956a1620g01 is a high-strength aviation structural component that complies with stringent as9100d standards and faa/easa airworthiness regulations, engineered for load-bearing reinforcement and structural stabilization in aircraft landing gear door assemblies during mro and assembly. fabricated from corrosion-resistant high-tensile aluminum alloy with a wear-resistant hard anodized coating, it operates stably across -60℃ to 230℃, withstanding aerodynamic pressure, landing impact vibration and aviation fluid erosion without structural distortion. its precision-machined mounting slots ensure seamless integration with door frames and fuselage brackets, eliminating jamming risks during gear deployment, taxiing and rough-landing phases. compact yet robust, it is a critical part for enhancing aircraft landing system reliability and overall 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.
