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PREN 2282 : 200P1

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

AEROSPACE SERIES - CHARACTERISTICS OF AIRCRAFT ELECTRICAL SUPPLIES

Available format(s)

Hardcopy , PDF

Withdrawn date

07-23-2013

Language(s)

English

0 Introduction
1 Scope
2 Normative references
3 Definitions
4 Requirements common to all electrical power systems
  4.1 General requirements for electrical power generation
  4.2 General requirements for utilization equipment
5 A.C. power system
  5.1 General
  5.2 Supply characteristics for category A (CF) system
  5.3 Supply characteristics for category A (NF) system
  5.4 Supply characteristics for category A (WF) system
  5.5 Requirements relating to utilization equipment
6 D.C. power system 28 V
  6.1 General
  6.2 Supply characteristics for 28 V systems
  6.3 Requirements relating to utilization equipment

Specifies the characteristics of electrical power supplied to the terminals of equipment installed in the aircraft. Also defines the supply system and compatibility requirements for equipment together with the special systems with constant and variable frequency. Applicable to a.c. and d.c. on-board or ground systems.

Committee
C2
DocumentType
Draft
Pages
24
PublisherName
Aerospace & Defence Industries Association of Europe
Status
Withdrawn

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STANAG 3456 : 0 AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS
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