BS 2G 232:1987
Current
The latest, up-to-date edition.
Specification for electric cables for general airframe or equipment interconnect use (135°C), wrapped insulation
Hardcopy , PDF
English
30-09-1987
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 |
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