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BS 3G 233:1990

Current

Current

The latest, up-to-date edition.

Specification for electric cables for general airframe or equipment interconnect use (135°C), extruded insulation

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

21-12-1990

€217.36
Excluding VAT

Foreword
Committees responsible
Specification
1. Scope
2. Classification
3. Construction
4. Designation and marking
5. Packaging and labelling
6. Tests
7. Reference samples
Tables
1. Type 01, class 1: single-core unscreened inter-
     connect cables (135 deg C)
2. Type 01/EL, class 1: single-core unscreened inter-
     connect cables (135 deg C)
3. Type 02, class 1: single-core unscreened airframe
     cables (135 deg C)
4. Type 02/EL, class 1: single-core unscreened airframe
     cables (135 deg C)
5. Type 01, classes 2, 3 and 4: multi-core unscreened,
     twisted interconnect cables without jacket
     (135 deg C)
6. Type 01/EL, classes 2, 3 and 4: multi-core
     unscreened, twisted interconnect cables without
     jacket (135 deg C)
7. Type 02, classes 2, 3 and 4: multi-core unscreened,
     twisted airframe cables without jacket (135 deg C)
8. Type 02/EL, classes 2, 3 and 4: multi-core
     unscreened, twisted airframe cables without jacket
     (135 deg C)
9. Type 03, classes 2, 3 and 4: multi-core unscreened,
     twisted interconnect cables with jacket (135 deg C)
10. Type 04, classes 2, 3 and 4: multi-core unscreened,
     twisted airframe cables with jacket (135 deg C)
11. Type 05, classes 1,2 3 and 4: single-core screened
     with jacket and multi-core twisted and screened
     with jacket, interconnect cables (135 deg C)
12. Type 05/EL, classes 1, 2, 3 and 4: single-core
     screened with jacket and multi-core twisted and
     screened with jacket, interconnect/airframe cables
     (135 deg C)
13. Type 06, classes 1, 2, 3 and 4: single-core screened
     with jacket and multi-core twisted and screened with
     jacket, interconnect airframe cables (135 deg C)
14. Type 06/EL, classes 1, 2, 3 and 4: single-core
     screened with jacket and multi-core twisted and
     screened with jacket, airframe cables (135 deg C)
15. Conductor overall diameter for extra-lightweight
     cables
16. Colour of insulation of class 1 extra-lightweight
     cables
17. Colour of insulation of classes 2, 3 and 4 extra-
     lightweight cables
18. Cable tests and requirements: types 01, 01/EL, 02,
     02/EL
19. Cable tests and requirements: types 05, 05/EL, 06,
     06/EL
20. Cable tests and requirements: types 03 and 04
21. Test applications
22. Specific test parameters
23. Current ratings for general purpose 135 deg C
     airframe cable
Figure
1. Variation of resistance of copper with temperature

Includes an additional range of extra-lightweight insulated cables for general airframe or equipment interconnect use.

Committee
ACE/6
DevelopmentNote
Supersedes 89/71917 DC and BS 2G233(1987). (12/2003) Reviewed and confirmed by BSI, December 2012. (11/2012)
DocumentType
Standard
Pages
28
PublisherName
British Standards Institution
Status
Current
Supersedes

This British Standard specifies construction and performance requirements for a range of lightweight and extra-lightweight cables (designated/EL) with extruded insulation suitable for general airframe use in all sizes. The cables are also suitable for equipment interconnect use in the size ranges 26 to 18 (standard lightweight cable) and 24 to 14 (extra-lightlightweight cable).

The following types of cables are specified:

type 01 and 01/EL interconnect

type 02 and 02/EL airframe

single-core or twisted

multi-cores only;

type 03 interconnect

type 04 airframe

two or more cores

with an outer jacket;

type 05 and 05/EL interconnect

type 06 and 06/EL airframe

single or multi-core,

with a screen and outer jacket.

The cables are suitable for continuous use. where the maximum stabilized conductor temperature does not exceed 135 °C, and for applications involving flexing at temperatures down to – 65 °C.

The cables are suitable for use where the potential between conductors or between a conductor and screen, or the aircraft structure does not exceed 600 V r.m.s and the frequency does not exceed 2 000 Hz.

Interconnect cables are suitable for use in areas with some physical protection, such as behind panels or bulkheads, and may also be used as the basis for cables having additional protection such as a jacket or screen and jacket. They also have an application for the internal wiring of equipment.

Airframe cables are of sufficiently robust construction to be used for open aircraft wiring.

The continuous and short-term current ratings for the cables are specified in this standard.

NOTE 1 The titles of the publications referred to in this standard are listed on the inside back cover.

NOTE 2 The latest revision of an Aerospace Series standard is indicated by a prefix number.

DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT
DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
DEFSTAN 61-12(PT33)/5(2005) : 2005 WIRES, CORDS AND CABLES ELECTRICAL - PART 33: AIRFRAME WIRES AND CABLES IN THE TEMPERATURE CATEGORIES OF 135 DEGREES C, 200 DEGREES C AND 260 DEGREES C
DEFSTAN 61-12(PT33)/4(2001) : 2001 AMD 4 2004 WIRES, CORDS AND CABLES, ELECTRICAL - PART 33: AIRFRAME WIRES AND CABLES IN THE TEMPERATURE CATEGORIES OF 135 DEGREES C, 150 DEGREES C, 200 DEGREES C AND 260 DEGREES C - SECTIONAL SPECIFICATION
DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT

BS 2G 231:1990 Specification for conductors for general-purpose aircraft electrical cables and aerospace applications
BS 3G 100-2.3.13:1973 Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Resistance to fire in designated fire zones
BS 2G 229:1987 Schedule for environmental conditions and test procedures for airborne equipment
BS 2G 230:1991 Specification for general requirements for aircraft electrical cables (second series)
BS 2011-2.1T:1981 Environmental testing. Tests Test T. Soldering

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