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owl.Engines library
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AVIADVIGATEL

D-30KP-2

Mixed-flow turbofan

ENGINE9 documented fields
Compare this engine
OpenAP reference record 1AA002. Values describe the source configuration and test conditions. Fuel-flow modes are reference test points, not an in-flight fuel prediction. Dimensions and certified operating limits are not supplied by this dataset.
Reference thrust117600 N
Bypass ratio2.2 :1
Pressure ratio19.45 :1
Takeoff fuel flow1.67 kg/s
REFERENCE COVERAGELoading coverage…
PROVENANCE1 linked source
LAST RETRIEVED2026-09-05
View missing fields and source dates

Source editions

OpenAP engine propertiesEdition / snapshot: Reference snapshot, September 2026Retrieved: 2026-09-05

Retrieval dates record when Owl obtained the data; they are not publication dates or proof that a specification is current. Where the edition contains only a snapshot date, the original publication date is not recorded.

01

Output

Reference maximum thrustOpenAP engine dataset · 1AA002 · max_thrust
117,600 N
02

Architecture

Bypass ratioOpenAP engine dataset · 1AA002 · bpr
2.2 :1
Overall pressure ratioOpenAP engine dataset · 1AA002 · pr
19.45 :1
03

Fuel flow

Approach fuel flowOpenAP engine dataset · 1AA002 · ff_app
0.49 kg/s
Climb-out fuel flowOpenAP engine dataset · 1AA002 · ff_co
1.42 kg/s
Idle fuel flowOpenAP engine dataset · 1AA002 · ff_idl
0.21 kg/s
Reference LTO fuelOpenAP engine dataset · 1AA002 · fuel_lto
703 kg
Takeoff fuel flowOpenAP engine dataset · 1AA002 · ff_to
1.67 kg/s
04

Provenance

Source manufacturer nameHistorical source label retained.
Aviadvigatel

Aircraft connections

Exact engine-name matches in the aircraft catalogue. This is not a complete installation or certification list.

No exact aircraft connection documented in this dataset.

Dimensions, dry weight, shaft-power ratings and certified limits are not documented in this engine dataset.

Sources & context

Reference values vary with model, rating and conditions. Consult the relevant manufacturer documentation for certified specifications.