Size (CM)：96*53*20 Weight (KG)：22 

856A1063G06 CFM56 Compressor Stator Blade Case Installation Tool Kit

Overview
The 856A1063G06 is a professional-grade, specialized tool kit specifically engineered for the installation and assembly of compressor stator blades and casings on CFM56 series engines. This precision-machined set is essential for ensuring the aerodynamic integrity and mechanical alignment of the compressor section. Designed to meet the stringent requirements of aviation maintenance, it is a staple in the toolboxes of world-class MRO facilities and airline engine shops.

Key Points
High-Precision Alignment: Engineered to provide exact positioning of stator blades within the casing, preventing stage-to-stage interference and ensuring optimal engine performance.

Optimized Maintenance Efficiency: Streamlines the complex assembly process of the compressor module, significantly reducing downtime during engine shop visits or line maintenance.

Durable Industrial Construction: Manufactured from high-strength, corrosion-resistant alloys designed to withstand the high-torque and repetitive use environments of aerospace hangars.

Comprehensive Set: Includes all necessary fixtures and guides required for the secure seating of stator vanes and the accurate closure of the compressor case.

Standardized Compliance: Built to align with CFM International’s maintenance manual (AMM) specifications, ensuring that all repairs meet certified airworthiness standards.

Applications
Engine Overhaul (MRO): A vital tool for full-performance restorations and compressor module reassemblies at major maintenance bases.

CFM56 Fleet Support: Compatible with various CFM56 variants, making it a versatile asset for airlines operating Boeing 737 Classic/NG and Airbus A320 family aircraft.

On-Wing Maintenance: Facilitates precise repairs and blade inspections that require casing stabilization or component replacement.

Technical Training: Ideal for use in aviation technical schools and engine training centers to demonstrate standard assembly procedures for high-bypass turbofans.