FIELD: aviation.
SUBSTANCE: invention relates to maintenance of power plants of aircrafts. Manipulation assembly (31) for a propulsion assembly containing a gondola and a turbojet engine of an aircraft contains manipulation shell (35) and at least two mating nodes (43) for attachment of slings. Manipulation shell (35) covers at least half a circumference of outer wall (37) of air intake (33) of the gondola, when the specified propulsion assembly is installed on specified manipulation assembly (31). Mating nodes (43) for attachment of slings are intended for connection to lifting system (47) outer relatively to specified manipulation assembly (31).
EFFECT: possibility of use of a manipulation assembly with gondolas of a laminar type is achieved.
15 cl, 10 dwg
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