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  • MIL-D-8708 Revision C:1991

    Current The latest, up-to-date edition.

    DEMONSTRATION REQUIREMENTS FOR AIRPLANES

    Available format(s):  PDF

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

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

    General Product Information - (Show below) - (Hide below)

    Document Type Standard
    Product Note NEW CHILD NOT 1 2019 IS NOW ADDED.
    Publisher US Military Specs/Standards/Handbooks
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    SAE AS 81366 : 2002 BOUNDARY LAYER CONTROL SYSTEM; PRESSURE
    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
    MIL-STD-7080 Base Document:1994 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
    SAE ARP 217 D : 2016 TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS)
    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)/14(2014) : 2014 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)/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)/15(2015) : 2015 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-HDBK-244 Revision A:1990 GUIDE TO AIRCRAFT - STORES COMPATIBILITY
    MIL-A-8865 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS
    MIL STD 1763 : A AIRCRAFT STORES CERTIFICATION PROCEDURES
    MIL-A-8863 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
    MIL-A-8867 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
    MIL-A-8868 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
    MIL-D-23143 Revision A:1982 DATA, TECHNICAL AIRCRAFT, FOR DESIGN OF AVIATION TRAINING DEVICES
    MIL-I-8670 Revision B:1993 INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT
    JSSG-2006 Base Document:1998 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    MIL W 006729 : B (1) WATERTIGHTNESS OF AIRCRAFT, TESTING
    MIL-A-18717 Revision C:1993 ARRESTING HOOK INSTALLATIONS, AIRCRAFT
    MIL-A-8861 Revision B:1986 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
    MIL-HDBK-1763 Base Document:1998 AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
    MIL-STD-2072 Base Document:1977 SURVIVABILITY, AIRCRAFT, ESTABLISHMENT AND CONDUCT OF PROGRAMS FOR
    MIL-F-8785 Revision C:1980 FLYING QUALITIES OF PILOTED AIRPLANES
    SAE AS 8860 : 2012 LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL-T-5522 Revision D:1975 TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
    MIL-I-6115 Revision A:1951 INSTRUMENT SYSTEMS, PITOT TUBE AND FLUSH STATIC PORT OPERATED, INSTALLATION OF
    DOD-STD-2167 Revision A:1988 DEFENSE SYSTEM SOFTWARE DEVELOPMENT
    MIL-B-83769 Revision D:1983 BATTERY, STORAGE, LEAD ACID, GENERAL SPECIFICATION FOR
    MIL F 15160 : G FUSE, INSTRUMENT, POWER, AND TELEPHONE, GENERAL SPECIFICATION FOR
    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
    DOD-C-85050 Base Document:1982 CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR
    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
    MIL-A-8591 Revision H:1990 AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR
    MIL-T-81571 Base Document:1967 THERMAL PROTECTIVE SYSTEM, AIRCRAFT COCKPIT, GENERAL SPECIFICATION FOR
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL-E-85583 Revision A:1987 ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-P-26292 Revision C:1969 PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF
    MIL-STD-1333 Revision B:1987 AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT
    MIL-C-18244 Revision A:1962 CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL B 85110 : A BAR, REPEATABLE RELEASE HOLDBACK, AIRCRAFT LAUNCHING, GENERAL DESIGN REQUIREMENTS FOR
    MIL-E-6051 Revision D:1967 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
    MIL-A-8870 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    NISO Z39.18 : 1995 SCIENTIFIC AND TECHNICAL REPORTS - PREPARATION, PRESENTATION, AND PRESERVATION
    MIL-STD-1760 Revision E:2007 AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
    MIL-D-6728 Revision A:1956 DAMPER, ENGINE EXHAUST FLAME AND GLARE
    MIL-I-8675 Base Document:1953 INSTALLATION, AIRCRAFT ARMOR
    MIL-C-23866 Revision A:1965 CONTROL SET, APPROACH POWER AN/ASN-54 (V)
    MIL-E-7016 Revision F:1976 ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF
    MIL STD 470 : B MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS)
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MIL E 24021 : J NOTICE 1 ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT
    MIL C 83413 : A CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR
    MIL-L-18276 Revision C:1964 LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF
    MIL-I-8671 Revision D:1994 INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS
    MIL-D-19326 Revision H:1990 DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR
    DOD STD 2169 : 1985 HIGH ALTITUDE ELECTROMAGNETIC PULSE (HEMP) ENVIRONMENT (U) (CLASSIFIED)
    MIL-E-18927 Revision E:1983 ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR
    MIL-S-18471 Revision G:1983
    MIL F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-STD-1388-1 Revision A:1983 LOGISTIC SUPPORT ANALYSIS
    MIL-H-18325 Revision B:1959 HEATING AND VENTILATING SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-F-17874 Revision B:1965 FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
    MIL-T-5842 Revision B:1985 TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR
    MIL-L-22589 Revision D:1991 LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT
    MIL-STD-1757 Revision A:1983 LIGHTNING QUALIFICATION TEST TECHNIQUES FOR AEROSPACE VEHICLES AND HARDWARE
    MIL-L-85762 Revision A:1988 LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION
    MIL-E-5007 Revision D:1973 ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR
    MIL-STD-882 Revision E:2012 System Safety
    MIL F 5372 : D FUSE, CURRENT LIMITER TYPE, AIRCRAFT
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MS90298 Revision C:1981 CONNECTOR, RECEPTACLE ELECTRIC GROUNDING
    MIL-A-8868 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
    MIL-C-8678 Base Document:1984 COOLING REQUIREMENTS OF POWER PLANT INSTALLATIONS
    MIL-A-8867 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
    MIL-STD-471 Revision A:1973 MAINTAINABILITY DEMONSTRATION
    MIL B 8565 : J BATTERY AND CELL, STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-A-8861 Revision B:1986 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
    MIL-F-23447 Base Document:1962 FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF
    MIL-S-8512 Revision D:1974 SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
    MIL-STD-1472 Revision G:2012 HUMAN ENGINEERING
    MIL-W-6729 Revision C:1993 WATERTIGHTNESS OF AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-A-18717 Revision C:1993 ARRESTING HOOK INSTALLATIONS, AIRCRAFT
    MIL B 81757 : C BATTERIES & CELLS STORAGE, NICKEL CADMIUM, AIRCRAFT GENERAL SPECIFICATION FOR
    MIL-T-18606 Base Document:1955 TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS
    MIL-I-85071 Revision A:1992 INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR
    MIL-R-23761 Revision B:1975 Regulators, Voltage, and Control Panels Aircraft, Direct Current Generator, General Specification for
    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 LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
    MIL-I-8700 Revision A:1970 INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR
    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
    MIL-A-19736 Revision A:1960 AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
    MIL-E-81910 Revision A:1977 ELECTRICAL POWER GENERATING AND CONTROL EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATIONS FOR
    MIL-G-7940 Revision C:1971 GAGE, LIQUID QUANTITY, CAPACITOR TYPE, INSTALLATION AND CALIBRATION OF
    MIL-C-5809 Revision G:1987 CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    MIL-STD-877 Base Document:1968 ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF
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