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ANTONOV An-30
From SKYbrary Wiki
AN30
| Aircraft | |||
|---|---|---|---|
| Name | An-30 | ||
| Manufacturer | ANTONOV | ||
| Body | Narrow | ||
| Wing | Fixed Wing | ||
| Position | High wing | ||
| Tail | Regular tail, low set | ||
| WTC | Medium | ||
| APC | B | ||
| Type code | L2T | ||
| Engine | Turboprop | ||
| Engine count | Multi | ||
| Position | (Front) Wing leading mounted | ||
| Landing gear | Tricycle retractable | ||
| Mass group | 3 | ||
|
| |||
ANTONOV An-30
Description
Aerial survey and mapping aircraft. In service since the early seventies. Special version of An-24 with a glazing nose for survey and cartography is used by many countries in the open skies programme. Can easily be turned into and is often used as an An-26 type transport.
Technical Data
| Wing span | 29.2 m95.801 ft |
|---|---|
| Length | 24.3 m79.724 ft |
| Height | 8.3 m27.231 ft |
| Powerplant | 2 x 2.820 SHP Ivchenko AI-24VT turboprops with 4 blade propellers. |
| Engine model | Ivchenko AI-24 |
Performance Data
| Take-Off | Initial Climb (to 5000 ft) |
Initial Climb (to FL150) |
Initial Climb (to FL240) |
MACH Climb | Cruise | Initial Descent (to FL240) |
Descent (to FL100) |
Descent (FL100 & below) |
Approach | ||||||||||
| V2 (IAS) | kts | IAS | 200 kts | IAS | 200 kts | IAS | 230 kts | MACH | TAS | 286 kts | MACH | IAS | 270 kts | IAS | 240 kts | Vapp (IAS) | kts | ||
| Distance | m | ROC | 1000 ft/min | ROC | 800 ft/min | ROC | 400 ft/min | ROC | ft/min | MACH | ROD | ft/min | ROD | 1500 ft/min | MCS | kts | Distance | m | |
| MTOW | 2300023,000 kg 23 tonnes kg |
Ceiling | FL290 | ROD | 1000 ft/min | APC | B | ||||||||||||
| WTC | M | Range | 14001,400 nm 2,592,800 m 2,592.8 km 8,506,561.686 ft NM |
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Accidents & Serious Incidents involving AN30
None on SKYbrary