| Technical data | |
|---|---|
| Type | Il-62 |
| Function | Long-range Passenger |
| Year (service start) |
1967 |
| Crew | 5 |
| Engines |
4*9,500kg NK-8-3 4*10,500kg NK-8-4 |
| Length | 53.12m |
| Height | 12.35m |
| Wingspan | 43.3m |
| Wing area | 282.2m2 |
| Empty weight | 69,400kg |
| Loaded weight | 162,000kg |
| Wing Load (kg/m2) | 574 |
| Thrust to Weight |
0.23 to 0.26 |
| Cruising Speed | 860km/h |
| Cruising Altitude | 10,000m |
| Landing Speed | 230km/h |
| Landing Roll | 1,000m |
| Takeoff Roll | 1,800m |
| Range | |
| Payload 10,000kg | 9,200km+1h |
| Payload 23,000kg | 6,700km+1h |
| Range | km |
| Service Ceiling | 13,000m |
| Payload | |
| Fuel | 83,325kg |
| Cabin size LxWxH | ?x3.49x2.12m3 |
| Seats | 186 |
| Cargo | 23,000kg |
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The routine service of the NK-8 powered Il-62 was initiated on 10 March 1967 on Moscow-Khabarovsk and Moscow-Novosibirsk routes, joined on July 14 by Moscow-Tashkent line. The first International service was to Montreal on September 15 same year for Expo'67.
Czechoslovakia became the first non-Soviet Il-62 operator in 1968, followed by other Eastern block countries. Initial production of 6 airframes/year was extended to 10/year in 1969.
Airframe (see description at Il-62 prototypes) life in the standard version was estimated as 25,000 to 30,000 hours, while engine overhaul time was a point of controversy. Declared originally to be 1,000hours with NK-8-3, it was dropped to 300hours and late raised to 3,000hours when NK-8-4 engines were introduced.
Il-62 was severely criticized for its poor operating economics, and in 1970 new Il-62M-200 version was announced. Today, only few aircraft of the original model Il-62 are left, while the more powerful Il-62M remains in service mainly with Aeroflot, Cubana de Aviacion, Domodedovo Airlines and Khabarovsk Air Enterprise.
| Predecessors | Modifications |
|---|---|
| Il-62 prototypes | Il-62M-200 |
| References | |
|---|---|
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| Created June 30, 1999 |
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