{"id":332401,"date":"2024-10-19T23:09:29","date_gmt":"2024-10-19T23:09:29","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bs-g-257-32004\/"},"modified":"2024-10-25T22:01:08","modified_gmt":"2024-10-25T22:01:08","slug":"bs-g-257-32004","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bs-g-257-32004\/","title":{"rendered":"BS G 257-3:2004"},"content":{"rendered":"
This part of BS G 257 is written to assist engineers working at all levels within companies involved in the aircraft industry to meet the applicable EMH requirements.<\/p>\n
This part of BS G 257 is intended to assist engineers with planning the certification process and to ensure that the correct processes are applied to the writing of procedures and plans, and that the presently recognized methods of test are appropriately used.<\/p>\n
The guide does not contain mandatory requirements, only guidance to assist in the solution of design problems.<\/p>\n
The guide does not cover:<\/p>\n
PDF Pages<\/th>\n | PDF Title<\/th>\n<\/tr>\n | ||||||
---|---|---|---|---|---|---|---|
1<\/td>\n | BRITISH STANDARD AEROSPACE SERIES <\/td>\n<\/tr>\n | ||||||
2<\/td>\n | Committees responsible for this British\ufffdStandard <\/td>\n<\/tr>\n | ||||||
3<\/td>\n | Contents <\/td>\n<\/tr>\n | ||||||
5<\/td>\n | Introduction 1 Scope 2 Normative references <\/td>\n<\/tr>\n | ||||||
6<\/td>\n | 3 Certification process 3.1 Planning 3.2 Route to certification <\/td>\n<\/tr>\n | ||||||
7<\/td>\n | Route to certification <\/td>\n<\/tr>\n | ||||||
8<\/td>\n | 4 Functional criticality 4.1 General 4.2 Assessment of criticality 5 Certification rationale 5.1 General <\/td>\n<\/tr>\n | ||||||
9<\/td>\n | Functional criticality 5.2 Whole aircraft test 5.3 Equipment tests 5.4 Analysis 5.5 Similarity <\/td>\n<\/tr>\n | ||||||
10<\/td>\n | 6 Certification plan 6.1 General 6.2 Contents 7 Test plan 7.1 Test plan key elements 7.2 Outline description of the operation of the systems to be tested 7.3 Pass\/fail criteria for each of the systems <\/td>\n<\/tr>\n | ||||||
11<\/td>\n | 7.4 Methods of achieving testable system modes 7.5 Methods of response measurement to be used 7.6 Preparing the aircraft and\/or system prior to test <\/td>\n<\/tr>\n | ||||||
12<\/td>\n | 8 Equipment level testing 8.1 General 8.2 Magnetic effect 8.3 Power\ufffdinput 8.4 Voltage spike 8.5 Audio frequency conducted susceptibility \u2014 Power outputs 8.6 Induced susceptibility 8.7 RF susceptibility (radiated and conducted) 8.8 Emission of RF energy <\/td>\n<\/tr>\n | ||||||
13<\/td>\n | 8.9 Lightning-induced transient susceptibility 9 Power supply disturbances 9.1 Main areas of disturbance 9.2 Transients 9.3 Over and under voltages 9.4 Harmonics 10 Inter-system EMC 10.1 General <\/td>\n<\/tr>\n | ||||||
14<\/td>\n | 10.2 Transceiver frequency matrix <\/td>\n<\/tr>\n | ||||||
15<\/td>\n | 10.3 Operational assessment 10.4 Measurements of the EM environment due to on-board RF sources <\/td>\n<\/tr>\n | ||||||
17<\/td>\n | 11 HIRF 11.1 General 11.2 Development of the external environment <\/td>\n<\/tr>\n | ||||||
18<\/td>\n | 11.3 Environments 11.4 Peak and average field strengths 11.5 Time factor of incident RF energy and aircraft in flight <\/td>\n<\/tr>\n | ||||||
19<\/td>\n | 11.6 Certification requirements 11.7 Major elements of conformity verification Test requirements <\/td>\n<\/tr>\n | ||||||
21<\/td>\n | Aircraft system function criticality <\/td>\n<\/tr>\n | ||||||
22<\/td>\n | Routes to conformity <\/td>\n<\/tr>\n | ||||||
24<\/td>\n | Routes to conformity \u2014 Expanded view of steps 7 to 9 <\/td>\n<\/tr>\n | ||||||
31<\/td>\n | 11.8 Maintenance, quality control, repair and modifications 12 System susceptibility to lightning 12.1 General <\/td>\n<\/tr>\n | ||||||
32<\/td>\n | 12.2 Certification for lightning protection <\/td>\n<\/tr>\n | ||||||
33<\/td>\n | 12.3 Certification Plan 12.4 Lightning performance assessment <\/td>\n<\/tr>\n | ||||||
36<\/td>\n | 13 Certification report <\/td>\n<\/tr>\n | ||||||
37<\/td>\n | (informative) Requirements of the airworthiness authorities (informative) Requirements of the airworthiness authorities Requirements Introduction Direct effects Indirect effects <\/td>\n<\/tr>\n | ||||||
38<\/td>\n | Standards and specifications Approaches to conformity demonstration Routes Direct effects <\/td>\n<\/tr>\n | ||||||
39<\/td>\n | Indirect effects <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":" Design of electromagnetic hazard protection of civil aircraft – Guide to clearance and testing<\/b><\/p>\n |