DEFSTAN 00-970(PT7)SEC2/SUPPF/4(2014) : INTERIM
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 7: ROTORCRAFT - SUPPLEMENT F: EQUIPMENT (SUBPART F)
30-01-2015
15-12-2014
1 RADIO AND RADAR INSTALLATIONS
2 RADOMES
3 INSTRUMENT/DISPLAY INSTALLATIONS
4 AVIONIC EQUIPMENT INSTALLATIONS
5 STATIC AND PITOT PRESSURE SYSTEMS
6 MAGNETIC COMPASS INSTALLATIONS
7 ELECTRICAL INSTALLATIONS
8 ELECTRICAL SYSTEMS
9 NAVIGATION AND ANTI-COLLISION LIGHTS
10 EMERGENCY LIFERAFT INSTALLATIONS
11 ICE PROTECTION
12 ICE PROTECTION SYSTEMS
13 ELECTROMAGNETIC COMPATIBILITY OF SAFETY
CRITICAL SYSTEMS
14 HYDRAULIC SYSTEMS
15 HYDRAULIC SYSTEMS
16 PNEUMATIC SYSTEMS
17 PRESSURISED GAS STORAGE VESSELS
18 HEALTH AND USAGE MONITORING SYSTEMS
19 RESCUE HOIST AND SONAR HOIST INSTALLATIONS
DevelopmentNote |
Supersedes DEFSTAN 00-970(PT7)SEC2/3(2010). (12/2014)
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DocumentType |
Miscellaneous Product
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PublisherName |
UK Ministry of Defence Standards
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Status |
Superseded
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SupersededBy | |
Supersedes |
STANAG 3456 : 0 | AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS |
STANAG 3153 : 0 | AIRCRAFT NAVIGATION AND ANTI-COLLISION LIGHTS |
BS C 13:1960 | Sizes of gravity filling orifices on aircraft |
STANAG 3632 : 0 | AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING |
STANAG 3329 : 0 | NUMERALS AND LETTERS IN AIRCREW STATIONS |
STANAG 3212 : 2017 | DIAMETERS FOR GRAVITY FILLING ORIFICES |
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