856a2686g01 is a high-reliability aviation structural component compliant with stringent as9100d quality standards and faa/easa airworthiness certifications, engineered for lightweight load-bearing support and vibration isolation in aircraft vertical stabilizer rudder actuator mounting assemblies during mro and original equipment integration. fabricated from high-strength aerospace-grade aluminum alloy, it features a wear-resistant hard anodized finish and hydraulic fluid-compatible coating, delivering stable operation across a temperature range of -60℃ to 240℃. the component withstands cyclic actuation loads, intense flight vibration, and exposure to aviation fluids and environmental contaminants without fatigue, deformation, or chemical degradation. its precision-machined mounting lugs and actuator interfaces ensure seamless integration with rudder systems and vertical stabilizer structures, maintaining actuation precision and structural integrity during all flight phases, including takeoff, cruise, landing, and emergency maneuvering. lightweight yet robust, it is a critical part for enhancing yaw control responsiveness, improving flight stability, and boosting overall aircraft operational safety and handling reliability.
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.
