AN-148
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|
An-148-100A |
An-148-100B |
An-148-100E |
|
Dimensions | |||
|
wing span (m) |
28,91 | ||
|
overall length (m) |
29,13 | ||
|
overall height (m) |
8,19 | ||
|
wing area (m2) |
87,32 | ||
|
Engines | |||
|
type |
High bypass D-436-148 turbo fans | ||
|
quantity |
2 | ||
|
max takeoff thrust (kg) |
2 ? 6830 | ||
|
compliance with ICAO standards |
Ch. IV, Annex 16 | ||
|
Weight and Volume | |||
|
max takeoff weight (t) |
38,550 |
41,550 |
43,700 |
|
max payload (t) |
9,0 | ||
|
max fuel tanks capacity (t) |
12050/11930 | ||
|
Performance Characteristics | |||
|
cruising speed (km/h) |
800 - 870 | ||
|
max payload range (km) |
2100 |
3500 |
4400 |
|
cruising flight altitude (m) |
12200 | ||
|
average fuel consumption (kg/h) |
1550 |
1600 |
1650 |
|
required concrete runway length (m) |
1560 |
1800 |
1885 |
|
operating temperature range |
-55 …+ 45 | ||
|
ICAO landing category |
I, II, IIIA | ||
|
Crew and Passengers | |||
|
flight crew |
2+2 | ||
|
passengers |
85 (seat pitch 30”) | ||
|
Design and Operational Life | |||
|
calendar |
30 years | ||
|
flight cycles |
60000 |
40000 |
30000 |
|
flight hours |
80000 | ||
| Version | Passenger Capacity | Range (km) |
| An-148-100A | 70-80 | 2000-3000 |
| An-148-100B (basic version) | 70-80 | 3000-4000 |
| An-148-100Å | 70-80 | 4000-5100 |
| Àn-148-100Å1 (extended range version) | 40-55 | 6000-7000 |
| Àn-148-100Å2 (VIP version) | 10-30 | 7500-8500 |
| An-148-200A (stretched-fuselage version) | 90-100 | 2000-3000 |
| An-148-200B (stretched-fuselage version) | 90-100 | 3500-4500 |
| AN-148-100 | AN-148-200 | ||||||
| A | B | E | E1 | E2 | A | B | |
| Passenger capacity | 75 pax | 75 pax | 75 pax | 40 pax | 10 pax | 100 pax | 100 pax |
| Range | 2200 km | 3600 km | 5100 km | 7000 km | 8700 km | 2200 km | 3500 km |
| Maximum fuel load | 12100 kg | ||||||
| Speed | 820-870 km/h | ||||||
| Flight altitude | 11000-11600 m | ||||||
| Required RW length | 1750-2300 m | 2000-2100 m | |||||
| Aerodrome elevation | up to 3000 m | ||||||
| Operating temperature range | -55...+45°C | ||||||
| Fuel consumption | 1454 kg/h | 1690 kg/h | 1770 kg/h | ||||
| Fuel efficiency | 24.0 g/pax | 22.2 g/pax | 22.1 g/pax | ||||
| Landing category | II, IIIA | ||||||
| Community noise level | Chapter IV | ||||||
| Maximum | 37130 kg | 39900 kg | 43050 kg | 13100 kg | 46170 kg | ||
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