SAE AS 85075 : 2000
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR
Published date
01-01-2000
Publisher
Superseded date
08-10-2020
Superseded by
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Specifies the tie down assemblies for use on helicopter blades.
| Committee |
AGE-2D
|
| DevelopmentNote |
Supersedes MIL T 85075 (A). (03/2000)
|
| DocumentType |
Standard
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| 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)/13(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)/12(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)/8(2011) : 2011 | 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(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL HDBK 5 : G_VOL2 | METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-H-6875 Revision H:1989 | Heat Treatment of Steel, Process for (S/S by SAE-AMS-H-6875) |
| SAE AMS5643U | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb (Nb) - 4.0Cu Solution Heat Treated, Precipitation Hardenable |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-C-320) |
| MIL-T-10727 Revision C:1989 | TIN PLATING: ELECTRODEPOSITED OR HOT-DIPPED, FOR FERROUS AND NONFERROUS METALS (S/S BY ASTM-B545, ASTM-B339) |
| QQ-S-365 Revision D:1985 | SILVER PLATING, ELECTRODEPOSITED, GENERAL REQUIREMENTS FOR (USERS MAY CONSULT ASTM-B700) |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-STD-794 Revision E:1982 | PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF |
| MIL C 26074 : E | COATINGS, ELECTROLESS NICKEL, REQUIREMENTS FOR |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-T-85075-2 Revision A:1985 | TIE DOWN ASSEMBLY, HELICOPTER BLADE CH-53 HELICOPTER (NO S/S DOCUMENT) |
| MIL-T-85075-1 Revision A:1985 | TIE DOWN ASSEMBLY, HELICOPTER BLADE CH-46 HELICOPTER (NO S/S DOCUMENT) |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
| QQ-N-290 Revision A:1971 | NICKEL PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-N-290) |
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