(Ref. Fig. 005B)
**ON A/C 301-399,
(Ref. Fig. 005C)
**ON A/C ALL
(3) Wing and horizontal stabilizer (left and right) **ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 006) R **ON A/C 151-199, 401-499,
(Ref. Fig. 006A)
1EFF : ALL 1 06-20-00Page 14 1 1 Aug 01/05 1 1 1CES 1
R Zones - Fuselage and Vertical Stabilizer
R Figure 004B
R 1EFF : 301-399, 1 06-20-00 Page 15
1 1 May 01/04
1 1
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Zones - Doors
Figure 005
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 06-20-00Page 16 1224-224, 228-228, 1May 01/05 1 1 1CES 1
Unit Zones - Doors Figure 005A
R 1EFF : 1 1 1CES 151-199, 401-499, 1 111 06-20-00 Page 17 Aug 01/05
Zones - Doors Figure 005B
R 1EFF : 1 1 1CES 201-220, 222-223, 225-227, 229-299, 1 111 06-20-00 Page 18 Feb 01/05
R Unit Zones - Doors
R Figure 005C
R 1EFF : 301-399, 1 06-20-00 Page 19
1 1 May 01/04
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Zones - Wing and Horizontal Stabilizer (Left and Right Sides)
Figure 006
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 06-20-00Page 20 1 1 May 01/05 1 1 1CES 1
Zones - Wing and Horizontal Stabilizer (Left and Right Sides)
Figure 006A
R 1EFF : 151-199, 401-499, 1 06-20-00Page 21 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 06-20-00Page 22 1 1 May 01/04 1 1 1CES 1R Zones - Wing and Horizontal Stabilizer (Left and Right Sides) R Figure 006B
R **ON A/C 301-399,
R (Ref. Fig. 006B)
**ON A/C ALL
(4) landing gear (Ref. Fig. 007)
(5) Nacelle - Left and Right Side (Ref. Fig. 008)
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Zones - Landing gear
Figure 007
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Zones - Nacelles - Left and Right Sides
Figure 008
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1 1 May 01/04
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STATIONS - DESCRIPTION AND OPERATION
____________________________________
1. General
_______
A. Stations
(1)
This section gives the stations and their related frames or ribs.
(2)
The stations (STA) are given in millimeters.
(3)
To facilitate use of this section, the subject is the ATA reference of the system concerned.
B. Stringers
(Ref. Fig. 001)
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Typical Arrangement of Stringers on the Frames
Figure 001
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FUSELAGE - DESCRIPTION AND OPERATION
____________________________________
1. General
_______
The fuselage stations are measured along the X datum line.
The fuselage is divided into frames.
The frames and their stations are shown on the figures below:
-FR0 to FR24
(Ref. Fig. 001)
-FR24 to FR35
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 002) R **ON A/C 151-199, 401-499,
(Ref. Fig. 002A)
**ON A/C 301-399,
(Ref. Fig. 002B)
**ON A/C ALL
-FR35 to FR47
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 003) R **ON A/C 151-199, 401-499,
(Ref. Fig. 003A)
**ON A/C 301-399,
(Ref. Fig. 003B)
1EFF : ALL 1 06-31-53Page 1 1 1 Aug 01/05 1 1 1CES 1
Stations - Fuselage FR0 to FR24.
Figure 001
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1 1 Feb 01/98
1 1
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Stations - Fuselage FR24 to FR35.
Figure 002
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 06-31-53Page 3 1 1 May 01/05 1 1 1CES 1
Stations - Fuselage FR24 to FR35.
Figure 002A
R 1EFF : 151-199, 401-499, 1 06-31-53Page 4 1 1 Aug 01/05 1 1 1CES 1 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM 尺寸和區域(7)
