| AN 148 |
|
 |
| PRODUCT RANGE |
|
|
|
| Antonov An-148 |
| |
| AIRCRAFT PERFORMANCE |
| |
| |
Аn-148-100А
|
Аn-148-100В |
Аn-148-100Е
|
| Basic dimensions |
wingspan (m)
|
28,91
|
28,91 |
28,91 |
aircraft length (m)
|
29,13
|
29,13
|
29,13 |
aircraft height(m)
|
8,19
|
8,19
|
8,19 |
wing area(m2)
|
87,32 |
87,32
|
87,32 |
Mass characteristics
|
maximum takeoff mass (t) |
38,95
|
41,95 |
43,7 |
maximum payload (t) |
9,00 |
9,00 |
9,00 |
maximum fuel load mass (kg) |
11700 |
11700 |
11700 |
Seating capacity
|
crew
|
2 +3 stewards
|
| passengers (max) |
80 |
cruising speed (km/h) |
|
800-870 |
|
maximum payload range (km) |
2100 |
3500 |
4400 |
max. flight height (m) |
|
12500 |
|
fuel consumption per hour (kg/h)
|
1550 |
1600 |
1650 |
| required concrete runway length (m) |
1560 |
1800 |
1885 |
operation temperature (on ground)
|
-55 …….+45
|
ICAO landing category
|
II ( IIIA )
|
Service life
|
| calendar |
30 years
|
30 years
|
30 years
|
number of flights
|
60000 |
40000 |
30000 |
| number of flight hours |
|
80000 |
|
Payload and flight range dependency diagram
Cruising level -11600 m, Cruising Speed – 820 km/h.
En-route fuel reserve: per 30 flight min. on the circuit altitude + 185 km range. +5% from consumed fuel.
Max. fuel weight by γ=0,81 f.m/m³ - 12100 kgf.
Conditions: СА, calm
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