MIL-W-38387B, MILITARY SPECIFICATION: WEIGHT AND BALANCE SYSTEM, AIRCRAFT, INTEGRAL A/A32H-8 (06-MAY-1976) [NO S/S DOCUMENT]

MIL-W-38387B, MILITARY SPECIFICATION: WEIGHT AND BALANCE SYSTEM, AIRCRAFT, INTEGRAL A/A32H-8 (06-MAY-1976) [NO S/S DOCUMENT]., This specification covers a weight and balance system, designated A/A32H-8, suitable for use in Type C-130 aircraft. The system is to be mounted in the aircraft and become a part of the flight vehicle. No ground equipment nor external ground power is required to operate the system. In use on the ground, the weight and balance system shall weigh the aircraft (including fuel and payload) arid display both its total weight and center-of-gravity. The center-of-gravity shall be displayed as a percent of the mean aerodynamic chord (MAC) of the aircraft.