MIL-STD-2089 Base Document:1981
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
AIRCRAFT NONNUCLEAR SURVIVABILITY TERMS (NO S/S DOCUMENT, SEE MIL-HDBK-2089 FOR GUIDANCE)
Available format(s)
PDF
Published date
21-07-1981
Publisher
Superseded date
30-05-1997
Superseded by
£13.91
Excluding VAT
| DevelopmentNote |
For guidance see MIL-HDBK-2089 dated 30 May 1997
|
| DocumentType |
Standard
|
| Pages |
164
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| DEFSTAN 00-970(PT13)/5(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| 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 |
| MIL-STD-2069 Base Document:1961 | REQUIREMENTS FOR AIRCRAFT NONNUCLEAR SURVIVABILITY PROGRAM (S/S BY MIL-HDBK-2069) |
| MIL-HDBK-2069 Base Document:1997 | Aircraft Survivability |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| 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)/7(2011) : 2011 | 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)/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)/11(2013) : 2013 | 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)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | 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 |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| 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-1799 Base Document:1997 | Survivability, Aeronautical Systems (For Combat Mission Effectiveness)(S/S by JSSG-2000 and JSSG-2001) |
| MIL-D-8804 Revision B:1993 | Deicing System, Pneumatic Boot, Aircraft, General Specification for (S/S by SAE-AS8804) |
| DEFSTAN 00-970(PT13)/7(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT7)SEC3/5(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 3: MILITARY SPECIFIC ITEMS |
| DEFSTAN 00-970(PT7)SEC1/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 1: GENERAL AND OPERATIONAL REQUIREMENTS |
| DEFSTAN 00-970(PT13)/11(2015) : 2015 | 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(PT13)/9(2014) : 2014 | 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)/3(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| MIL-STD-1944 Base Document:1985 | POLYMER MATRIX COMPOSITES (NO S/S DOCUMENT) |
| MIL A 46108 : B | ARMOR, TRANSPARENT, GLASS; GLASS/PLASTIC; PLASTIC LAMINATES (GENERAL SPECIFICATION) |
| DEFSTAN 00-970(PT7)SEC1/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 1: GENERAL AND OPERATIONAL REQUIREMENTS |
| DEFSTAN 00-970(PT13)/10(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
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£13.91
Excluding VAT
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