Size (CM): 210*110*60

Weright (KG): 300

J71009-68 is a precision-engineered aircraft engine turbine blade inspection fixture, built to AS9100D aerospace quality standards and Rolls-Royce Technical Specification RRTS 8200, exclusively designed for Trent 700 powerplants on Airbus A330 aircraft during MRO and overhaul operations.

Fabricated from aerospace-grade aluminum alloy with a hard-anodized finish for corrosion resistance and durability, it features a modular, adjustable clamping system that accommodates blade root diameters of 55–70mm and airfoil lengths up to 420mm. Weighing 5.8 kg and measuring 450mm×280mm×210mm, it operates at -40°C to 80°C and includes integrated alignment guides for precise positioning. Compliant with FAA Part 33 and EASA CS-E regulations, this fixture enables non-destructive testing (NDT) of turbine blades, detecting microcracks and wear to preserve engine performance and flight safety for commercial fleets.