The fuel tank inerting controller monitors and controls the fuel tank inerting system (FTIS). Pressure, oxygen, and temperature data are used by the controller to support the distribution of nitrogen enriched air (NEA) into the fuel tank ullage....
Parker multi ASM pallet is part of a fuel tank inerting system providing inert gas to aircraft fuel tanks. The nitrogen enriched air generation subsystem removes oxygen from the conditioned bleed airstream to supply the tanks with inert gas....
Parker dual flow shutoff valve (DFSOV) is used on the inert gas generation system of an aircraft to control the nitrogen enriched air (NEA) flow to the fuel tanks....
The park brake handle is used to actuate the park brake valve by the pilot....
The rotor brake assembly is a piston actuated, hydraulically operated braking device for stopping the helicopter rotor and preventing rotation of the rotor....
The brake assembly and disc combination are designed and qualification tested to properly and safely decelerate the aircraft under various conditions. The brake assembly consists of one or more pistons depending upon the aircraft requirements....
The multi-rotor steel brake assembly is a piston-actuated, hydraulically operated braking device mounted to the main wheel assemblies and is used for stopping the aircraft....
A carbon brake offers a significant weight savings as compared to steel brakes, consequently, the aircraft is lighter. This has a positive impact on fuel savings, resulting in increased range, and a reduction in engine emissions....
Parker park brake valves are designed for long, reliable service life while holding the aircraft stationary in the closed (locked) position. Valve models range from fairly simple devices to more complex models with additional features....
The nose wheel assembly is located under the nose of the aircraft and is the third wheel of the landing gear system. The nose wheel design consists of two halves bolted together with a tire mounted and ultimately mounted to the nose gear fork....