Over deze norm
|Commissie||Lucht- en ruimtevaart|
This International Standard specifies electrical output characteristics , and interface requirements, between an aircraft and ground support electrical supplies. This includes all external electric power generation facilities, provided as part of a central source or in point -of-use application. Requirements for safety features are included also. Not addressed in this document are performance and safety issues under regional cont rol. Also excluded are requirements for ground traffic control purposes, such as towing points, identification and warning lights, etc. The electrical characteristics relate to nominal 28 V d.c. and either 115/200 Volt or 230/400 Volt three-phase, 400 Hz, a.c., outputs measured at the aircraft attaching connector as indicated in figure 1.
|Nederlandse titel||Aircraft - Ground support electrical supplies - General requirements|
|Engelse titel||Aircraft - Ground support electrical supplies - General requirements|