This paper analyzes the reasons of the overtemperature in a turbojet andprovides the available measures to eliminate it

such as the strict requirements for the engine overhaul at the repair factory and the reasonable engine adjustment in the field maintenance. It is essential for the field maintenance to adjust properly the relationship between the turbine pressure ratio and the exhaust nozzle area

so that the turbine gas temperature comes down without afterburning temperature drop. In this way

the influence of the above problem on the operational performance of the engine can be minimized on condition that the engine reliability is guaranteed.