MIL S 25057 : B
Withdrawn
Withdrawn
SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR
Publisher
Withdrawn date
07-23-2013
Sorry this product is not available in your region.
Outlines requirements for retractable and fixed air inlet screen systems for use with gas turbine engines.
| DocumentType |
Standard
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Withdrawn
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| MIL-I-83294 Base Document:1971 | Installation Requirement, Aircraft Propulsion Systems, General Specification for (No S/S Document) |
| MIL-I-81550 Revision C:1983 | Insulating Compound, Electrical, Embedding, Reversion Resistant Silicone (S/S by SAE-AS81550) |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| TT-P-1757 Revision B:1997 | Primer Coating, ALKYD Base, One Component |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-M-3171 Revision C:1966 | Magnesium Alloy, Processes for Pretreatment and Prevention of Corrosion on (S/S by SAE-AMS-M-3171) |
| TT-E-489 Revision J:1994 | Enamel, Alkyd, Gloss, Low VOC Content (See Notice 2 for Replacement Information) |
| MIL-STD-480 Revision B:1988 | Configuration Control - Engineering Changes, Deviations and Waivers (S/S by MIL-STD-973) |
| MS35649 Revision H:1988 | NUT, PLAIN, HEXAGON, MACHINE SCREW, UNC-2B (S/S BY NASM35649) |
| MIL-D-8181 Revision B:1965 | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification for (S/S by SAE-AS8181) |
| MS9500 Revision A:1969 | BOLT, MACHINED - HEXAGON HEAD, DRILLED, 1 HOLE, FULL SHANK, AMS 5731, .190-32 UNJF-3A (S/S BY SAE-AS9500) |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| AN737 Revision 8:1956 | CLAMP, HOSE, AIRCRAFT (SS/ BY NAS1924) |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| MIL S 8516 : F | SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL-S-8879 Revision C:1991 | Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-STD-1523 Revision A:1984 | AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIEL (FOR AEROSPACE APPLICATIONS) (S/S BY SAE-AS1933 AND SAE-ARP5316) |
| MIL S 23586 : E | SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS (S/S BY ASME-Y14.100, ASME-Y14.24, ASME-Y14.35M, AND ASME-14.34M) |
| MIL-E-38453 Revision A:1971 | Environmental Control, Environmental Protection, and Engine Bleed Air Systems, Aircraft, General Specification for (S/S by MIL-E-87145) |
| MIL-T-5544 Revision C:1991 | THREAD COMPOUND, ANTISEIZE, GRAPHITE-PETROLATUM (S/S BY SAE-AMS2518) |
| MIL C 6021 : H NOTICE 1 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
Summarise
Sorry this product is not available in your region.