856a3752g04 is a high-precision aviation structural component compliant with as9100d standards and faa/easa regulations, engineered for load-bearing and adjustment functions in aircraft horizontal stabilizer trim systems during mro and assembly. fabricated from high-strength corrosion-resistant titanium alloy with fatigue-resistant coating, it withstands extreme temperatures from -60℃ to 220℃, resisting aerodynamic stress, mechanical vibration and aviation fluid erosion without structural deformation. its precision-machined adjustment interfaces ensure seamless, stable fitting with stabilizer trim actuators, eliminating loosening risks during long-haul cruise and critical flight maneuvers. compact yet robust, it optimizes tail compartment space utilization and serves as a critical part for aircraft flight control stability and 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.
