FIELD: aircrafts.
SUBSTANCE: drive unit contains an engine, such as two-circuit turbojet engine (4), and a nacelle containing an air intake, side front fairings (8), a thrust reverser containing deflecting grates (6) and movable rear fairings upstream from the outside around an annular path of a fresh air flow. Side front fairings surround deflecting grates (6) of the thrust reverser when it is closed, while movable rear fairings are made with the possibility of movement backwards with specified grates (6) to open the thrust reverser. The engine contains lifting points (14) forming stable attachment points designed to accommodate manipulation brackets providing the possibility of lifting and transportation of the drive unit. Lifting points (14) are two upper lifting points (14) located on the engine, each on one side of the engine radially behind side front fairings (8) above horizontal diameter (D) of the drive unit.
EFFECT: easier transportation and manipulation of a drive unit is achieved.
14 cl, 10 dwg
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