C 130 Hydraulic System Schematic

C 130 Hydraulic System Schematic. The type of fluid to be used depends on the. Nose landing gear hydraulic system 4.

Web utility hydraulic system (additional simulated schematic to supplement the main schematic), single switch type elevator trim electrical control (control switch and. Located on the forward section, starboard side of the main landing gear. Web hydraulic fluid case hydraulic fluid is specially designed for high pressure applications and for the case hydraulic system.

B Axle Lock A Swing Lock Solenoid Valve 53 Solenoid Valves (Dozer/Stabiliser):

Wing flap hydraulic motor 2. Nose landing gear hydraulic system 4. Web utility hydraulic system (additional simulated schematic to supplement the main schematic), single switch type elevator trim electrical control (control switch and.

Main Landing Gear Brakes 5.

Web as you know at high altitude of aircraft less pressure is require to move rudder ( reduce pressure 1275 to 1300 psi both system) pilot must be monitored the. The type of fluid to be used depends on the. 2nd during flight, crew noticed an issue with the.

B Swing Brake Solenoid Valve A Stabiliser.

Web this module integrates 18 simulated electrical schematics and approximately 150 photographs and drawings to support the teaching and comprehension of this system. Web 1 swing motor a drive isolate 2 swing brake control: Web hydraulic fluid case hydraulic fluid is specially designed for high pressure applications and for the case hydraulic system.

Follow All Safety Recommendations And Safe Shop Practices Outlined In The Front Of This.

Main landing gear hydraulic motors 3. Operated by engines 3, and 4. Located on the forward section, starboard side of the main landing gear.