Size (CM): 210*190*50

Weright (KG): 250

J25011-64 is a specialized aircraft fuel system pressure testing manifold, engineered to AS9100D aerospace quality standards and SAE AS4809 specifications, tailored for fuel system maintenance on Boeing 737 MAX and Airbus A320neo narrow-body aircraft during MRO operations.

Crafted from aerospace-grade stainless steel with a PTFE coating for anti-corrosion and contamination resistance, it features a 0–1,500 psi pressure range with ±0.5% accuracy, 6 quick-disconnect ports for simultaneous testing of multiple fuel lines, and a precision pressure relief valve for safety. Weighing 3.1 kg and measuring 280mm×160mm×110mm, it operates at -40°C to 85°C and is compatible with both jet-A fuel and test fluids. Compliant with FAA Part 25 and EASA CS-25 regulations, this manifold verifies fuel line integrity, preventing leaks and ensuring reliable engine fuel delivery for commercial fleets.