SAE ARP 1755 : 2000
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
EFFECT OF CLEANING AGENTS ON AIRCRAFT ENGINE MATERIALS, STOCK LOSS TEST METHOD
Available format(s)
Hardcopy , PDF
Superseded date
10-11-2023
Superseded by
Language(s)
English
Published date
01-01-2000
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.This ARP covers the determination of the stock loss caused by use of chemical cleaning agents for aircraft turbine engine materials.
| DocumentType |
Standard
|
| Pages |
23
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| 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 |
| SAE AMS1551B:2008(S2023) | Cleaner, Turbine Engine Gas Path Aqueous Type |
| 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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