Aircraft Gas Turbine Engine Rear Frame Strut
Item Name Code (INC) 53247
Additional Information for Aircraft Gas Turbine Engine Rear Frame Strut
The Aircraft Gas Turbine Engine Rear Frame Strut is a component that belongs to the supply class Gas Turbines And Jet Engines, Aircraft, Prime Moving; And Components in the supply group Engines, Turbines, And Components.
The rear frame strut is a structural component that provides support and stability to the rear section of the gas turbine engine. It is typically made of high-strength materials such as titanium or steel to withstand the high temperatures and loads experienced during engine operation.
The rear frame strut connects the rear frame of the engine to other engine components, such as the exhaust system and the engine casing. It helps to distribute the loads and forces generated by the engine, ensuring proper alignment and structural integrity.
In addition to providing structural support, the rear frame strut may also have other functions, such as housing fuel lines, electrical wiring, or other auxiliary systems that are necessary for the operation of the engine.
Overall, the Aircraft Gas Turbine Engine Rear Frame Strut plays a crucial role in the safe and efficient operation of the gas turbine engine, ensuring that it remains stable and properly aligned during operation.
Related Item Names for INC 53247 Aircraft Gas Turbine Engine Rear Frame Strut
NATO Stock Numbers with Item Name 53247 Aircraft Gas Turbine Engine Rear Frame Strut Page 1 of 1
- 70305-02119-101
- RNCC: 3 | RNVC: 2 | DAC: 1
- 4136406
- RNCC: 3 | RNVC: 2 | DAC: D
- 4131508-01
- RNCC: 3 | RNVC: 2 | DAC: D
- 4136692
- RNCC: 3 | RNVC: 2 | DAC: D
- 4131789-01
- RNCC: 3 | RNVC: 2 | DAC: D
- 4135884
- RNCC: 3 | RNVC: 2 | DAC: D
- 4136590
- RNCC: 3 | RNVC: 2 | DAC: D