Abstract: A tool for forming an abradable coating in an aircraft turbine engine module, this module having an annular stator casing and a central rotor which can move inside the casing about an axis, wherein it has a first portion which is attached to the rotor, a second portion which includes at least one first trans-verse arm extending radially outwards and carrying spreading rollers, and a flywheel centered on the axis and configured to be rotated manually by an operator in order to rotate the tool and the rotor within the casing, so that the spreading rollers are capable of spreading a resin in order to form the coating.