During all normal flight operations, the hydraulic system operation is unchanged from that of a standard 727-200. In preparation for going to Zero G flight, all three of the modification valves are closed through manual operation of the cockpit switch. When the valves are closed, three status lights change from green to amber, indicating that the valves are closed. Upon completion of the zero-G maneuver, the hydraulic system is restored to normal by opening the three modification valves.
The valve between the reservoir and return line filter is open at all times except during periods of zero-G. It is closed during periods of zero-G, in order to direct return oil to the pump supply line as required by the pumps or to the accumulators. The two valves just below the reservoir are also open at all times except during periods of zero-G. They are closed during periods of zero-g to prevent return oil from going to the reservoir, thereby keeping it confined to the pump supply lines and accumulators.
The hydraulic accumulators are plumbed in parallel with a gage and filler valve on the air side. Prior to installation, the accumulator pistons are positioned to the oil end by pressurizing the air end. The accumulators are installed oil end up and filled with fluid, 2 to 3 in.3 With all components in place and joints and fittings sealed, the air side of the accumulators are serviced with nitrogen to 15 ±3 psig. With the reservoir pressurized to 45 psig from either a nitrogen bottle or engine bleed, the accumulators will contain approximately 100 in.3 of oil.
Zero-G's hydraulic modification was designed for ease of maintenance and simplicity. When the system is not being used for parabolic flight, no special maintenance procedures are needed.
Due to the high-level of involvement by the FAA, all potential problems were anticipated and dealt with in the design — leaving passengers to worry more about their breakfast than the hydraulic controls keeping them safe.