The invention discloses a device for vibration monitoring data of a turboshaft engine. By means of the device, the problems that factors of hovering, low-altitude flying and the like of existing helicopters are very likely to cause damage, abrasion and corrosion of an engine, besides, factors of installation, use, maintenance and the like of the engine have an influence are solved. The device comprises a main control chip ARM, a high-speed Ethernet chip W5300 connected with the main control chip ARM, a RJ-45 port connected with the high-speed Ethernet chip W5300, a data collection chip FPGA connected with the main control chip ARM, a simultaneous dynamic random access memory (SDRAM) connected with the data collection chip FPGA, an A/D collector connected with the data collection chip FPGA and a signal conditioner connected with the A/D collector. By means of the scheme, the purpose of improvement of the durability and reliability of the engine is achieved, and the device has very high practical value and popularization value.