Aircraft for sale & Dry Lase (6 aircraft) six An-148-100V, full service program, all of the equipment, crew training, aircraft maintenance equipment at the airport. The Antonov An-148 is a regional jet airliner designed by the Ukrainian Antonov company and produced by Antonov itself and also on outsource by Russia's Voronezh Aircraft Production Association. The aircraft completed its certification programme on 26 February 2007. The An-148 has a maximum range of 2,100–4,400 km (1,100–2,400 nmi; 1,300–2,700 mi) and is able to carry 68–85 passengers, depending on the configuration. The An-148 aircraft is a high-wing monoplane with two turbofan jet engines mounted in pods under the wing. This arrangement protects the engines and wing structure against damage from foreign objects (FOD). A built-in auto-diagnosis system, auxiliary power unit, high reliability, and the wing configuration allow the An-148 to be used at poorly equipped airfields. Modern flight and navigation equipment, featuring five 15 by 20 cm (5.9 by 7.9 in) liquid crystal display (LCD) panels built by Russia’s Aviapribor and a fly-by-wire system enable the An-148 aircraft to operate day and night, under Instrument flight rules (IFR) and Visual flight rules (VFR) weather conditions on high density air routes. Similar to the Boeing 737, the main landing gear rotates into the belly of the aircraft when in flight, with partial doors covering the legs and the sides of the tires remaining exposed. Other design advantages include the high fuel-efficiency of the Motor Sich D-436-148 engines and entrance stairs that enable boarding and deboarding the aircraft without extra ground equipment.
AN-148V Basic Performance Data | |||
Maximum passenger capacity, pax | 85 | ||
Service range, km | |||
- with 75 pax (32", economy class) | 3500 | ||
Maximum cruising flight speed. km/h | 870 | ||
Maximum cruising flight altitude. m | 12200 | ||
Take-off length requored. m | 1800 | ||
ICAO Landing Category | III A | ||
Aircraft Noise Level | Chapter IV | ||
Aircraft service life: | |||
- hours | 80000 | ||
Engines | |||
- type | D436-148 Turbofan | ||
- thrust (H=0, MCA). kgf | 2 x 6400 | ||
Dimensions An-148-100B |
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Length (m) |
29.1 |
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Wingspan (m) |
28.9 |
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Height (m) |
8.2 |
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Wing area (m2) |
87.3 |
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Weight |
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Maximum take-off weight (kg) |
41 950 |
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Maximum payload (kg) 9 000 |
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Performance |
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Range with max payload (km) |
3 600 |
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Cruise speed (km/h) |
820 |
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Maximum speed (km/h) |
870 |
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Maximum operating altitude (m) |
12 200 |
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Engines |
D-436-148, |
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Fuel flow rate (kg/h) |
1 600 |
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Cabin Data |
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Passengers (1-class) |
75-80 |
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Cabin width (m) |
2.11 |
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