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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Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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Withdrawn date

23-07-2013

Language(s)

English

€184.64
Excluding VAT

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Withdrawn

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09/30212621 DC : 0 BS EN 3682-001 - AEROSPACE SERIES - CONNECTORS, PLUG AND RECEPTACLE, ELECTRICAL, RECTANGULAR, INTERCHANGEABLE INSERT TYPE, RACK TO PANEL, OPERATING TEMPERATURE 150 DEGREE C CONTINUOUS - PART 001: TECHNICAL SPECIFICATION
EN 2592:1990 Aerospace series - Three-pole circuit breakers temperature compensated rated currents up to 25 A - Product standard
EN 2495:1990 Aerospace series - Single-pole circuit breakers temperature compensated rated currents up to 25 A - Product standard

STANAG 3456 : 0 AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS
ISO 1540:2006 Aerospace — Characteristics of aircraft electrical systems
PREN 3830 : 200P1 AEROSPACE SERIES - ELECTRICAL SYSTEM - LOAD ANALYSIS

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