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MIL-D-8708 Revision C:1991

Current

Current

The latest, up-to-date edition.

Demonstration: Aircraft Weapon Systems, General Specification for

Available format(s)

PDF

Language(s)

English

Published date

12-08-1991

€16.67
Excluding VAT

Covers general requirements of NAVAIR (Naval Air Systems Command Headquarters) for the contractor demonstration of airplanes. Describes reporting requirements relating to demonstrations.

DocumentType
Standard
Pages
284
ProductNote
NEW CHILD NOT 1 2019 IS NOW ADDED.
PublisherName
US Military Specs/Standards/Handbooks
Status
Current

This specification establishes the general requirements for demonstration of Naval aircraft weapon systems during full scale engineering development.

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MIL-A-8860 Revision B:1987 Airplane Strength and Rigidity, General Specification for
MIL-A-8866 Revision C:1987 Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance
MIL T 6396 : E TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING
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DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
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DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
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MIL-A-8863 Revision C:1993 Airplane Strength and Rigidity Ground Loads for Navy Acquired Airplanes
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MIL-I-8670 Revision B:1993 Installation of Fixed Guns and Associated Equipment in Naval Aircraft
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MIL-I-6115 Revision A:1951 Instrument Systems, Pitot Tube and Flush Static Port Operated, Installation of
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MIL-F-8785 Revision C:1980 Flying Qualities of Piloted Airplanes
MIL-STD-704 Revision F:2004 Aircraft Electric Power Characteristics
MIL-P-26366 Revision A:1962 Propeller Systems, Aircraft, General Specification for
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MIL-A-8863 Revision C:1993 Airplane Strength and Rigidity Ground Loads for Navy Acquired Airplanes
MIL-C-7762 Revision A:1967 Compass, Installation of (No S/S Document)
MIL-A-8591 Revision H:1990 Airborne Stores, Suspension Equipment and Aircraft-Store Interface (Carriage Phase); General Design Criteria for (S/S by MIL-STD-8591)
MIL-T-81571 Base Document:1967 THERMAL PROTECTIVE SYSTEM, AIRCRAFT COCKPIT, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT)
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
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MIL-A-8870 Revision C:1993 Airplane Strength and Rigidity Vibration, Flutter, and Divergence
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MIL-I-8675 Base Document:1953 Installations: Aircraft Armor (No S/S Document)
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MIL-E-7016 Revision F:1976 Electric Load and Power Source Capacity, Aircraft, Analysis of
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MIL-T-5842 Revision B:1985 Transparent Areas On Aircraft Surfaces (Windshields And Canopies), Rain Removing And Washing Systems For, De-Frosting, De-Icing, Defogging, General Specification For
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MIL-L-85762 Revision A:1988 LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION
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MIL-I-8670 Revision B:1993 Installation of Fixed Guns and Associated Equipment in Naval Aircraft
MIL-B-5087 Revision B:1964 Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464)
MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
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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 (S/S by MIL-STD-7080)
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MIL-E-81910 Revision A:1977 Electrical Power Generating and Control Equipment, Aircraft, General Specifications for
MIL-G-7940 Revision C:1971 Gages, Liquid Quantity, Capacitor Type, Installation and Calibration of (No S/S Document)
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€16.67
Excluding VAT