STANAG 3372 : 2014
Current
Current
The latest, up-to-date edition.
LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
05-11-2014
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Describes the essential dimensions, functional configuration and minimum clearances for electrical connectors associated with low pressure air engine starting.
| DevelopmentNote |
Supersedes DEFSTAN 16-10/3(1983) (08/2003)
|
| DocumentType |
Standard
|
| Pages |
6
|
| PublisherName |
NATO
|
| Status |
Current
|
| Supersedes |
| DEFSTAN 00-970(PT1)SEC5/13(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/11(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| 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)/12(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)/15(2015) : 2015 | 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(PT1)SEC5/8(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5 - POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/9(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 5: POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/6(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| DEFSTAN 16-10/3(1983) : 1983 AMD 1 | LOW PRESSURE AIR STARTING OF AIRCRAFT ENGINES |
| JSSG-2001 Revision B:2004 | Air Vehicle |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| DEFSTAN 00-970(PT1)SEC5/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 5: POWERPLANT |
| SAE ARP 1796 : 2015 | ENGINE BLEED AIR SYSTEMS FOR AIRCRAFT |
| DEFSTAN 00-970(PT0)/18(2017) : 2017 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT1)SEC5/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5 - POWERPLANT |
| SAE ARP292C | Environmental Control Systems for Helicopters |
| ISO 2026:1974 | Aircraft Connections for starting engines by air |
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