The invention relates to an integrated mounting frame for aero-engine test run. The integrated mounting frame for aero-engine test run is characterized by comprising a suspension holder 1, a left main fulcrum switching seat 2, a right main fulcrum switching seat 3, a left main fulcrum supporting seat 4, a right main fulcrum supporting seat 5, a left auxiliary fulcrum switching seat 6, a right auxiliary fulcrum switching seat 7, a left auxiliary fulcrum supporting seat 8, a right auxiliary fulcrum supporting seat 9 and a base plate 10, wherein the suspension holder 1 is bilaterally symmetrical in itself, the left main fulcrum switching seat 2 and the right main fulcrum switching seat 3 are bilaterally symmetrically mounted, the left main fulcrum supporting seat 4 and the right main fulcrum supporting seat 5 are bilaterally symmetrically mounted, the left auxiliary fulcrum switching seat 6 and the right auxiliary fulcrum switching seat 7 are bilaterally symmetrically mounted, the left auxiliary fulcrum supporting seat 8 and the right auxiliary fulcrum supporting seat 9 are bilaterally symmetrically mounted, and the base plate 10 is bilaterally symmetrical in itself. The integrated mounting frame for aero-engine test run has the advantages that the mounting frame can be suitable for supporting test beds and suspension test beds, and can be transported directly on an operation platform to meet the use requirements of engines with similar sizes, so that pre-installation and transfer of the engines are facilitated.