Commercial Aircraft Directory - Aircraft Specification
Antonov - An-26
View specification units in: METRIC | IMPERIAL
SPECIFICATION
| First Flight date: | ||
| Certification date: |
PRINCIPAL DIMENSIONS
| Fuselage width: | 2.9 m | |
| Fuselage height: | 8.59 m | |
| Fuselage length: | 23.8 m | |
| Cabin length: | 11.5 m | |
| Cabin width: | 2.78 m | |
| Cabin height: | 1.91 m | |
| Cabin volume: | ||
| Hold volume: |
WEIGHTS
| Empty operating: | 15,850 kg | |
| Max zero fuel: | 21,300 kg | |
| MTOW: | 24,230 kg | |
| MLW: | ||
| Standard fuel capacity: | 5,500 kg | |
| Max fuel capacity: | 5,500 kg |
SPEEDS
| Normal cruise: | ||
| Max cruise: | 540 km/h |
PERFORMANCE
| Long Range Cruise alt: | ||
| Max ceiling: | 7,500 m | |
| Take off field length: | ||
| Landing field length: | ||
| Max Payload Range: | 1,100 m | |
| Range notes: | ||
| Max passengers: | 38 | |
| Typical passengers: | 38 |
POWERPLANT
| Category: | Turboprop | |
| Manufacturer: | Motor Sich / Ivchenko Progress | |
| Model/Submodel: | AI-24 T/VT | |
| Thrust: | 0 kN |
POWERPLANT
| Category: | Turboprop | |
| Manufacturer: | Motor Sich / Ivchenko Progress | |
| Model/Submodel: | AI-24 T/VT | |
| Thrust: | 0 kN |
MAINTENANCE PROVIDERS
| Aircraft Maintenance Base Domodedovo (AMB) |
| Aviation Technical Centre |
| Aviavilsa |
| Joint Stock Company Rostov Civil Aviation Factory N 412 |
| Kiev Aviaremont N410 |
| Volga-Dnepr Gulf (Sharjah, UAE) |
