DEFSTAN 00-970(PT0)/3(2003) : 2003
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
Hardcopy , PDF
01-27-2006
English
01-01-2003
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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Superseded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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