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  • MIL-P-8564 Revision D:1970

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    PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG]

    Available format(s):  PDF

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    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Covers requirements for pneumatic components used in aircraft systems conforming to MIL-P-5518.

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

    Committee FSC 1650
    Development Note D NOTICE 1 - Notice of Inactivation for New Design. D NOTICE 2 - Notice of Validation but remains Inactive for New Design. (02/2008)
    Document Type Standard
    Product Note NEW CHILD NOT 3 2019 IS NOW ADDED
    Publisher US Military Specs/Standards/Handbooks
    Status Current

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

    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)/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)/13(2014) : 2014 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)/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
    MIL F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    MIL-T-25363 Revision D:1973 TANK, PNEUMATIC PRESSURE, AIRCRAFT, GLASS FIBER
    MIL B 8075 : D BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF
    SAE AS 1297 : 2008(S2014) REDUCERS, PNEUMATIC PRESSURE, MISSILE
    MIL-S-8812 Revision D:1975 STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR
    MIL-V-19593 Base Document:1956 VALVE-CONTROL, AIRCRAFT PNEUMATIC 28 VOLT D-C SOLENOID OPERATED
    MIL-D-8804 Revision B:1993 DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR
    SAE ARP 1070E : 2019 DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY
    MIL-DTL-9490 Revision E:2008 FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-R-8573 Revision A:1957 RESERVOIRS, AIR, NONSHATTERABLE STEEL
    SAE AIR 4994 : 2013 HIGH PRESSURE PNEUMATIC COMPRESSORS USERS GUIDE FOR AEROSPACE APPLICATIONS
    MIL R 8572 : 0 REDUCERS, PNEUMATIC PRESSURE AIRCRAFT
    SAE ARP 1070 : 2014 DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY
    MIL-P-87210 Base Document:1984 PNEUMATIC POWER SYSTEMS, HIGH PRESSURE
    MIL R 25534 : A NOTICE 1 ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR
    MIL R 25532 : A ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR

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

    MS28772 Revision B:1971 PACKING D, RING, SHOCK STRUT
    MS33540 Revision J:1986 SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR
    MIL-STD-129 Revision R:2014 Military Marking for Shipment and Storage
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    MIL C 26500 : E CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE, CIRCULAR, ENVIRONMENT RESISTING, GENERAL SPECIFICATION FOR
    MS9058 Revision D:1997 RING-BACK-UP, BOSS CONNECTION, AMS 3652, AMS 3656, AMD 3660, AMS 3667
    MIL I 6866 : B INSPECTION, PENETRANT METHOD OF
    MS33515 Revision J:1973 FITTING END, STANDARD DIMENSIONS FOR BULKHEAD FLARELESS TUBE CONNECTIONS
    ASME B46.1 : 2009 SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY)
    MS28774 Revision M:2009 RETAINER, PACKING BACKUP, SINGLE TURN, POLYTETRAFLUOROETHYLENE
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MS28778 Revision C:1984 PACKING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS
    MS33656 Revision J:1987 FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
    QQ-C-320 Revision B:1974 CHROMIUM PLATING (ELECTRODEPOSITED)
    MS33566 Revision B:1975 FITTING, INSTALLATION OF FLARELESS TUBE, STRAIGHT THREADED CONNECTOR
    MS28782 Revision E:2006 RETAINER, PACKING, BACK-UP, TEFLON
    MIL-T-10727 Revision C:1989 TIN PLATING, ELECTRODEPOSITED OR HOT-DIPPED FOR FERROUS AND NONFERROUS METALS
    QQ-S-365 Revision D:1985 SILVER PLATING, ELECTRODEPOSITED, GENERAL REQUIREMENTS FOR
    MIL-G-5514 Revision G:1993 GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR
    MS20995 Revision E:1974 WIRE, SAFETY OR LOCK
    MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MIL-M-8609 Revision B:1965 MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-I-6868 Revision E:1976 INSPECTION PROCESS, MAGNETIC PARTICLE
    MIL C 5541 : E CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS
    MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
    MS28783 Revision F:2006 RING, GASKET, BACK-UP, PTFE
    MIL-P-6906 Revision B:1969 PLATE, IDENTIFICATION AIRCRAFT
    MIL-M-7969 Revision C:1965 MOTOR, ALTERNATING CURRENT, 400 CYCLE, 115/200 VOLT SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL C 5015 : G CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR
    AND10476 : 0002 WASHER - LIMITATIONS ON USAGE OF LOCK
    MIL C 26074 : E COATINGS, ELECTROLESS NICKEL, REQUIREMENTS FOR
    QQ-P-416 Revision F:1991 PLATING, CADMIUM (ELECTRODEPOSITED)
    MS33514 Revision G:1990 FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG)
    MIL-G-4343 Revision C:1978 GREASE, PNEUMATIC SYSTEMS
    QQ-N-290 Revision A:1971 NICKEL PLATING (ELECTRODEPOSITED)
    MS33547 Revision C:1957 PIN, SPRING, FUNCTIONAL LIMITATIONS OF (ASG)
    AN6230 Revision 9:1982 GASKET "O"-RING HYDRAULIC
    MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
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