MIL C 85704 : B
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
CLEANING COMPOUND, TURBINE ENGINE GAS PATH
Available format(s)
PDF
Language(s)
English
Publisher
Superseded date
07-15-1998
Superseded by
US$20.00
Excluding Tax where applicable
Describes a turbine engine gas path cleaning compound used in installed aircraft turbine engines in a starter crank operation.
| Committee |
FSC 6850
|
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| JSGS-87231 Revision A:1995 | Engines, Aircraft, Turbine (S/S by JSSG-2007) |
| SAE AMS1548B | Cleaner, Turbine Engine Gas Path Solvent Emulsion Type |
| SAE AMS2416L | Plating, Nickel-Cadmium Diffused |
| FED-STD-313 Revision D:1996 | Material Safety Data, Transportation Data, and Disposal Data for Hazardous Materials Furnished to Government Activities |
| QQ-A-250-12 Revision F:1982 | Aluminum Alloy 7075, Plate and Sheet (See Notice 3 for Replacement Information) |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-147 Revision E:2008 | Palletized Unit Loads |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| ASTM D 1141 : 1998 : EDT 1 | Standard Practice for the Preparation of Substitute Ocean Water |
| 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 |
| PPP-D-705 Revision E:1994 | Drum, Shipping and Storage: Steel, 16 and 30 Gallon Capacity (Future acquisitions for this material should refer to MIL-DTL-6054) |
| MIL-T-9046 Revision J:1983 | TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE (S/S BY SAE-AMS-T-9046) |
| QQ-A-250-11 Revision F:1982 | Aluminum Alloy 6061, Plate and Sheet (See Notice 3 for Replacement Information) |
| 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 |
| MIL C 22750 : F | COATING, EPOXY, VOC-COMPLIANT |
| MIL-C-81751 Revision B:1972 | Coating, Metallic-Ceramic |
| QQ-S-766 Revision D:1988 | Steel, Stainlessand Heat Resisting, Alloys, Plate, Sheetand Strip (S/S By ASTM-A240, ASTM-A666,and ASTM-A693) |
| ASTM D 93 : 2016-07 | TEST METHODS FOR FLASH POINT BY PENSKY-MARTENS CLOSED CUP TESTER |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| PPP-D-729 Revision E:1977 | Drums, Shipping and Storage, Steel, 55-Gallon (208 Liters) |
| TT-L-32 Revision A:1969 | Lacquer, Cellulose Nitrate, Gloss, for Aircraft use (S/S by A-A-3165) |
| QQ-A-250-5 Revision F:1971 | Aluminum Alloy Alclad 2024, Plate and Sheet (See Notice 5 for Replacement Information) |
| PPP-P-704 Revision E:1981 | Pails, Metal: (Shipping, Steel, 1 through 12 Gallons) |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
| MIL-C-83286 Revision B:1973 | Coating, Urethane, Aliphatic Isocyanate, for Aerospace Applications (S/S by MIL-C-85285 S/S by MIL-PRF-85285) |
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