DEFSTAN 59-113/2(2012) : 2012
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
LIGHTNING STRIKE PROTECTION REQUIREMENTS FOR SERVICE AIRCRAFT
Hardcopy , PDF
27-02-2023
English
01-01-2012
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Foreword
0 Introduction
1 Scope
2 Warning
3 Normative References
4 Applicability and Reference Information
5 Requirements
Annex A - External Derived Lightning Environment
(Lighting Threat Levels) to be used as Design
Criteria
Annex B - Lightning Zoning Requirements for
Rotary Wing Aircraft
Annex C - General and Particular Design Requirements
Annex D - Requirements for the Assessment and
Certification of the Capability of Aircraft to
Withstand Lightning Effects
Annex E - Evaluation of the Hazards Caused by Transients
Induced on Aircraft Wiring
Annex F - Evaluation of Fuel and Explosive Vapour Hazards
Annex G - Waveforms for Test and Analysis Derived from
the External Threat
Annex H - Internal Environments and Waveforms
Annex I - Test Methods
Annex J - Preferred Format for Lightning Protection
Plan Status Report
Describes the design, evaluation and testing requirements, with risk assessment procedures, to be used for ensuring the safety and suitability for service of UK Military Aircraft when exposed to a lightning threat.
| DevelopmentNote |
Supersedes DEFSTAN 59-113/1(2006). (11/2012) This standard is obsolescent because it is no longer required for procurement of new equipment but is retained for maintenance purposes in support of existing in-service equipment. (01/2018)
|
| DocumentType |
Standard
|
| Pages |
84
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| DEFSTAN 59-411(PT1)/2(2014) : 2014 | ELECTROMAGNETIC COMPATIBILITY - PART 1: MANAGEMENT AND PLANNING |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
| AEP-41 VOL 6 : 2014 | NATO IMPLEMENTATION OF UNIFIED PROTECTION AGAINST ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE[3]) |
| AECTP-250 : 2014 | ELECTRICAL AND ELECTROMAGNETIC ENVIRONMENTAL CONDITIONS |
| STANAG 4327 : 0 | LIGHTNING, MUNITION ASSESSMENT AND TEST PROCEDURES |
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