Size (CM)：357*242*212 Weight (KG)：2442 856A1122G17 is a certified ground support fixture for aircraft engine turbine blade inspection, engineered to AS9100D quality standards and RTCA DO-160G specifications, optimized for CFM56-5B/-7B and LEAP-1A/1B turbofan MRO workflows. It enables secure, precise positioning of turbine and compressor blades for non-destructive testing (NDT) during overhaul and routine safety checks. Constructed from high-strength alloy steel with anti-corrosion plating, it features adjustable clamping jaws (±0.02mm alignment accuracy), a 360° rotating and tilting work platform, and integrated mounting points for ultrasonic and fluorescent penetrant testing tools. Its ergonomic height (0.7–1.6m) reduces technician fatigue, while non-marring padding protects blade surfaces. Weighing 270kg and measuring 1750×1150×980mm, it complies with FAA/EASA regulations, streamlines NDT processes, minimizes inspection errors, and ensures post-maintenance engine airworthiness for commercial fleets.