
The C-22B requires four crew members and three or four in-flight passenger specialists for passenger service and safety. The avionics package includes one UHF and two VHF radio altimeters, variable instrument switching and two Collins FD-108 flight directors. A third vertical gyro and an additional VHF transceiver are available in case of failure of the primary systems.
The aircraft has heated and pressurized baggage compartments - one on the right side forward and the second just aft of the wheel well. The two compartments provide 425 cubic feet (12.75 cubic meters) of cargo space. The fuselage also incorporates a forward entry door and hydraulically opened integral aft stairs in the tail cone. Fuel is contained in three main tanks inside the wing center section. Rapid pressure fueling and defueling is accomplished at the fueling station on the right wing. The total fuel capacity is approximately 50,000 pounds (22,500 kilograms) of JP-4. Fuel may be dumped down to 35,000 pounds (15,750 kilograms) from all tanks.
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