SAE AS 85075 : 2000

Name: SAE AS 85075 : 2000
Brand: SAE

Superseded

View Superseded by

TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR

Superseded date

08-10-2020

Published date

01-01-2000

Publisher

SAE International

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Status	Superseded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	SAE AS85075:2000(R2017)
Supersedes	MIL-T-85075 Revision A:1985

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 RAW MATERIALS
SAE AMS 5643 : 2016	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	DISSIMILAR METALS
MIL-STD-831 Base Document:1963	TEST REPORTS, PREPARATION OF
QQ-C-320 Revision B:1974	CHROMIUM PLATING (ELECTRODEPOSITED)
MIL-T-10727 Revision C:1989	TIN PLATING, ELECTRODEPOSITED OR HOT-DIPPED FOR FERROUS AND NONFERROUS METALS
QQ-S-365 Revision D:1985	SILVER PLATING, ELECTRODEPOSITED, GENERAL REQUIREMENTS FOR
MIL-STD-143 Revision B:1969	STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
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)
MIL-T-85075-2 Revision A:1985	TIE DOWN ASSEMBLY HELICOPTER BLADE CH-53 HELICOPTER
MIL-T-85075-1 Revision A:1985	TIE DOWN ASSEMBLY, HELICOPTER BLADE CH-46 HELICOPTER
MIL-STD-105 Revision E:1989	SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES
QQ-N-290 Revision A:1971	NICKEL PLATING (ELECTRODEPOSITED)