• Shopping Cart
    There are no items in your cart

BS 2G 232:1987

Current

Current

The latest, up-to-date edition.

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

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-09-1987

€156.59
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
     interconnect cables (135 deg C)
2. Type 02, class 1: single-core unscreened airframe
     cables (135 deg C)
3. Type 01, classes 2, 3 and 4: multi-core unscreened,
     twisted interconnect cables without jackets
     (135 deg C)
4. Type 02, classes 2, 3 and 4: multi-core unscreened,
     twisted airframe cables without jacket (135 deg C)
5. Type 03, classes 2, 3 and 4: multi-core unscreened,
     twisted interconnect cables with jacket (135 deg C)
6. Type 04, classes 2, 3 and 4: multi-core unscreened,
     twisted airframe cables with jacket (135 deg C)
7. Type 05, classes 1, 2, 3 and 4: single-core screened
     with jacket, interconnect cables (135 deg C)
8. Type 06, classes 1, 2, 3 and 4: single-core screened
     with jacket, and multi-core twisted and screened
     with jacket, airframe cables (135 deg C)
9. Test application
10. Specific test parameters
11. Current ratings in amperes for general purpose
     135 deg C airframe cable
Figure
1. Variation of resistance of copper with temperature

Specifies the construction and performance requirements for a range of lightweight cables with wrapped insulation suitable for general airframe use in the size range 26 to 0000, and for equipment interconnect in the size range 26 to 18.

Committee
ACE/6
DevelopmentNote
Supersedes BS G232(1984) and 85/71991 DC (11/2003) Reviewed and confirmed by BSI, December 2012. (11/2012)
DocumentType
Standard
Pages
22
PublisherName
British Standards Institution
Status
Current
Supersedes

This British Standard specifies construction and performance requirements for a range of lightweight cables with wrapped insulation suitable for general airframe use in the size range 26 to 0000, and for equipment interconnect in the size range 26 to 18. The following types of cable are specified. The cables are suitable for continuous use where the maximum stabilized conductor temperature does not exceed 135 °C. They are suitable 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. 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 short-term and long-term current ratings for the cables are specified in this standard. NOTE The titles of the publications referred to in this standard are listed on the inside back cover.

DEFSTAN 00-970(PT1)SEC6/4(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 6: EQUIPMENT
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)SEC6/12(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 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)SEC6/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
BS G 246:1991 Specification for cable ties for installation under controlled tension on aircraft electric cable harnesses
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT

BS G 230:1984 Specification for general requirements for aircraft electrical cables (second series)
BS G 231:1983 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 G 229:1982 Schedule for environmental conditions and test procedures for airborne equipment
BS 2011-2.1T:1981 Environmental testing. Tests Test T. Soldering

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.