• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2010-08-25 15:35来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-25
Page 604
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Outboard Flap Outboard Track Wear Limits
Figure 601 (Sheet 2 of 2)/27-51-25-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-25
Page 605
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-51-25-200-802
3. Outboard Flap Inboard Track Inspection
(Figure 602)
A. General
(1) This task gives wear limits for the inboard track on the outboard flap.
(2) this task is applicable to the flap tracks at flap supports No. 2 and 3.
B. References
Reference Title
27-51-25-000-802 Outboard Flap Inboard Track Removal (P/B 401)
27-51-25-400-802 Outboard 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
543 Left Wing - Fairing Flap Support No. 2
643 Right Wing - Fairing Flap Support No. 7
E. Procedure
SUBTASK 27-51-25-020-020
(1) Do this task: Outboard Flap Inboard Track Removal, TASK 27-51-25-000-802.
SUBTASK 27-51-25-020-021
(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 27-51-25-020-022
(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.
Table 602/27-51-25-993-806
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 BUSHING I.D. 0.8080 in 0.8175 in 0.8198 in
20.523 mm 20.765 mm 20.823 mm 0.0313 in
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-25
Page 606
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
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 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. 0.7980 in 0.8075 in 0.8075 in
20.269 mm 20.511 mm 20.511 mm 0.0195 in
#2 FUSE PIN O.D. 0.7880 in 0.7885 in 0.7880 in 0.4953 mm
20.015 mm 20.028 mm 20.015 mm
#3 BUSHING I.D. 0.5620 in 0.5670 in 0.5670 in
14.275 mm 14.402 mm 14.402 mm 0.0065 in
#3 BOLT O.D. 0.5605 in 0.5615 in 0.5605 in 0.1651 mm
14.237 mm 14.262 mm 14.267 mm
#4 BUSHING I.D. 0.5000 in 0.5050 in 0.5050 in
12.700 mm 12.827 mm 12.827 mm 0.0065 in
#4 BOLT O.D. 0.4985 in 0.4995 in 0.4985 in 0.1651 mm
12.662 mm 12.687 mm 12.662 mm
#5 BUSHING I.D. 0.5620 in 0.5670 in 0.5695 in
14.275 mm 14.402 mm 14.465 mm 0.0700 in
#5 BOLT O.D. 0.4985 in 0.4995 in 0.4970 in 1.7780 mm
12.662 mm 12.687 mm 12.624 mm
#6 BUSHING I.D. 0.5620 in 0.5670 in 0.5695 in
14.275 mm 14.402 mm 14.465 mm 0.0080 in
#6 BOLT O.D. 0.5605 in 0.5615 in 0.5590 in 0.2032 mm
14.237 mm 14.262 mm 14.199 mm
SUBTASK 27-51-25-420-014
(4) Do this task: Outboard Flap Inboard Track Installation, TASK 27-51-25-400-802.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-25
Page 607
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Outboard Flap Inboard Track Wear Limits
Figure 602 (Sheet 1 of 2)/27-51-25-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-25
Page 608
Feb 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(24)