曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

* Upper rod
* Fuse link
* Pivot linkage link
* Frangible cartridge
* Lower rod
* Wear shoe
* Skirt fairing
* Drag link
* Lanyard.
The wear shoe and skirt fairing are on the outside lower surface
of the tail of the airplane. All other tail skid components are in
the lower area of the stabilizer compartment.
Functional Description
When a tail strike occurs that has a small force, the wear shoe
rubs on the runway to absorb the force of the tail strike. Four
wear dimples on the lower surface of the shoe, two forward and
two aft, show when you must replace the wear shoe. You
replace the wear shoe when the material of the shoe wears to
the level of the wear dimples. If the wear shoe hits an object
while it rubs on the runway, the lower part of the wear shoe
shears off. The lower part of the wear shoe shears at the shear
channel. This prevents damage to the tail skid components.
When a tail strike occurs that has a large force, the frangible
cartridge crushes to absorb the force of the tail strike. The wear
shoe attaches to a drag link which pivots on airplane structure.
The warning placard on the aft surface of the skirt fairing shows
how much the cartridge has been crushed. The lower part of the
placard is red, the upper part is green. Usually you can see both
parts of the placard. If you can not see the green part of the
placard, the cartridge has been crushed to its limit. You must
now replace the cartridge. The lanyard holds the drag link when
you replace the cartridge.
If the tail strike has very large force, the force shears the fuse
pin. The fuse pin prevents damage to the airplane structure. The
fuse pin attaches the fuse link to the pivot linkage link. As the tail
skid drag link rotates up with the force, the pivot link rotates up
on its pivot on airplane structure.
Follow this caution when doing maintenance on the tail skid
assembly.
CAUTION: DO NOT LET THE TAIL SKID ASSEMBLY MOVE
FORWARD. THIS CAN CAUSE DAMAGE TO THE
FAIRING.
TAIL SKID - FUNCTIONAL DESCRIPTION
EFFECTIVITY
GUN 001-099, 201-999 32-71-00
Page 6
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
32-71-00-002
TAIL SKID - FUNCTIONAL DESCRIPTION
TAIL SKID - FUNCTIONAL DESCRIPTION
EFFECTIVITY
GUN 001-099, 201-999 32-71-00
Page 7
D633A101-GUN Oct 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
32-71-00-002
CHAPTER
33
Lights
Subject/Page Date COC
EFFECTIVE PAGES
1 thru 7 Oct 10/2006
8 BLANK
33-CONTENTS
1 Jun 10/2002
2 Jun 10/2002
3 Oct 10/2005
4 Oct 10/2005
O 5 Oct 10/2006
O 6 Oct 10/2006
33-00-00
1 Oct 10/2002
2 Oct 10/2002
3 Feb 10/2003
4 BLANK
33-10-00
1 Oct 10/2002
2 Oct 10/2002
3 Feb 10/2003
4 BLANK
33-11-00
1 Oct 10/2002
2 Oct 10/2002
3 Feb 10/2003
Subject/Page Date COC
33-11-00 (cont.)
4 Oct 10/2002
5 Feb 10/2003
6 Oct 10/2002
7 Feb 10/2003
8 Oct 10/2002
9 Feb 10/2003
10 Oct 10/2002
11 Feb 10/2003
12 Oct 10/2002
13 Feb 10/2003
14 Oct 10/2002
15 Feb 10/2003
16 Oct 10/2002
17 Feb 10/2003
18 Oct 10/2002
19 Feb 10/2003
20 Oct 10/2002
21 Feb 10/2003
22 Oct 10/2002
23 Feb 10/2003
24 Oct 10/2002
25 Feb 10/2003
26 Oct 10/2002
A=Added, R=Revised, D=Deleted, O=Overflow, C=Customer Originated Change
33-EFFECTIVE PAGES
Page 1
D633A101-GUN Oct 10/2006
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
CHAPTER 33
Lights
Subject/Page Date COC
33-11-00 (cont.)
27 Feb 10/2003
28 BLANK
33-14-00
1 Oct 10/2002
2 Oct 10/2002
3 Feb 10/2003
4 Oct 10/2002
5 Feb 10/2003
6 Oct 10/2002
7 Feb 10/2003
8 Oct 10/2002
9 Feb 10/2003
10 Oct 10/2002
11 Feb 10/2003
12 Oct 10/2002
13 Feb 10/2003
14 BLANK
33-17-00
1 Oct 10/2002
2 Oct 10/2005
3 Jun 10/2006
4 Oct 10/2002
5 Feb 10/2003
Subject/Page Date COC
33-17-00 (cont.)
6 Oct 10/2002
7 Feb 10/2003
8 Oct 10/2002
9 Feb 10/2003
10 Feb 10/2003
11 Feb 10/2003
12 BLANK
33-18-00
1 Oct 10/2002
2 Oct 10/2002
3 Feb 10/2003
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737NGAMM7(66)