AM.III.B.K6
KnowledgeProcedures required after the installation of a turbine engine.
From the FAA library
- Chapter 8: Engine Removal & Replacement › Introduction
installation procedures for reciprocating, turboprop, and turbofan engines. There are some common tasks that must be accomplished when replacing an aircraft engine. Most engines require disconnecting and reconnecting electrical, hydraulic, fuel supply, intake and exhaust air path components, engine controls ... turbine engines are used in this chapter to describe and represent general and typical procedures for engine buildup, removal, preservation, storage, and installation. Although these two types of engines have some common areas, each procedure has been included to ensure…
- Chapter 8: Engine Removal & Replacement › General Procedures for Engine Removal & Installation › Depreservation of an Engine
solvent to remove all accumulations that could restrict the oil circulation and…
- Chapter 10: Engine Maintenance & Operation › Combustion Section Inspection › Turbine Blade Replacement Procedure
Turbine Blade Replacement Procedure Turbine blades are generally replaceable, subject to moment-weight limitations. These limitations are contained in the engine manufacturer’s applicable technical instructions. If visual inspection of the turbine assembly discloses several broken, cracked, or eroded blades ... turbine disc. The number 1 blade is then installed adjacent to the number 1 on the disc. [Figure 10-68] The remaining blades are then installed consecutively in a clockwise direction, viewed from the rear face of the turbine disc…