BS 3G 233:1990
Current
The latest, up-to-date edition.
Specification for electric cables for general airframe or equipment interconnect use (135°C), extruded insulation
Hardcopy , PDF
English
21-12-1990
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 |
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.