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ANTONOV An-70
From SKYbrary Wiki
AN70
| Aircraft | |||
|---|---|---|---|
| Name | An-70 | ||
| Manufacturer | ANTONOV | ||
| Body | Narrow | ||
| Wing | Fixed Wing | ||
| Position | High wing | ||
| Tail | Regular tail, low set | ||
| WTC | Medium | ||
| APC | C | ||
| Type code | L4T | ||
| Engine | Turboprop | ||
| Engine count | Multi | ||
| Position | (Front) Wing leading mounted | ||
| Landing gear | Tricycle retractable | ||
| Mass group | 4 | ||
|
| |||
ANTONOV An-70
Description
Heavy freighter. On order for Russian and Ukrainian Air Force. Developed as replacement for AN-12. Short take-off freighter version An-70T. Presently existing as prototype only. Planned in many military and civil versions.
Technical Data
| Wing span | 44.1 m144.685 ft <br /> |
|---|---|
| Length | 40.7 m133.53 ft <br /> |
| Height | 16.1 m52.822 ft <br /> |
| Powerplant | 4 x 13.800 SHP Progress D-27 turbofans with 14 blade propellers. |
| Engine model | Progress D-27 |
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 | 220 kts | IAS | 400 kts | IAS | kts | MACH | TAS | 430 kts | MACH | IAS | kts | IAS | kts | Vapp (IAS) | kts | ||
| Distance | 1800 m | ROC | 1000 ft/min | ROC | 1000 ft/min | ROC | ft/min | ROC | ft/min | MACH | ROD | ft/min | ROD | ft/min | MCS | kts | Distance | 2200 m | |
| MTOW | 130000130,000 kg <br />130 tonnes <br /> kg | Ceiling | FL400 | ROD | ft/min | APC | C | ||||||||||||
| WTC | M | Range | 730730 nm <br />1,351,960 m <br />1,351.96 km <br />4,435,564.308 ft <br /> NM | ||||||||||||||||
Accidents & Serious Incidents involving AN70
None on SKYbrary