|
 |


|
|
|
| SPECIFICATIONS

|
|
Numbers
in parentheses are highest options. |
Aircraft dimensions |
Overall
Length
|
153ft
1in
|
|
46.66m
|
Cabin
Length
|
109ft
1in
|
|
33.25m
|
Fuselage
Diameter
|
18ft
6in
|
|
5.64m
|
Max.
Cabin Width
|
17ft
4in
|
|
5.28m
|
Height
|
51ft
10in
|
|
15.80m
|
Wheelbase
|
49ft
11in
|
|
15.21m
|
Track
|
31ft
6in
|
|
9.60m
|
Wing dimensions |
Wing
Span (geometric)
|
144ft
0in
|
|
43.90m
|
Wing
Area (reference)
|
2 360ft2
|
|
219m2
|
Sweep
(25% chord)
|
28
degrees
|
Design weights |
Max.
Ramp Weight
|
lb x 1
000
|
332.7
(363.5)
|
|
tonnes
|
150.9
(164.9)
|
Max.
Take-off Weight
|
lb x 1
000
|
330.7
(361.6)
|
|
tonnes
|
150.0
(164.0)
|
Max.
Landing Weight
|
lb x 1
000
|
271.2
(273.4)
|
|
tonnes
|
123.0
(124.0)
|
Max.
Zero Fuel Weight
|
lb x 1
000
|
249.1
(251.3)
|
|
tonnes
|
113.0
(114.0)
|
Max.
Fuel Capacity
|
USg
|
16 130 (19
940)
|
|
litres
|
61 070 (75
470)
|
Typical Operating Weight Empty
|
lb x 1
000
|
178.2
(182.1)
|
|
tonnes
|
80.8
(82.6)
|
Typical Volumetric Payload
|
lb x 1
000
|
58.9
(47.6)
|
|
tonnes
|
26.7
(21.6)
|
Basic operating
data |
Powerplants
|
two CF6-80C2 or PW
4000
|
Thrust
Range
|
lb
slst
|
52 000-59 000
|
 |
Typical Seating (two class) |
220 |
Range
(max. pax) |
nm
|
4 350 (5
200)
|
|
km
|
8 050 (9
600)
|
Max.
Operating Mach No. (Mmo)
|
M0.84
|
 |
Containers Underfloor - Standard/Option
|
14
(15)
|
Pallets
Underfloor
|
3 |
Bulk
Hold Volume - Standard/Option
|
610 (318)ft3 |
|
17.3 (9.0)m3 |
Total
Volume - Standard/Option
|
2 822 (2688)ft3 |
|
79.9 (76.1)m3 | | |
 |
TECHNICAL For information on aircraft cabin layouts,
technical specification and performance,
|
|
| | |
 |
ORDERS
AND DELIVERIES |
|
General history of Airbus and
A300/A310 Family product milestones. | |
Vectorial drawings
of our aircraft are
available. | | | |
top
|