Size (CM): 109*109*22
Weight (KG): 213.5

Overview
The 856A1411G05 HPT Rotor Rear Blade Fixture is a highly specialized engine maintenance tool engineered for the precise handling of critical hot-section components. Featuring an advanced push-pull clamping mechanism, this fixture is designed to securely hold, position, and stabilize the High Pressure Turbine (HPT) rotor rear blades during complex assembly, disassembly, or inspection procedures in the engine overhaul shop.

Precision & Safety in Engine Maintenance
High Pressure Turbine blades are among the most expensive and delicate components within a jet engine, operating under extreme mechanical and thermal stress. Improper handling or the use of generic clamping tools can easily cause micro-fractures, galling at the dovetail root, or damage to the airfoil coating. The 856A1411G05 utilizes a controlled push-pull action to apply exact, evenly distributed securing force. This eliminates the risk of slipping or over-tightening, ensuring absolute protection for high-value turbine assets while providing technicians with a stable, secure grip for precision work.

Key Features & Benefits
• Push-Pull Mechanism: Delivers swift, secure, and highly controlled clamping force, preventing any mechanical distortion to the blade structure.
• Custom HPT Geometry: Precision-machined to perfectly match the specific contours of the HPT rotor rear blades, ensuring a flawless, non-marring fit.
• Protects Critical Assets: Eliminates the risk of dropped components or surface damage during delicate rotor build-up or tear-down phases.
• Enhanced MRO Efficiency: Streamlines the repetitive and time-consuming process of blade installation and removal, reducing overall engine shop turnaround time (TAT).