| Technical data | |
|---|---|
| Type | Yak-18A |
| Function | trainer |
| Year | 1957 |
| Crew | 2 |
| Engine | 260hp AI-14R |
| Length | 8.18m |
| Wing span | 10.6m |
| Wing area | 17m2 |
| Empty Weight | 1025kg |
| Maximum Weight | 1316kg |
| Max. Speed | 263km/h |
| Landing Speed | 105km/h |
| Take off climb | 3.5m/s |
| Take off | 215m |
| Landing Roll | 250m |
| Range | 710km |
| Ceiling | 5060m |
| Climb | |
| 500m | 1.6min |
| 1000m | 3.4min |
| 5000m | 43.2min |
| Payload | |
| Fuel | 95kg |
The Yak-18U with tricycle landing gear turned to be somewhat overweight for M-11FR engine. When new A.I.Ivchenko AI-14 9-cylinder became available, it was quickly fitted to Yak-18U airframe. Smaller outer diameter allowed to replace helmet-type cowling to simple NACA-type with cooling gills, providing all-new look to the aircraft. New metal V-530-D-35 two-blade controllable pitch propeller was installed.
Other changes included metal skinning extended back to the tail, fin area increased (by a small dorsal fillet). Canopy was slightly enlarged, with new raked whip aerial installed. On some late production batches more powerful AI-14FR was fitted, boosting top speed of Yak-18A to the 300km/h.
Yak-18A was first mentioned by Soviet Press as Yak-20.
1052 were assembled in the USSR (Kharkov and Arsenyevsk) during period from 1957 to 1962, and 1796 more in China.
| Predecessors | Modifications |
|---|---|
![]() Yak-18U |
![]() Yak-18P |
| References | Links | |
|---|---|---|
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| Created February 29, 1996 Modified October 26, 1999 |
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