ANTONOV An-24
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AN24
| Aircraft | ||||||
|---|---|---|---|---|---|---|
| Name | An-24 | |||||
| Manufacturer | ANTONOV | |||||
| Body | Narrow | |||||
| Wing | Fixed Wing | |||||
| Position | High wing | |||||
| Tail | Regular tail, high 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-24
Description
Regional airliner and freighter. In service since 1963. Original aircraft of the Antonov family of twin turboprop civil and military transports. Developed to AN-26, -30, -32. Chinese version Y-7 series. More than 1100 An-24s were built. Approximately 880 remain in commercial service. Ukrainian production ceased in 1978, Chinese production continues.
Technical Data
| Wing span | 29.2 m95.801 ft |
|---|---|
| Length | 23.5 m77.1 ft |
| Height | 8.3 m27.231 ft |
| Powerplant | An24: 2 x 2.550 SHP Ivchenko AI-24A turboprops with 4 blade propellers.
Y-7: 2 x 2.790 SHP Dongan WJ5A I turboprops with 4 blade propellers. |
| Engine model | Dongan WJ5, 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 | 230 kts | IAS | 180 kts | MACH | TAS | 242 kts | MACH | IAS | 240 kts | IAS | kts | Vapp (IAS) | kts | ||
| Distance | 1750 m | ROC | 1000 ft/min | ROC | 300 ft/min | ROC | 1000 ft/min | ROC | ft/min | MACH | ROD | ft/min | ROD | 1000 ft/min | MCS | kts | Distance | 1590 m | |
| MTOW | 2100021,000 kg 21 tonnes kg |
Ceiling | FL275 | ROD | ft/min | APC | B | ||||||||||||
| WTC | M | Range | 17001,700 nm 3,148,400 m 3,148.4 km 10,329,396.333 ft NM |
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Accidents & Serious Incidents involving AN24
None on SKYbrary