| Engine |
Pratt & Whitney PT6A-62 turbo-prop engine with four-bladed, hydraulically driven propeller |
| Power/traction |
1150 HP reduced to 950 HP |
| Propeller diameter |
2,440 m |
| Maximum speed |
593 km/h |
| Range |
1538 km (without additional fuel tanks) |
| Flight duration |
4 h 30 min (without additional fuel tanks) |
| Maximum flight altitude |
11580 m |
| Allowed load factor |
od +7 do -3,5 g |
| Wingspan |
10,19 m |
| Length |
10,17 m |
| Height |
3,26 m |
| Crew |
1 ali 2 |
| Maximum take-off weight |
3200 kg |
| Useful load weight (cargo and fuel) |
1475 kg |
| Under-wing combat load weight |
1040 kg |
| Take-off runway length |
242 m |
| Landing-runway length |
350 m |
| Combat load |
1050 kg |
| Additional equipment and armament |
154 l fuel tank |
| Cargo container |
100 kg |
| 6170 bomb rack |
Mk-81 and Mk-82 |
| T-65 training bomb rack |
BDU in IBDU |
| HMP container with 12.7 machine gun |
250 rounds of ammunition |
| LAU 7A 70 mm launcher |
7 missiles |
| LAU 19A 70 mm launcher |
19 missiles |
| CFP self-protection container |
60 dummies |
| Container with LRF laser |
Up to 20 km |
| ATMS container, including air-to-air missile simulator and heat transmitter |
Up to 7 km |
| DM container used as a counterweight |
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