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DEFSTAN 00-970(PT0)/3(2003) : 2003

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS

Available format(s)

Hardcopy , PDF

Superseded date

27-01-2006

Language(s)

English

Published date

01-01-2003

€17.53
Excluding VAT

Preface
Section One - General
0 Introduction
1 Scope
2 WARNING
3 Related Documents
4 Definitions
Section Two - Format of 00-970
Section Three - Use of 00-970
Section Four - Qualification of Equipment for Use on Aircraft
Section Five - Amendment Procedure
Section Six - Status of Issue
Annex A - Table of Contents
Annex B - Index
Annex C - Applicable NATO Standardization Agreements (STANAGs)
Annex D - Applicable UK Defence Standards
Annex E - US Military Specifications
Annex F - Definitions
Annex G - Leaflets

Provides guidance and content information, together with definitions of the terms used throughout this document.

DevelopmentNote
Supersedes DEFSTAN 00-970(PT0)/2(1999) (04/2005)
DocumentType
Standard
Pages
64
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy
Supersedes

STANAG 3370 : 2004 AIRCREW STATION ALERTING SYSTEMS
STANAG 3456 : 0 AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS
STANAG 3217 : 2006 OPERATION OF CONTROLS AND SWITCHES AT AIRCREW STATIONS
STANAG 3558 : 2002 LOCATION OF ELECTRICAL CONNECTORS FOR AIRCRAFT STORES
STANAG 3368 : 2014 INTERNAL AIRCRAFT ENGINE STARTING SYSTEM
STANAG 3153 : 0 AIRCRAFT NAVIGATION AND ANTI-COLLISION LIGHTS
STANAG 3104 : 2015 IDENTIFICATION OF AIRCRAFT AND MISSILE PIPELINES AND ELECTRICAL CONDUITS
STANAG 3294 : 0 AIRCRAFT FUEL CAPS AND FUEL CAP ACCESS COVERS
STANAG 3315 : 1998 AIRCRAFT CABIN PRESSURIZING TEST CONNECTIONS
STANAG 3312 : 0 PROFILE DIMENSIONS OF FLANGES FOR V-BAND COUPLINGS FOR PIPING AND DUCTING
STANAG 3278 : 2014 AIRCRAFT TOWING ATTACHMENTS AND DEVICES
STANAG 3639 : 2004 AIRCREW STATION DIMENSIONAL DESIGN FACTORS
STANAG 3865 : 2009 PHYSIOLOGICAL REQUIREMENTS FOR AIRCRAFT MOLECULAR SIEVE OXYGEN CONCENTRATING SYSTEMS
STANAG 3400 : 2010 RESTRAINT OF CARGO IN FIXED WING AIRCRAFT
STANAG 3230 : 2007 EMERGENCY MARKINGS ON AIRCRAFT
STANAG 3499 : 0 CHARACTERISTICS OF SUPPLY EQUIPMENT FOR LIQUID OXYGEN
STANAG 3224 : 2005 AIRCRAFT INTERIOR AND EXTERIOR LIGHTING NIGHT VISION GOGGLE (NVG) AND NON-NVG COMPATIBLE
STANAG 3747 : 2016 GUIDE SPECIFICATIONS (MINIMUM QUALITY STANDARDS) FOR AVIATION TURBINE FUELS (F-24, F-27, F-34, F-35, F-37, F-40 AND F-44)
STANAG 3208 : 2009 AIR CONDITIONING CONNECTIONS
STANAG 3198 : 2017 FUNCTIONAL REQUIREMENTS OF AIRCRAFT OXYGEN EQUIPMENT AND PRESSURE SUITS
STANAG 3766 : 2017 GREASE NIPPLES
STANAG 3632 : 0 AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING
STANAG 3447 : 2016 AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS
STANAG 4270 : 0 AVIATION FUEL DESIGN PARAMETER FOR FUTURE NATO LAND BASED TURBINE POWERED MILITARY AIRCRAFT
STANAG 3296 : 0 AIRCRAFT GASEOUS OXYGEN REPLENISHMENT COUPLINGS
STANAG 3441 : 2007 DESIGN OF AIRCRAFT STORES
STANAG 3258 : 0 POSITION OF PILOT OPERATED NAVIGATION AND RADIO CONTROLS
STANAG 3219 : 0 LOCATION AND GROUPING OF ELECTRICAL SWITCHES IN AIRCRAFT
STANAG 3105 : 2014 PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT
STANAG 3329 : 0 NUMERALS AND LETTERS IN AIRCREW STATIONS
STANAG 3462 : 0 AVAILABILITY OF WEIGHT AND BALANCE REQUIREMENTS AND LOADING CRITERIA FOR TRANSPORT AIRCRAFT
STANAG 3469 : 2010 PARACHUTE EXTRACTION ASSEMBLIES AND AIRCRAFT EXTRACTION PARACHUTE EJECTOR INSTALLATIONS
STANAG 3950 : 0 HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION
STANAG 3209 : 2014 TYRE VALVE COUPLINGS
STANAG 3212 : 2017 DIAMETERS FOR GRAVITY FILLING ORIFICES

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