(b)
Maximum width: 2640 mm (103.9370 in.)
(c)
Height: 1249 mm (49.1732 in.)
(d)
Usable bulk volume: 28.91 m3 (1020.947 ft.3) **ON A/C ALL
(Ref. Fig. 003)
D. Fuselage Datum Lines
(1)
X = Fore and aft distance from any point to STA0.
(2)
Y = Lateral distance from any point to aircraft centerline.
(3)
Z = Vertical distance from any point to aircraft centerline.
R 1EFF : ALL 1 06-10-00Page 11 1 1 May 01/05 1 1 1CES 1
Fuselage Datum Lines Figure 003
1EFF : 1 1R 1CES ALL 1 11 1 06-10-00 Page 12 May 01/05
ZONING - DESCRIPTION AND OPERATION
__________________________________
1. General
_______
The aircraft is divided into zones as follows:
-
the major zones
-
the major sub-zones
-
the zones
A three digit number identifies the zones.
A.
Major zones
**ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
(Ref. Fig. 001)
R **ON A/C 151-199, 401-499,
(Ref. Fig. 001A)
**ON A/C 201-220, 222-223, 225-227, 229-299,
(Ref. Fig. 001B)
**ON A/C 301-399,
(Ref. Fig. 001C)
**ON A/C ALL
(1) The major zones are identified by the hundreds as follows:
-100 Lower Half of the Fuselage to Aft Pressure Bulkhead
-200 Upper Half of the Fuselage to Aft Pressure Bulkhead
-300 STABILIZERS
-400 NACELLES
-500 LEFT WING
-600 RIGHT WING
-700 LANDING GEAR
-800 DOORS
1EFF : ALL 1 06-20-00Page 1 1 1 Aug 01/05 1 1 1CES 1
Major Zones Figure 001
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1224-224, 228-228, 1 1CES 1 111 06-20-00 Page 2 May 01/05
Major Zones Figure 001A
R 1EFF : 1 1 1CES 151-199, 401-499, 1 111 06-20-00 Page 3 Aug 01/05
Major Zones Figure 001B
R 1EFF : 1 1 1CES 201-220, 222-223, 225-227, 229-299, 1 111 06-20-00 Page 4 Feb 01/05
R Major Zones
R Figure 001C
R 1EFF : 301-399, 1 06-20-00 Page 5
1 1 May 01/04
1 1
1CES 1
B. Major sub-zones The major sub-zones are identified by the tens of the major zones
(1) Fuselage and vertical stabilizer
**ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
(Ref. Fig. 002) R **ON A/C 151-199, 401-499,
(Ref. Fig. 002A)
**ON A/C 201-220, 222-223, 225-227, 229-299,
(Ref. Fig. 002B)
**ON A/C 301-399,
(Ref. Fig. 002C)
**ON A/C ALL
(2) Wing and Nacelle (Right and Left)
(Ref. Fig. 003)
C. Zones The zones are identified by the number of the units of the major zones.
(1) Fuselage and vertical stabilizer
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 004) R **ON A/C 151-199, 401-499,
(Ref. Fig. 004A)
1EFF : ALL 1 06-20-00Page 6 1 1 Aug 01/05 1 1 1CES 1
Major Sub-Zones - Fuselage and Vertical Stabilizer
Figure 002
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 06-20-00Page 7 1224-224, 228-228, 1May 01/05 1 1 1CES 1
Major Sub-Zones - Fuselage and Vertical Stabilizer
Figure 002A
R 1EFF : 151-199, 401-499, 1 06-20-00Page 8 1 1 Aug 01/05 1 1 1CES 1
Major Sub-Zones - Fuselage and Vertical Stabilizer
Figure 002B
R 1EFF : 201-220, 222-223, 225-227, 229-299, 1 06-20-00Page 9 1 1 Feb 01/05 1 1 1CES 1R Major Sub-Zones - Fuselage and Vertical Stabilizer R Figure 002C
R 1EFF : 301-399, 1 06-20-00Page 10 1 1 May 01/04 1 1 1CES 1
Major Sub-Zones - Wing and Nacelle (Left and Right) Figure 003
R 1EFF : 1 1 1CES ALL 1 111 06-20-00 Page 11 May 01/04
Zones - Fuselage and Vertical Stabilizer
Figure 004
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 06-20-00Page 12 1 1 May 01/05 1 1 1CES 1
Zones - Fuselage and Vertical Stabilizer
Figure 004A
R 1EFF : 151-199, 401-499, 1 06-20-00Page 13 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 301-399,
(Ref. Fig. 004B)
**ON A/C ALL
(2) Doors **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
(Ref. Fig. 005) R **ON A/C 151-199, 401-499,
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