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BS G 244:1989

Current

Current

The latest, up-to-date edition.

Code of practice for installation/repair of aircraft electrical interconnection systems

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-11-1989

Foreword
Committees responsible
Code of practice
1. Scope
2. Definitions
3. Limitations
4. Sources of supply and user responsibility
5. Installation groups
6. Service life
7. Smoke and fire hazards
8. Electrical protection
9. Cables
10. Cable stripping
11. Cable marking
12. Sleeving
13. Mechanically applied cable ties
14. Terminals
15. Connectors
16. Potting
17. Clips
Tables
1. British Standard cable specifications
2. Nominal current ratings of cables
3. Ultimate storage life
4. Recommended torque loading of terminal assemblies
     for BS G 197 terminal blocks
5. Contact cable size relationship
6. 'P' clips
Figures
1. Matched die type mechanical stripper blades
2. Knife type mechanical stripper blades
3. Terminal bending
4. Preferred orientation of 'P' clips

Guidance on the preferred choice of electrical cables, splices, terminations, connectors and accessories and methods of installing these elements in wiring system form.

This code of practice gives the preferred choice of electrical cables, splices, terminations, connectors and accessories and the methods of installing these elements in wiring system form. The guidance given in this document is intended for general applications where design standards are not provided by a recognized design authority. Such design authority may be implied where the design practices of an approved installation are followed in that same installation for the purposes of modifications or repair.

Attention is drawn to clause 3 ‘Limitations’ of this document.

NOTE. The titles of the publications referred to in this code of practice are listed on the inside back page.

Committee
ACE/6
DevelopmentNote
Supersedes 88/71787 DC. (06/2005) Reviewed and confirmed by BSI, December 2012. (11/2012)
DocumentType
Standard
Pages
22
PublisherName
British Standards Institution
Status
Current

DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F)
SAE AIR 5575 : 2017 HOT STAMP WIRE MARKING CONCERNS FOR AEROSPACE VEHICLE APPLICATIONS

BS G 230:1984 Specification for general requirements for aircraft electrical cables (second series)
BS 2G 198-3:1985 Sleeves for aircraft electric cables and equipment wires Specification for heat-shrinkable sleeving for binding and insulation
BS 3G 198-1:1989 Sleeves for aircraft electric cables and equipment wires Specification for elastomeric sleeves for binding and identification
BS 2G 198-2:1982 Sleeves for aircraft electric cables and equipment wires Specification for slip-on sleeves for identification purposes
BS G 236:1987 Specification for electric cables for general airframe or equipment interconnect use (200°C), wrapped insulation with nickel plated conductors
BS G 231:1983 Specification for conductors for general purpose aircraft electrical cables and aerospace applications
BS G 227:1979 Specification for Tersil type electric cables (metric units)
BS 2G 198-4:1990 Sleeves for aircraft electric cables and equipment wires Specification for semi-rigid high performance heat shrinkable sleeving for binding and insulation
BS G 210:1970 Specification for PTFE insulated equipment wires (with silver plated copper conductors)
BS G 229:1982 Schedule for environmental conditions and test procedures for airborne equipment
BS G221(1976) : LATEST
BS G 232:1984 Specification for electric cables for general airframe or equipment interconnect use (135°C), wrapped insulation
BS G 177:1961 Specification for Nyvin type electrical cables for aircraft
BS G 237:1987 Specification for electric cables for general airframe or equipment interconnect use (200°C), extruded insulation with nickel plated conductors
BS G 203:1967 Specification for Unified screws with captive facing and locking washers
BS G 202:1968 Specification for design and performance requirements for aircraft electrical plugs and sockets for d.c. and low frequency a.c. applications
BS G 225:1979 Specification for performance of environment-resistant terminal junction modules with removable crimp-type contacts
BS G 233:1984 Specification for electric cables for general airframe or equipment interconnect use (135°C), extruded insulation
BS 4G 178-2:1986 Crimped joints for aircraft electrical cables and wires Specification for control of crimping (including user control tests)
BS G 206:1969 Specification for Fepsil type electric cables with copper conductors
SAEITC TS 4 ISSUE 5:2004 PERFORMANCE SPECIFICATION FOR ALL METAL SELF LOCKING NUTS (UNIFIED THREADS) 160,000 LBF/IN[2] MIN. TENSILE (71 TONF/IN[2]) 250 DEGREE C MAX
BS G 239:1987 Specification for primary active lithium batteries for use in aircraft
BS G 235:1987 Specification for electric cables for general airframe or equipment interconnect use (150°C), wrapped insulation with silver plated conductors
BS G 238:1987 Specification for electric cables for general airframe or equipment interconnect use (260°C), wrapped insulation with nickel plated conductors
BS G 222:1976 Specification for Efglas type electric cables (metric units)
BS G 204:1967 Specification for copper terminal ends for crimping to electric cables with copper conductors
BS G197(1967) : LATEST

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