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  • MIL S 25057 : B

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR

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    Withdrawn date:  23-07-2013

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    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Outlines requirements for retractable and fixed air inlet screen systems for use with gas turbine engines.

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

    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Withdrawn

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

    MIL-I-83294 Base Document:1971 INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR

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

    MIL-I-81550 Revision C:1983 INSULATING COMPOUND, ELECTRICAL, EMBEDDING, REVERSION RESISTANT SILICONE
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    TT-P-1757 Revision B:1997 PRIMER COATING, ALKYD BASE, ONE COMPONENT
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    MIL-M-3171 Revision C:1966 MAGNESIUM ALLOY PROCESSES FOR PRETREATMENT AND PREVENTION OF CORROSION
    TT-E-489 Revision J:1994 ENAMEL, ALKYD, GLOSS, (FOR EXTERIOR AND INTERIOR SURFACES)
    MIL-STD-480 Revision B:1988 CONFIGURATION CONTROL - ENGINEERING CHANGES, DEVIATIONS AND WAIVERS
    MS35649 Revision H:1988 NUT, PLAIN, HEXAGON, MACHINE SCREW, UNC-2B
    MIL-D-8181 Revision B:1965 DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR
    MS9500 Revision A:1969 BOLT, MACHINE CRES AMS 5731, HEXAGON HEAD, DRILLED, 1 HOLE, 190-32 UNJF-3A
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    AN737 Revision 8:1956 CLAMP, HOSE, AIRCRAFT
    MIL-STD-831 Base Document:1963 TEST REPORTS, PREPARATION OF
    MIL-STD-838 Revision C:1983 LUBRICATION OF MILITARY EQUIPMENT
    MIL S 8516 : F SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED
    MIL-STD-143 Revision B:1969 STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
    MIL-S-8879 Revision C:1991 SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
    MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
    MIL-STD-1523 Revision A:1984 AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL
    MIL S 23586 : E SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED
    MIL-STD-100 Revision G:1997 ENGINEERING DRAWINGS
    MIL-E-38453 Revision A:1971 ENVIRONMENTAL CONTROL, ENVIRONMENTAL PROTECTION, AND ENGINE BLEED AIR SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR
    MIL-T-5544 Revision C:1991 THREAD COMPOUND, ANTISEIZE, GRAPHITE-PETROLATUM
    MIL C 6021 : H NOTICE 1 CASTINGS, CLASSIFICATION AND INSPECTION OF
    MIL-F-7179 Revision G:1993 FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
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