SAE AMS 1551 : 2008
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
CLEANER, TURBINE ENGINE GAS PATH AQUEOUS TYPE
Hardcopy , PDF
11-08-2020
English
01-01-2008
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Specifies petroleum distillate-free cleaner in the form of an aqueous-base liquid concentrate or a ready-to-use liquid.
| Committee |
AMS-J
|
| DocumentType |
Standard
|
| Pages |
11
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| SAE AMS2416L | PLATING, NICKEL-CADMIUM DIFFUSED |
| SAE AMS 7273 : 2011 | RUBBER: FLUOROSILICONE (FVMQ) HIGH TEMPERATURE FUEL AND OIL RESISTANT FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
| ASTM D 4192 : 2015 : REDLINE | Standard Test Method for Potassium in Water by Atomic Absorption Spectrophotometry |
| 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 AMS2475G | PROTECTIVE TREATMENTS, MAGNESIUM ALLOYS |
| SAE AMS 4911 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
| SAE AMS 5608 : 2016 | COBALT ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 40CO - 22CR - 22NI - 14.5W - 0.07LA, SOLUTION HEAT TREATED |
| ASTM D 4191 : 2015 : REDLINE | Standard Test Method for Sodium in Water by Atomic Absorption Spectrophotometry |
| ASTM D 1141 : 1998 : EDT 1 | Standard Practice for the Preparation of Substitute Ocean Water |
| SAE AMS 4376 : 2011(R2018) | PLATE, MAGNESIUM ALLOY - 3.0AL - 1.0ZN - 0.20MN (AZ31B-H26) COLD ROLLED AND PARTIALLY ANNEALED |
| SAE AMS7276H | RUBBER: FLUOROCARBON (FKM) HIGH-TEMPERATURE-FLUID RESISTANT LOW COMPRESSION SET FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
| SAE AMS 5504 : 2002 | STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 12.5CR (410), ANNEALED |
| SAE AMS5536N | 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 7267 : 2001 | RINGS, SEALING, SILICONE (VSI) RUBBER, HEAT RESISTANT, LOW COMPRESSION SET, 70-80 |
| SAE AMS 4045 : 2016 | ALUMINUM ALLOY SHEET AND PLATE 5.6ZN - 2.5MG - 1.6CU - 0.23CR 7075: (-T6 SHEET, -T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED |
| 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 |
| ASTM E 70 | TEST METHOD FOR PH OF AQUEOUS SOLUTIONS WITH THE GLASS ELECTRODE |
| SAE AMS5510S | STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP AND PLATE, 18CR - 10.5NI - 0.40TI (SAE 30321) SOLUTION HEAT TREATED |
| SAE AMS 7271 : 2010 | RINGS, SEALING, BUTADIENE-ACRYLONITRILE (NBR) RUBBER FUEL AND LOW TEMPERATURE RESISTANT 60 - 70 |
| MIL-C-81751 Revision B:1972 | Coating, Metallic-Ceramic |
| SAE AMS 4025 : 2014 | ALUMINUM ALLOY, SHEET AND PLATE, 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061-O) ANNEALED |
| ASTM D 93 : 2016-07 | TEST METHODS FOR FLASH POINT BY PENSKY-MARTENS CLOSED CUP TESTER |
| SAE AMS 5046 : 2012 | CARBON STEEL, SHEET, STRIP, AND PLATE, (SAE 1020 AND 1025) |
| SAE ARP 1755 : 2000 | EFFECT OF CLEANING AGENTS ON AIRCRAFT ENGINE MATERIALS, STOCK LOSS TEST METHOD |
| SAE AMS 4916 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
| SAE AMS5040N | Steel, Sheet and Strip 0.15 Carbon, Maximum Deep Forming Grade |
| ASTM E 442 : 1991 | Test Method for Chlorine, Bromine, or Iodine in Organic Compounds by Oxygen Flask Combustion (Withdrawn 1997) |
| SAE AMS2470N | 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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