AM.III.F.S14

From the FAA library

• Aviation Maintenance Technician Handbook - Powerplantp. 5-9
  Chapter 5: Engine Starting Systems › Gas Turbine Engine Starters

  This valve directs hot gas to the turbine, bypassing the hot gas nozzle, as the pressure rises above the preset maximum. Thus, the pressure of the gas within the hot gas circuit is maintained at the optimum level ... fuel combustion starter was used to start gas turbine engines by using the combustion energy of jet A fuel and compressed air. The starter consists of a turbine-driven power unit and auxiliary fuel, air, and ignition systems. Operation…

• Aviation Maintenance Technician Handbook - Powerplantp. 5-1
  Chapter 5: Engine Starting Systems › Introduction

  Chapter 5: Engine Starting Systems Introduction Most aircraft engines, reciprocating or turbine, require help during the starting process. Hence, this device is termed the starter. A starter is an electromechanical mechanism capable of developing large amounts of mechanical energy that ... applied to an engine, causing it to rotate. Reciprocating engines need only to be turned through at a relatively slow speed until the engine starts and turns on its own. Once the reciprocating engine has fired and started, the starter…

• Aviation Maintenance Technician Handbook - Powerplantp. 8-17
  Chapter 8: Engine Removal & Replacement › Engine Mounts › Turbine Vibration Isolation Engine Mounts

  Mounts for Turbofan Engines The engine mounts on most turbofan engines perform the same basic functions of supporting the engine and transmitting the loads imposed by the engine to the aircraft structure. Most turbine engine mounts are made of stainless ... steel and are typically located as illustrated in Figure 8-17. Some engine mounting systems use two mounts to support the forward end of the engine and a single mount at the rear end. Turbine Vibration Isolation Engine Mounts…