BS G 229:1982
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Schedule for environmental conditions and test procedures for airborne equipment
Available format(s)
Hardcopy
Language(s)
English
Published date
26-02-1982
Publisher
Superseded date
23-07-2013
Superseded by
€236.17
Excluding VAT
| DocumentType |
Standard
|
| Pages |
0
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy |
| Standards | Relationship |
| ISO 7137:1995 | Identical |
| BS M 62:1987 | Specification for design and qualification testing of clamp blocks for fluid system tube lines having axial alignment. Metric series |
| 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 236:1987 | Specification for electric cables for general airframe or equipment interconnect use (200°C), wrapped insulation with nickel plated conductors |
| BS 2G 232:1987 | Specification for electric cables for general airframe or equipment interconnect use (135°C), wrapped insulation |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| BS G 241:1988 | Specification for fire proof electric cables for engine fire zone and airframe use |
| BS 3G 100-4.1.1:1982 | Specification for general requirements for equipment for use in aircraft. Electrical equipment. Construction and general Electrical insulation tests |
| BS G 248:1993 | Specification for hybrid remote power controllers. General requirements |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| BS G 244:1989 | Code of practice for installation/repair of aircraft electrical interconnection systems |
| BS G 237:1987 | Specification for electric cables for general airframe or equipment interconnect use (200°C), extruded insulation with nickel plated conductors |
| BS 4G 173-1:1985 | Connectors for ground electrical supplies for aircraft Specification for design, performance and test requirements |
| BS G 257-3:2004 | Design of electromagnetic hazard protection of civil aircraft Guide to clearance and testing |
| BS G 243:1990 | Specification for igniter cables for engine use (4 kV d.c.) |
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