TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR

Amended by

MIL-T-5842 Revision B Notice 1 - Validation:2019

Available format(s)

PDF

Language(s)

English

Publisher

US Military Specs/Standards/Handbooks

Establishes requirements, on aircraft for systems to keep transparent areas clear of frost, ice, fog, rain, snow, salt, insects, dust, gun gas residue and grease.

DocumentType	Standard
Pages	23
ProductNote	NEW CHILD NOT 1 2019 NOW ADDED
PublisherName	US Military Specs/Standards/Handbooks
Status	Current

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DEFSTAN 00-970(PT0)/11(2013) : 2013	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
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DEFSTAN 00-970(PT0)/16(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
AFGS-87266 Base Document:1992	AIRCRAFT COCKPIT TRANSPARENCY SYSTEM
MIL-D-23222 Revision A:1971	DEMONSTRATION REQUIREMENTS FOR HELICOPTERS
MIL-I-8673 Base Document:1955	INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS
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MIL-W-81752 Revision A:1987	WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR
MIL-W-18326 Revision A:1956	WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR
MIL-D-8708 Revision C:1991	DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL-A-9482 Base Document:1954	ANTI-ICING EQUIPMENT FOR AIRCRAFT HEATED SURFACE TYPE, GENERAL SPECIFICATION FOR
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MIL-STD-704 Revision F:2004	AIRCRAFT ELECTRIC POWER CHARACTERISTICS
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MIL-STD-810 Revision G:2008	ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
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MS33656 Revision J:1987	FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
QQ-C-320 Revision B:1974	CHROMIUM PLATING (ELECTRODEPOSITED)
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MIL-E-18927 Revision E:1983	ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR
MIL T 6396 : E	TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING
MIL-STD-882 Revision E:2012	System Safety
MIL-STD-203 Revision G:1991	AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT
MIL A 8625 : F	ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
MIL-STD-250 Revision D:1974	AIRCREW STATION CONTROLS AND DISPLAYS FOR ROTARY WING AIRCRAFT
MIL-STD-1472 Revision G:2012	HUMAN ENGINEERING
MIL-T-18606 Base Document:1955	TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS
QQ-P-416 Revision F:1991	PLATING, CADMIUM (ELECTRODEPOSITED)
MIL R 81589 : NOTICE 1	RAIN REPELLENT FLUID APPLICATION SYSTEM AIRCRAFT WINDSHIELD
MIL-STD-785 Revision B:1980	RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION
MIL-E-7080 Revision B:1962	ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF
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MIL-S-7742 Revision D:1991	SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR