Gas turbine engine with a geared turbofan arrangement

A gas turbine engine, comprising:

• a propulsive fan,
• a first shaft,
• a second shaft,
• a planetary gearbox including a sun gear, a carrier, an output side and an input side, the planetary gearbox being driveably connected with the first shaft on the output side and with the second shaft on the input side,
• wherein the propulsive fan is supported through a front load path and a rear load path, wherein:
• the front load path comprises a first bearing as an intershaft bearing between the first shaft and the sun gear,
• the rear load path comprises a second bearing between the second shaft and a fixed structure of the gas turbine engine, the second shaft being supported by the second bearing and the fixed structure, and
• the first shaft comprises a first portion of the shaft as a torque carrying part,
• the torque carrying part comprises a torque carrying coupling being connected to the first shaft and to the carrier,
• the propulsive fan is connected to the first shaft and driven by the carrier.