Il-276 SVTS - Specifications
| New transport | An-12 | IL-276 |
| Layout | freestanding high-wing with single-keystone vertical plumage | single-body high-wing with T-tail |
| Overall Length, m | 33.1 | 37.7 |
| Overall Wingspan, m | 38 | 35.5 |
| Wing area (trapezium), m² | 160 | |
| Height, m | 12.95 | |
| Diameter of fuselage, m | 4.8 | |
| Cargo cabin parameters Length x Width x Height, m | 13.85 x 3.45 x 3.4 | |
| Engines | 4 turboprop | 2 turbojet |
| Engines | forced turboprop engine AI-20M with four-blade propellers of left rotation | Turbofan PS-90A-76 - at the first stage, PD-14 - after the tests |
| Maximum thrust (ISA, H = 0), kgf | 16,000 | |
| Cargo compartment | not sealed | sealed |
| Max. take-off weight, t | 61 | 72 |
| Max. payload, t | 21 | 20 |
| Fuel capacity, l | 25,880 | 30,700 |
| Max. speed, km / h | 670 | 800 |
| Cruising speed, km / h | 800 | |
| Flight altitude, m | 10,200 | 12 100 |
| Range, km | 5700 | 7000 |
| Range of flight with payload of 20 tons, km | 2,000 | |
| Required runway length, m | 1,530 | |
| Crew, people | 3 (2) | |
| Personnel, people |
1-deck version: 70 paratroopers 70 wounded 2-deck version: 150 personnel | |
| Armament |
| There are no data, since the question is in the competence of the Ministry of Defense of the Russian Federation (the customer of this aircraft). |
| Variants |
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| Project life | ||
| Calendar, years | 35 | |
| Number of flights | 24,000 | |
| Number of flying hours, h | 30 000 |
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