DEFSTAN 00-970/VOL2/1(1984) : 1984
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 - ROTORCRAFT
Hardcopy , PDF
27-01-2006
DEFSTAN 00-970(PT7)SEC8/1(2006) : 2006
DEFSTAN 00-970(PT7)SEC5/1(2006) : 2006
DEFSTAN 00-970(PT7)SEC3/1(2006) : 2006
DEFSTAN 00-970(PT7)SEC9/1(2006) : 2006
DEFSTAN 00-970(PT7)SEC10/1(2006) : 2006
DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006
DEFSTAN 00-970(PT7)SEC1/1(2006) : 2006
DEFSTAN 00-970(PT7)SEC6/1(2006) : 2006
DEFSTAN 00-970(PT7)SEC2/1(2006) : 2006
DEFSTAN 00-970(PT7)SEC4/1(2006) : 2006
English
01-01-1984
Consists of 3 books - Book 1 (Parts 0 to 3), Book 2 (Parts 4 to 6), Book 3 (Parts 7 to 10)
DevelopmentNote |
Supersedes DEFSTAN 47-21/1(1979) & DEFSTAN 49-2/2(1975) (08/2003) Supersedes DEFSTAN 53-90(PT1)/1, DEFSTAN 53-90(PT2)/1 & DEFSTAN 53-87/1(1979) (09/2003)
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DocumentType |
Standard
|
Pages |
150
|
PublisherName |
UK Ministry of Defence Standards
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Status |
Superseded
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SupersededBy |
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Supersedes |
DEFSTAN 00-35(PT5)/3(1999) : 1999 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 5: INDUCED MECHANICAL ENVIRONMENTS |
DEFSTAN 00-970(PT1)SEC6/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT |
DEFSTAN 00-35(PT5)/4(2006) : 2006 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 5: INDUCED MECHANICAL ENVIRONMENTS |
DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 03-29/2(1997) : 1997 | PROTECTION OF METALLIC SPRINGS AGAINST CORROSION |
DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-25(PT19)/1(2004) : 2004 | HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 19: HUMAN ENGINEERING DOMAIN |
DEFSTAN 03-29/1(1988) : 1988 | PROTECTION OF METALLIC SPRINGS AGAINST CORROSION |
SAE AIR 1667 : 2013 | ROTOR BLADE ELECTROTHERMAL ICE PROTECTION DESIGN CONSIDERATIONS |
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
BS 4N 100-4(1999) : 1999 | AIRCRAFT OXYGEN SYSTEMS AND EQUIPMENT - PART 4: GUIDE TO THE PHYSIOLOGICAL FACTORS |
DEFSTAN 05-124/1(1992) : 1992 | PROCEDURES FOR THE PROCUREMENT OF AIRCRAFT ENGINES AND THEIR ACCESSORIES |
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