|
3 -engined jet airliner, development of the Yak-40.
Three production modifications (A,D,M) carry up to 120 passengers. First Yak-42 flew on March 25, 1975. Production started
in 1977.
| Technical data | |
|---|---|---|
| Type | Yak-42 | |
| Function | Airliner | |
| Year | 1977 | |
| Crew | 2-4 | |
| Engines | 3*6430kg D-36 | |
| Length | 36.5m | |
| Wingspan | 34.9m | |
| Height | 9.8m | |
| Wing area | 150.0m2 | |
| Empty weight | - | |
| Loaded weight | 52000kg | |
| Wing load | 346.7kg/m2 | |
| Power load | 0.371 | |
| Cruise Speed | 820km/h | |
| Maximum Speed | 870km/h | |
| Landing Speed | 180km/h | |
| Takeoff Roll | 500m | |
| Range (Empty) | 1850km | |
| Range (Loaded) | 1000km | |
| Ceiling | - | |
| Climb | 12.0 m/sec | |
| Payload | ||
| Seats | 120 | |
| Modified January 20, 1998
by Alexandre Savine; |
Back to Main Gate |