• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-03 11:44来源:蓝天飞行翻译 作者:航空
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

 5727 Access Door - Left Nacelle 5827 Access Door - Right Nacelle
 5728 Access Door - Left Nacelle 5828 Access Door - Right Nacelle
 5729 Access Door - Left Nacelle 5829 Access Door - Right Nacelle
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 54-10-00
 ALL  ú ú B01 Page 501 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ACCESS PANELS

NACELLE STRUT - RIGHT SIDE
BLOWOUT DOOR

NACELLE STRUT - TOP VIEW

Nacelle Strut Access Panels and Fairings Aerodynamic Smoothness
Figure 501 (Sheet 1)

A10778
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 54-10-00
 ALL  ú ú B01 Page 502 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
AIRFLOW AIRFLOW


Nacelle Strut Access Panels and Fairings Aerodynamic Smoothness
Figure 501 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 54-10-00
 ALL  ú ú B01 Page 503 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A10901
A

737-300/400/500
MAINTENANCE MANUAL


D

 

+0.025/-0.035 INCH (+0.635/-0.889 mm) MAX DISTANCE 0.30 |0.03 INCH
(7.62 |0.76 mm) WING SKIN FWD (0.889 mm) MAX DISTANCE

0.035 INCH
(0.889 mm) MAX DISTANCE

|0.025 INCH
(|0.635 mm)
MAX DISTANCE

FORWARD FAIRING

Nacelle Strut Access Panels and Fairings Aerodynamic Smoothness
Figure 501 (Sheet 3)

A10931
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 54-10-00
 ALL  ú ú B01 Page 504 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

 FWD


A-A  B-B

Nacelle Strut Access Panels and Fairings Aerodynamic Smoothness
Figure 501 (Sheet 4)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 54-10-00
 ALL  ú ú B01 Page 505 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A11388
A
737-300/400/500MAINTENANCE MANUAL
 E.  Procedure
 S 825-002-B00
 (1)  Adjust the clearances around the panel or fairing as follows (Fig. 501):
 (a)  If the clearances are more than the limits, do these steps: 1) Remove the access panel or fairing (Ref 12-30-00/201). 2) Use one or more of the steps that follow to adjust the
 aerodynamic smoothness.
 a) Decrease its thickness.
 b) Remove material from the edge.
 c) Add shims or change the contour.
 d) If the height of the forward panel is more than 0.015

 inch above the structure, remove material from the outer edge.
 NOTE: The slope of the new contour must be a minimum
____ of 10 times the height.
 CAUTION: MAKE SURE THE INSIDE OF THE STRUT IS FREE OF ALL
_______ TOOLS AND UNWANTED OBJECTS. IF ALL TOOLS AND UNWANTED OBJECTS ARE NOT REMOVED, BLOCKAGE OF THE DRAIN TUBES CAN OCCUR.
 3)  Remove all tools and unwanted objects from the inside of the strut.
 4)  If the clearance between the panels or fairings is more than 0.030 inch, apply sealant to the clearance and make it smooth.
 NOTE: This is not applicable to doors and panels that open
____
 and close.

 (b)  If the clearance between the panel or fairing and the structure is less than 0.030 inch, it is not necessary to decrease the height of the panel or fairing. 1) It is not necessary to apply the sealant.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 NACELLES/PYLONS(9)