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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 <br /> |
---|---|
Length | 24.3 m79.724 ft <br /> |
Height | 8.3 m27.231 ft <br /> |
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 <br />23 tonnes <br /> kg | Ceiling | FL290 | ROD | 1000 ft/min | APC | B | ||||||||||||
WTC | M | Range | 14001,400 nm <br />2,592,800 m <br />2,592.8 km <br />8,506,561.686 ft <br /> NM |
Accidents & Serious Incidents involving AN30
None on SKYbrary