• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-30 10:34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

510  Outboard Flap Track Fairing Wear Limits 
Aug 01/96  Figure 601 (Sheet 2)  27-51-121 
Page 603 
B
O
E
I
NG
P
R
OP
R
I
E
T
A
R
Y
 - Copyri
ght
 . - Unpubl
i
s
hed
W
o
r
k
 -
S
ee
t
i
t
l
e page f
o
r de
t
a
i
l
s
.
 


INBOARD FLAP TRACK FAIRING - REMOVAL/INSTALLATION
1.  Remove Inboard Flap Track Fairing
A.  Remove access panels L3501/3601R. 
B.  Remove cotter pin and nut (Fig. 401).
C.  Move fairing forward to disengage support pins. Lower fairing from airplane.
2.  Install Inboard Flap Track Fairing
A.  Position fairing to align support pins with holes in attach plates (Fig. 401).
B.  Move fairing aft to engage pins with attach plates.
C.  Secure fairing with washer and nut. Install cotter pin.
D.  Check that gaps at inboard edge and at aft end of fairing are 0.10 +0.05 inch and that mismatch does not exceed 0.03 inch. If gaps and mismatch are not within limits, adjust fairing (Ref Inboard Flap Track Fairing - A/T).
E.  If new fairing is being fitted:
(1)  
Jack airplane until all tires are clear of ground (Ref Jacking, Chapter 7).

(2)  
Check that electrical power is available.

(3)  
Pressurize pneumatic manifold (Ref Chapter 36).

(4)  
Connect external hydraulic test bench. Do not pressurize hydraulic system A.

(5)  
Remove gear ground lockpin from applicable main landing gear.

(6)  
Place landing ear control lever in UP position.

(7)  
Operate test bench to slowly retract gear.

(8)  
Check that gap between fairing and main gear shock strut door is 0.25 ±0.10 inch.

(9)  
Adjust fairing fore and aft to obtain proper gap.

NOTE: Gap limits at aft end of fairing must be maintained.

(10)
Extend landing gear and remove jacks (Ref Airplane Jacking, Chapter 7).


F.  Check that seal at forward end of fairing contacts structure firmly.
G.  Install access panels L3501/3601R. 
500 
Aug 01/96  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-51-141 Page 401 


G43204
Inboard Flap Track Fairing Installation  535 
27-51-141  Figure 401  Jun 20/90 
Page 402 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 


INBOARD FLAP TRACK FAIRINGS - ADJUSTMENT/TEST
1.  Inboard Flap Track Fairing Adjustment
A.  Adjust Flap Track Fairing
(1)  
Check that gaps at inboard edge and at aft end of fairing are 0.10 (+ 0.05) inch and that mismatch does not exceed 0.03 inch.

(2)  
If gaps and mismatch are not within limits determine amount of adjustment required, remove fairing and proceed as follows:

NOTE:  The following adjustments may be made individually or simultaneously, as necessary.

(3)  
Adjust fairing laterally and vertically as follows:

(a)  
Loosen clamping bolts (5) enough to allow movement of serrated plates (8). (See figure 501.)

(b)  
Position fairing flush with adjacent surfaces.

(c)  
Tighten bolts (5).

 

(4)  
Adjust fairing fore and aft as follows:

(a)  
Loosen nut (2) and checknuts (7). (See figure 501.)

(b)  
Rotate pin (6) as necessary to shift fairing fore and aft to the required position.

(c)  
Tighten nut (2) and checknuts (7). Install cotter pin.

 

(5)  
Rotate fairing as follows:


(a)  Loosen seal assembly attaching screws in inboard side of forward end of fairing.
NOTE:  Seal plate attaching screw holes are elongated to provide for seal plate adjustment.
500 
May 15/67  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-51-141 Page 501 


G19747G21359
Inboard Flap Track Fairing Adjustment  535 
27-51-141  Figure 501 (Sheet 1)  Feb 15/73 
Page 502 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 


500  Inboard Flap Track Fairing Adjustment 
May 15/67  Figure 501 (Sheet 2)  27-51-141 
Page 503 
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 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 3(45)