| General Information | |
|---|---|
| Type | An-218 |
| Function | Airliner |
| Year | Project |
| Crew | 2 + flight attendants |
| Powerplant | |
| Type (major) | 2*D-18TM |
| Thrust (static) | 2*25,000kg |
| Fuel consumption | 2*9.0 g/passenger/km |
| Type (upgrade I) | 2*D-18TP |
| Thrust (static) | 2*27,500kg |
| Type (upgrade II) | 2*Rolls-Roys RB.211-524H4 |
| Thrust (static) | 2*?kg |
| Size | |
| Length | 58.15m |
| Fuselage Diameter | 5.62m |
| Height | 15.6m |
| Wingspan | 50.0m |
| Wing area | 270m2 |
| Weights and loads | |
| Empty (equipped) | 90,000 to 91,000kg |
| Maximum takeoff | 170,000kg |
| Wing Load (kg/m2) | 630 |
| Thrust to Weight | 3.1 |
| Speed | |
| Cruising at 11,000m | 860km/h |
| Landing | ?km/h |
| Takeoff/Landing | |
| Runway required | 2900m |
| Range | |
| Maximum payload | 4570km |
| 400 passengers | 5100km |
| 350 passengers | 6300km |
| 300 passengers | 7200km |
| 200 passengers | 9400km |
| Ceiling | |
| Cruising | 10,100 to 21,100m |
| Payload | |
| Fuel | ?kg |
| Maximum Cargo | 42,000kg |
| Cabin size LxWxH | ?m3 |
| Seats (spacing) | |
| Economy (81cm) | 350 to 400 |
| 3-class (102/87/81cm) | 300 |
| Other | |
| Airframe resource | 60,000 flight hours |
| Annual flight time | 3,500 to 4,000 hours |
| Service | 9.5 man-hours per flight-hour |
Project of wide-body Airbus-class airliner for mid-range routes was initiated in 1991. It is the first attempt of the Antonov ANTK to develope aircraft of this class. Special attention was paid to aircraft reliability - the plane was designed according to damage tolerance approach: fatigue cracks were not allowed to cause catastrophic failure between scheduled maintenance inspections.
An-218 design includes solutions, technologies and schemes developed for commercial cargo planes An-124 and An-70. Parts and components of series Tu-204 airliner are used. Production was planned at Ukraina in cooperation with Russian aircraft plants.
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Landing gear construction allows to operate An-218 from same airfield used by the Tu-154M and Tu-204. This expands service area from 19 used by the closest analog Il-86 to more than 50. It is estimated that fuel consumption per passenger per km may be almost half of the Il-86. New aircraft also has to surpass Il-86 and Tu-154M on passenger comfort, cargo handling and serviceability.
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Perspective modification include long-range variant for 200 to 220 seats and stretched version carrying up to 400 passengers.
On-board electronics and navigation equipment corresponds to IIIA ICAO requirements. Pilots cockpit has high degree of automatization, flight control and monitoring system includes six multi-color multi-functional displays.
An-218 had technical documentation supposed to be ready in 1991, and first flight was scheduled for 1994. C.I.S. certification was planned for 1995.
| Predecessors | Modifications | |
|---|---|---|
| Tu-204 | An-218-100 | An-218-200 |
| An-218-300 | An-218-400 | |
| References | |
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| Links | |
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| Created November 27, 2000 |
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