A non-destructive inspection apparatus configured to perform non-destructive inspection of a bonded place between a base material (A1) and a bonding material (A2) of a gas turbine engine part (A), the gas turbine engine part being formed by bonding the bonding material formed of a metal material to the base material formed of a fiber-strengthened material, the non-destructive inspection apparatus comprising: a light source apparatus configured to emit a laser beam to heat the gas turbine engine part; and an infrared imaging apparatus configured to image the gas turbine engine part to which the laser beam is radiated, a moving apparatus configured to move the gas turbine engine part, and including a stage apparatus and an inversion apparatus , the stage apparatus being configured to move the gas turbine engine part in a horizontal direction, the inversion apparatus having a pivot frame to which the gas turbine engine part is fixed and which is rotatable about an axis parallel to the horizontal direction, the inversion apparatus being configured to invert the gas turbine engine part with respect to the light source apparatus by inverting the pivot frame; and a control and arithmetic processing apparatus configured to store form data of the gas turbine engine part, control the moving apparatus such that the laser beam is radiated to the bonded place based on the form data, and obtain a result showing a state of the bonded place based on imaging data obtained by the infrared imaging apparatus, wherein the control and arithmetic processing apparatus is configured to: cause the light source apparatus to emit the laser beam to heat an end portion of the bonded place from a first surface side thereof; acquire imaging data of the end portion of the bonded place of the first surface side by causing the infrared imaging apparatus to image the end portion of the bonded place to which the laser beam is radiated; cause the inversion apparatus to invert the gas turbine engine part with respect to the light source apparatus; cause the light source apparatus to emit the laser beam to heat the end portion of the bonded place from a second surface side thereof different from the first surface side; and acquire imaging data of the end portion of the bonded place of the second surface side by causing the infrared imaging apparatus to image the end portion of the bonded place to which the laser beam is radiated. a light source apparatus configured to emit a laser beam to heat the gas turbine engine part; and an infrared imaging apparatus configured to image the gas turbine engine part to which the laser beam is radiated, a moving apparatus configured to move the gas turbine engine part, and including a stage apparatus and an inversion apparatus , the stage apparatus being configured to move the gas turbine engine part in a horizontal direction, the inversion apparatus having a pivot frame to which the gas turbine engine part is fixed and which is rotatable about an axis parallel to the horizontal direction, the inversion apparatus being configured to invert the gas turbine engine part with respect to the light source apparatus by inverting the pivot frame; and a control and arithmetic processing apparatus configured to store form data of the gas turbine engine part, control the moving apparatus such that the laser beam is radiated to the bonded place based on the form data, and obtain a result showing a state of the bonded place based on imaging data obtained by the infrared imaging apparatus, <EOS>