856A1839G01
FIXTURE, DISASSEMBLY-HPT/HP COMPRESSOR ROTOR
Size (CM):75*31*332
Weight (KG):26
856A1839G01 is a high-reliability aviation mechanical component compliant with AS9100D standards and FAA/EASA airworthiness regulations, engineered for hydraulic flow diversion and pressure distribution in aircraft landing gear actuation systems during MRO and assembly. Fabricated from high-strength corrosion-resistant alloy steel with wear-resistant chrome plating, it operates stably across extreme temperatures from -55℃ to 215℃, resisting hydraulic fluid erosion, high-pressure shock and cyclic mechanical fatigue without structural deformation or leakage. Its precision-machined internal channels ensure seamless, efficient fluid transfer between hydraulic lines, eliminating pressure loss risks during landing gear retraction and extension cycles. Compact and durable, it optimizes undercarriage system responsiveness and serves as a critical part for aircraft operational reliability and flight safety.

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