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MIL-B-8584 Revision C:1970

Current

Current

The latest, up-to-date edition.

Brake Systems, Wheel, Aircraft, Design of

Available format(s)

PDF

Published date

12-08-1970

€16.67
Excluding VAT

DevelopmentNote
The initial release of SAE AS 8584 is intended to replace MIL B 8584 (C). (11/2002)
DocumentType
Standard
Pages
16
ProductNote
NEW CHILD NOT 1 2019 IS NOW ADDED.
PublisherName
US Military Specs/Standards/Handbooks
Status
Current

This specification covers the brake system design requirements for aircraft equipped with wheel-type landing gear.

MIL A 8862 : 0 AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS
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)/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)/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-8891 Revision A:1978 Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation and Data Requirements for, General Specification for
MIL-H-5440 Revision H:1993 Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440)
MIL-T-5522 Revision D:1975 Test Requirementsand Methodsfor Aircraft Hydraulicand Emergency Pneumatic Systems (S/S By MIL-STD-5522)
MIL-HDBK-516 Revision C:2014 Airworthiness Certification Criteria
MIL-HDBK-759 Revision C:1995 Human Engineering Design Guidelines (No S/S Document)
SAE ARP5632 Rotorcraft: Application of Existing Aircraft Designed Tires, Wheels and Brakes
SAE AS6026A Control Unit, Pressure Generating, Manually Operated, Aircraft Hydraulic Brake System
SAE ARP5770 Mechanical Control Design Guide
MIL-STD-1333 Revision B:1987 AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT (NO S/S DOCUMENT)
MIL-L-87139 Base Document:1979 LANDING GEAR SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES. WRIGHT-PATTERSON AFB OH 45433-6503
SAE AIR1934A Use of Structural Carbon Heat Sink Brakes on Aircraft
JSSG-2009 Revision A:2013 Air Vehicle Subsystems
MIL-W-5013 Revision L:1991 Wheel and Brake Assemblies, Aircraft General Specification For

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€16.67
Excluding VAT