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DEFSTAN 59-113/2(2012) : 2012

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

LIGHTNING STRIKE PROTECTION REQUIREMENTS FOR SERVICE AIRCRAFT

Available format(s)

Hardcopy , PDF

Superseded date

02-27-2023

Language(s)

English

Published date

01-01-2012

US$78.14
Excluding Tax where applicable

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Superseded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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