101-GUN
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Inboard Flap Outboard Flap Track Wear Limits
Figure 601 (Sheet 1 of 2)/27-51-15-990-803
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EFFECTIVITY
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D633A101-GUN
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Inboard Flap Outboard Flap Track Wear Limits
Figure 601 (Sheet 2 of 2)/27-51-15-990-803
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EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-51-15-200-802
3. Inboard Flap Inboard Track Inspection
(Figure 602)
A. General
(1) This task gives wear limits for the inboard track on the inboard flap.
(2) this task is applicable to the flap tracks at flap supports No. 4 and 5.
B. References
Reference Title
27-51-15-000-802 Inboard Flap Inboard Track Removal (P/B 401)
27-51-15-400-802 Inboard Flap Inboard Track 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
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
541 Left Wing - Fairing Flap Support No. 4
641 Right Wing - Fairing Flap Support No. 5
E. Procedure
SUBTASK 27-51-15-020-017
(1) Do this task: Inboard Flap Inboard Track Removal, TASK 27-51-15-000-802.
SUBTASK 27-51-15-020-018
(2) Use these tools to do a check for wear on the part of the inboard flap inboard track:
(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 27-51-15-020-019
(3) Examine the parts of the inboard flap inboard track (Table 602):
(a) Remove the parts that you will measure.
(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 not in tolerance, replace or repair the parts.
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Table 602/27-51-15-993-806
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
CLEARANCE
inches/mm
#1 BOLT I.D. 0.4960 in 0.4990 in 0.4990 in
 
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