856a1213g01 is a high-strength aviation structural component that complies with stringent as9100d standards and faa/easa airworthiness regulations, engineered for load-bearing support and structural stability in aircraft engine mounting assemblies during mro and assembly. fabricated from corrosion-resistant high-tensile steel alloy with a fatigue-resistant anti-corrosion plating, it operates stably across a wide temperature range of -60℃ to 300℃, withstanding engine vibration, thermal expansion stress and aviation fluid erosion without structural deformation. its precision-machined mounting holes ensure seamless integration with engine frames and fuselage structures, eliminating loosening risks during takeoff, cruise and landing phases. compact yet robust, it is a critical part for enhancing engine system reliability and aircraft operational safety.
Full technical pack — materials, tolerances, and inspection records — ships with every unit.
Our in-house engineering team can manufacture custom tooling to match your exact requirements — from one-off airline-specific variants to OEM-equivalent production tools.
This fixture is qualified for use across the following engine and aircraft platforms.
Frequently inquired alongside this fixture — based on shared engine and aircraft platforms.
