STANAG 3575 : 0
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Agreement to establish the interface and design criteria of aircraft stores ejector racks. Details are given in text.
| DevelopmentNote |
Supersedes DEFSTAN 10-21/1(1976) (08/2003)
|
| DocumentType |
Standard
|
| PublisherName |
NATO
|
| Status |
Withdrawn
|
| MIL-STD-8591 Base Document:2005 | AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE) |
| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| DEFSTAN 00-970(PT13)/7(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/6(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC9/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 9: MILITARY SPECIFIC SYSTEMS |
| 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(PT1)SEC9/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 9: MILITARY SPECIFIC SYSTEMS |
| 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(PT13)/3(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/11(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/4(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/10(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| 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)/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 07-85(PT1)/3(2006) : 2006 | DESIGN REQUIREMENTS FOR WEAPONS AND ASSOCIATED SYSTEMS - PART 1: MANDATORY DESIGN REQUIREMENTS |
| DEFSTAN 00-970(PT1)SEC9/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 9: MILITARY SPECIFIC SYSTEMS |
| DEFSTAN 00-970(PT13)/12(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/8(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 07-085(PT1)/4(2017) : 2017 | DESIGN REQUIREMENTS FOR WEAPONS AND ASSOCIATED SYSTEMS - PART 1: MANDATORY DESIGN REQUIREMENTS |
| DEFSTAN 00-970(PT13)/5(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| 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(PT13)/9(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
| MIL-A-8591 Revision H:1990 | AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR |
| STANAG 7117 : 2008 | RECHARGEABLE PNEUMATIC ENERGY SOURCE FOR AIRCRAFT STORES RELEASE |
| STANAG 3899 : 0 | GROUND FIT AND COMPATIBILITY CRITERIA FOR AIRCRAFT STORES |
| DEFSTAN 13-34/5(1988) : 1988 | CARTRIDGES, EJECTOR RELEASE UNITS |
| DEFSTAN 00-970(PT7)SEC3/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 3: MILITARY SPECIFIC ITEMS |
| MIL-HDBK-1763 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
| STANAG 3441 : 2007 | DESIGN OF AIRCRAFT STORES |
| DEFSTAN 00-970(PT0)/18(2017) : 2017 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| STANAG 3556 : 0 | AIRCRAFT STORE EJECTOR CARTRIDGES |
| STANAG 3605 : 0 | COMPATIBILITY OF ARMING SYSTEMS AND EXPENDABLE AIRCRAFT STORES |
| STANAG 3605 : 0 | COMPATIBILITY OF ARMING SYSTEMS AND EXPENDABLE AIRCRAFT STORES |
| STANAG 4187 : 2007 | FUZING SYSTEMS - SAFETY DESIGN REQUIREMENTS |
| STANAG 3556 : 0 | AIRCRAFT STORE EJECTOR CARTRIDGES |
| STANAG 3726 : 1996 | BAIL (PORTAL) LUGS FOR THE SUSPENSION OF AIRCRAFT STORES |
| STANAG 3441 : 2007 | DESIGN OF AIRCRAFT STORES |
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