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  • MIL-P-87210 Base Document:1984

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    PNEUMATIC POWER SYSTEMS, HIGH PRESSURE

    Available format(s):  PDF

    Withdrawn date:  16-03-2007

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Outlines performance, development, compatibility, and verification prerequisites for an aircraft or missile high pressure pneumatic power system and parts.

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

    Committee FSC 1650
    Development Note NOTICE 1 - Notice of Inactivation for New Design. NOTICE 2 - Notice of Cancellation without Replacement. (03/2007)
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Withdrawn

    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
    DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    MIL V 6164 : E VALVE, AIRCRAFT, AIR HIGH PRESSURE

    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-STD-1530 Revision D:2016 AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP)
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL J 5513 : C JOINT, HYDRAULIC SWIVEL
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL-R-8573 Revision A:1957 RESERVOIRS, AIR, NONSHATTERABLE STEEL
    MIL STD 470 : B MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS)
    MIL-STD-875 Revision A:1974 TYPE DESIGNATION SYSTEM FOR AERONAUTICAL AND SUPPORT EQUIPMENT
    SAE ARP 1625 : 2013 COLD GAS SYSTEMS, MISSILE OR PROJECTILES DESIGN, INSTALLATION, TESTS AND REQUIREMENTS FOR
    MIL-G-5514 Revision G:1993 GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR
    SAE ARP 994 : 2016 DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS
    MIL-STD-1568 Revision D:2015 Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems
    MIL-STD-1587 Revision D:2017 MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS
    MIL-STD-882 Revision E:2012 System Safety
    MIL-M-8609 Revision B:1965 MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    MIL-S-8879 Revision C:1991 SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
    MIL-STD-1523 Revision A:1984 AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL
    MIL-STD-471 Revision A:1973 MAINTAINABILITY DEMONSTRATION
    MIL-M-7969 Revision C:1965 Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for
    MIL-STD-490 Revision A:1985 SPECIFICATION PRACTICES
    SAE ARP 584D : 2012 COILED TUBING - CORROSION RESISTANT STEEL, HYDRAULIC APPLICATIONS, AEROSPACE
    MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS
    MIL-C-6591 Revision A:1952 COMPRESSOR UNIT, AIRCRAFT, ELECTRIC MOTOR DRIVEN, GENERAL SPECIFICATION FOR
    MIL-P-83461 Revision B:1980 PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C)
    MIL-STD-1247 Revision D:2009 MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS
    MIL-P-8564 Revision D:1970 PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG]
    MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL-G-4343 Revision C:1978 GREASE, PNEUMATIC SYSTEMS
    MIL-STD-785 Revision B:1980 RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION
    MIL A 83444 : 0 AIRPLANE DAMAGE TOLERANCE REQUIREMENTS
    MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
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