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DOD STD 1788 : LATEST

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

AVIONICS INTERFACE DESIGN STANDARD (METRIC)

Withdrawn date

23-07-2013

Published date

12-01-2013

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Outlines the form factor, mounting and cooling criteria used for military Line Replacement Units (LRUs) and associated equipment rack installed in military aircraft

DocumentType
Standard
PublisherName
US Military Specs/Standards/Handbooks
Status
Withdrawn

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09/30212621 DC : 0 BS EN 3682-001 - AEROSPACE SERIES - CONNECTORS, PLUG AND RECEPTACLE, ELECTRICAL, RECTANGULAR, INTERCHANGEABLE INSERT TYPE, RACK TO PANEL, OPERATING TEMPERATURE 150 DEGREE C CONTINUOUS - PART 001: TECHNICAL SPECIFICATION
DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
MIL-F-85731 Base Document:1986 FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR
DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT
DOD C 83527 : 0 CONNECTORS, PLUG AND RECEPTACLE, ELECTRICAL, RECTANGULAR MULTIPLE INSERT TYPE, RACK TO PANEL, ENVIRONMENT RESISTING, 150 DEGREES C - TOTAL CONTINUOUS OPERATING TEMPERATURE, GENERAL SPECIFICATION FOR
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
SAE AS 85731 : 2015 FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR
MIL C 83527 : A
DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT

MS14108 Revision F:1987
MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
MIL-F-85731 Base Document:1986 FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-E-6051 Revision D:1967 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
MIL C 38999 : J CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS
MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
MIL-STD-1472 Revision G:2012 HUMAN ENGINEERING
MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS
MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
DOD C 83527 : 0 CONNECTORS, PLUG AND RECEPTACLE, ELECTRICAL, RECTANGULAR MULTIPLE INSERT TYPE, RACK TO PANEL, ENVIRONMENT RESISTING, 150 DEGREES C - TOTAL CONTINUOUS OPERATING TEMPERATURE, GENERAL SPECIFICATION FOR
MIL-STD-1553 Revision B:1978 DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA

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