• SAE AMS 1536 : 2008

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

    CLEANER FOR AIRCRAFT COMPONENTS COLD TANK TYPE, SOLVENT-BASE

    Available format(s):  Hardcopy, PDF

    Superseded date:  13-09-2018

    Language(s):  English

    Published date:  01-01-2008

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. TECHNICAL REQUIREMENTS
    4. QUALITY ASSURANCE PROVISIONS
    5. PREPARATION FOR DELIVERY
    6. ACKNOWLEDGMENT
    7. REJECTIONS
    8. NOTES

    Abstract - (Show below) - (Hide below)

    Describes a liquid tank-type cleaner, primarily for removal of greasy soils, carbon or rubber from painted and unpainted aircraft components, such as wheels and landing gear, by immersing in cleaner as supplied, or as solvent diluted. Not suitable for plastic or aircraft windows, due to possibility of crazing.

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

    Committee AMS-J
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

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

    SAE AMS 4049 : 2016 ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD 5.6ZN - 2.5MG - 1.6CU - 0.23CR (ALCLAD 7075; -T6 SHEET - T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED
    SAE AMS 2475H : 2009 PROTECTIVE TREATMENTS, MAGNESIUM ALLOYS
    SAE AMS 4911 : 2014 TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED
    SAE AMS 4376 : 2011(R2018) PLATE, MAGNESIUM ALLOY - 3.0AL - 1.0ZN - 0.20MN (AZ31B-H26) COLD ROLLED AND PARTIALLY ANNEALED
    SAE AMS 4037 : 2014 ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED
    MIL-A-356 Revision A:1946 ASPHALTUM (GILSONITE)
    MIL-C-306 Revision C:1978 CARBON BLACK, POWDERED, DRY
    ASTM D 93 : 2016-07 TEST METHODS FOR FLASH POINT BY PENSKY-MARTENS CLOSED CUP TESTER
    MIL-L-6082 Revision E:1990 LUBRICATING OIL, AIRCRAFT PISTON ENGINE (NONDISPERSANT MINERAL OIL)
    SAE AMS 2470 : 2013 ANODIC TREATMENT OF ALUMINUM ALLOYS, CHROMIC ACID PROCESS
    SAE AMS 5045 : 2015 STEEL, SHEET AND STRIP, 0.25 CARBON, MAXIMUM HARD TEMPER
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