Designed for use on medium-haul passenger and transport aircrafts with a passenger capacity of up to 120 people or a payload of up to 10 tons. The D-36 series 1 engine was installed on the Yak-42 passenger aircraft, the D-36 series 1A, 2A on the An-72 transport aircraft, the D-36 series 2A, 3A on the An-74 transport aircraft. The engine has the Type Certificate. In conformity with existing ICAO Environmental Standard requirements. In commercial production since 1984.
| series 1 | series 1А, 2А | series 3А | |
| Takeoff (SLS, ISA+15ºС) | |||
| Thrust, kgf | 6,500 | ||
| Specific fuel consumption, kg/h/kgf | 0.358 | ||
| Max cruise (Н=8,000 m, М=0.75, ISA) | |||
| Thrust, kgf | 1,600 | ||
| Specific fuel consumption, kg/h/kgf | 0.65 | ||
| Dimensions, mm | 3,930 × 2,030 × 2,270 | 3,192 × 1,541 × 1,711.5 | 3,192 × 1,541 × 1,711.5 |
| Weight, dry, kg | 1,124 | ||
| Specified service life, h | 18,000 | 24,000 | 18,000 |
| Applicability | Yak-42 | An-72, An-74 | An-74 |
SAAU Type Certificate
IAC AR Type Certificate
Applicability
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Yak-42
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An-74
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(Українська) Аn-72