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  • SAE ARP 1755 : 2000

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    EFFECT OF CLEANING AGENTS ON AIRCRAFT ENGINE MATERIALS, STOCK LOSS TEST METHOD

    Available format(s):  Hardcopy, PDF

    Superseded date:  11-10-2023

    Language(s):  English

    Published date:  01-01-2000

    Publisher:  SAE International

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    Abstract - (Show below) - (Hide below)

    This ARP covers the determination of the stock loss caused by use of chemical cleaning agents for aircraft turbine engine materials.

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

    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

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

    SAE AMS 1379 : 2007 COMPOUND, ALKALINE RUST REMOVER, AIRCRAFT TURBINE ENGINE COMPONENTS
    MIL-PRF-32405 Base Document:2013 CLEANER, HAND WIPE, FOR AVIATION AND MISSILE SYSTEMS, METALLIC SUBSTRATES, LOW OR EXEMPT VOC
    SAE AMS 1386 : 2004 COMPOUND, SILICONE RUBBER REMOVER, AIRCRAFT TURBINE ENGINE COMPONENTS, ROOM TEMPERATURE APPLICATIONS
    SAE AMS 1741 : 2015 COMPOUND, ALKALINE DEGREASER, AIRCRAFT TURBINE ENGINE COMPONENTS
    SAE AMS 1383 : 2007 OXIDE CONDITIONER, ALKALINE PERMANGANATE AIRCRAFT TURBINE ENGINE COMPONENTS
    SAE AMS 1382 : 2007 OXIDE REMOVER COMPOUND, ACIDIC AIRCRAFT TURBINE ENGINE COMPONENTS
    SAE AMS 1740 : 2015 COMPOUND, ALKALINE AQUEOUS CLEANER, AIRCRAFT TURBINE ENGINE COMPONENTS
    SAE AMS 1385 : 2004 COMPOUND, HOT CARBON AND PAINT REMOVER AIRCRAFT TURBINE ENGINE COMPONENTS
    SAE AMS 1551 : 2008 CLEANER, TURBINE ENGINE GAS PATH AQUEOUS TYPE
    SAE AMS 1387B : 2004(S2018) REMOVER, ANTI GALLING COMPOUND, AIRCRAFT TURBINE ENGINE COMPONENTS, ROOM TEMPERATURE APPLICATION
    SAE AMS 1380 : 2007 SCALE CONDITIONER, ALKALINE, AIRCRAFT TURBINE ENGINE COMPONENTS
    SAE AMS 1384 : 2007 ACID, INHIBITED PHOSPHORIC AIRCRAFT TURBINE ENGINE COMPONENTS ROOM TEMPERATURE APPLICATION
    MIL C 29602 : 0 CLEANING COMPOUNDS, FOR PARTS WASHERS AND SPRAY CABINETS
    SAE AMS 1378 : 1995 COMPOUND, CARBON SOIL AND PAINT REMOVER, AIRCRAFT TURBINE ENGINE COMPONENTS, ROOM TEMPERATURE APPLICATION
    SAE AMS 1742 : 2015 COMPOUND, ALKALINE SOLVENT CLEANER, AIRCRAFT TURBINE ENGINE COMPONENTS, ROOM TEMPERATURE APPLICATION

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

    SAE AMS 2416 : 2010 PLATING, NICKEL-CADMIUM DIFFUSED
    SAE AMS 5525 : 2012 STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREE F (982 DEGREE C) SOLUTION HEAT TREATED
    SAE AMS 4911 : 2014 TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED
    SAE AMS 6431 : 2017 STEEL, BARS, FORGINGS, AND TUBING, 1.05CR - 0.55NI - 1.0MO - 0.11V (0.45 - 0.50C) (D6AC), VACUUM CONSUMABLE ELECTRODE REMELTED
    SAE AMS 4507 : 2016 COPPER ALLOY (BRASS), SHEET, STRIP, AND PLATE, 70CU - 30ZN, HALF HARD (H02)
    SAE AMS 5382 : 2012 COBALT ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 54CO - 25.5CR - 10.5NI - 7.5A, AS-CAST
    SAE AMS 5504 : 2002 STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 12.5CR (410), ANNEALED
    SAE AMS 5536 : 2012 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 47.5NI - 22CR - 1.5CO - 9.0MO - 0.60W - 18.5FE, SOLUTION HEAT TREATED
    SAE AMS 4037 : 2014 ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED
    SAE AMS 2418 : 2017 PLATING, COPPER
    SAE AMS 5544 : 2014 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 57NI - 19.5CR - 13.5CO - 4.2MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, ANNEALED
    SAE AMS 5537 : 2012 COBALT ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL, AND PLATE, 52CO - 20CR - 10NI - 15W, SOLUTION HEAT TREATED
    SAE AMS 4640 : 2011 ALUMINUM BRONZE, BARS, RODS, SHAPES, TUBES, AND FORGINGS, 81.5CU - 10.0AL - 4.8NI - 3.0FE, DRAWN AND STRESS RELIEVED (HR50) OR TEMPER ANNEALED (TQ50)
    SAE AMS 5613 : 2013 STEEL, CORROSION AND HEAT RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS 12.5CR (SAE 51410) ANNEALED
    SAE AMS 4375 : 2011 SHEET AND PLATE, MAGNESIUM ALLOY - 3.0AL - 1.0ZN - 0.20MN (AZ31B-0) ANNEALED AND RECRYSTALLIZED
    SAE AMS 2406 : 2015 PLATING, CHROMIUM, HARD DEPOSIT
    SAE AMS 4544 H: 2017 NICKEL-COPPER ALLOY, CORROSION RESISTANT, SHEET, STRIP, AND PLATE 67NI - 30CU, ANNEALED
    SAE AMS 2400 : 2013 PLATING, CADMIUM
    SAE AMS 2410 : 2010 PLATING, SILVER, NICKEL STRIKE, HIGH BAKE
    SAE AMS 5596 : 2016 NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL AND PLATE, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED
    SAE AMS 3065 : 2002 COMPOUND, CORROSION PREVENTIVE, THIN FILM, FINGERPRINT REMOVING
    SAE AMS 5040 : 2015 STEEL, SHEET AND STRIP, 0.15 CARBON, MAXIMUM DEEP FORMING GRADE
    SAE AMS 2437 : 2012 COATING, PLASMA SPRAY DEPOSITION
    SAE AMS 5524 : 2014 STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP AND PLATE 18CR - 13NI - 2.5MO (SAE 30316) SOLUTION HEAT TREATED
    SAE AMS 4442 : 2012 MAGNESIUM ALLOY SAND CASTINGS, 3.2 RARE EARTHS - 2.5ZN - 0.70ZR (EZ33A-T5), PRECIPITATION HEAT TREATED
    SAE AMS 5661 : 2012 NICKEL-IRON ALLOY, CORROSION AND HEAT RESISTANT, BARS, FORGINGS, AND RINGS - 42.5NI - 12.5CR - 5.8MO - 2.9TI - 0.015B - 35FE - CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED
    SAE AMS 5508 : 2014 STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 13CR - 2.0NI - 3.0W, ANNEALED
    SAE AMS 4928 : 2016 TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED
    SAE AMS 2470 : 2013 ANODIC TREATMENT OF ALUMINUM ALLOYS, CHROMIC ACID PROCESS
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