MIL-S-38399 Revision A:1975
Withdrawn
Withdrawn
Starter, Pneumatic, Aircraft Engine General Specification For (No S/S Document)
Available format(s)
PDF
Published date
02-14-1975
Publisher
Withdrawn date
11-24-2014
US$20.00
Excluding Tax where applicable
Specifies pneumatic starters for aeronautical gas turbine engines.
| DevelopmentNote |
A NOTICE 1 - Notice of Inactivation for New Design. (05/2000) A NOTICE 2 - Notice of Validation but remains Inactive for New Design. (11/2008) A NOTICE 3 - Notice of Cancellation without Replacement. (12/2014)
|
| DocumentType |
Standard
|
| Pages |
52
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This specification covers the general requirements for pneumatic starters for aeronautical gas turbine engines.
| MIL-I-81550 Revision C:1983 | Insulating Compound, Electrical, Embedding, Reversion Resistant Silicone (S/S by SAE-AS81550) |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540) |
| MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| MIL-I-8500 Revision D:1980 | Interchangeability and Replaceability of Component Parts for Aerospace Vehicles |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL-P-7105 Revision B:1965 | PIPE THREADS, TAPER, AERONAUTICAL NATIONAL FORM, SYMBOL ANPT, GENERAL REQUIREMENTS FOR (S/S BY SAE-AS71051) |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-STD-480 Revision B:1988 | Configuration Control - Engineering Changes, Deviations and Waivers (S/S by MIL-STD-973) |
| MIL I 6866 : B | INSPECTION, PENETRANT METHOD OF |
| MIL STD 470 : B | MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MIL-STD-875 Revision A:1974 | TYPE DESIGNATION SYSTEM FOR AERONAUTICAL AND SUPPORT EQUIPMENT (S/S BY MIL-STD-1812) |
| MIL-T-5021 Revision D:1969 | TEST, AIRCRAFT AND MISSILE WELDING OPERATORS QUALIFICATION (SEE MIL-STD 1595) |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| MIL-STD-453 Revision C:1984 | Inspection, Radiographic (S/S By ASTM-E1742) |
| MS33588 Revision E:1984 | Nuts, Self-Locking, Aircraft, Reliability and Maintainability Usage Requirements for (S/Sby NASM33588) |
| MS20995 Revision E:1974 | WIRE, SAFETY OR LOCK (S/S BY NASM20995) |
| MIL S 8516 : F | SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED |
| MIL-E-5007 Revision D:1973 | Engine, Aircraft, Turbojet and Turbofan, General Specification for |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL-I-6868 Revision E:1976 | Inspection Process, Magnetic Particle (S/S by MIL-STD-1949) |
| 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-STD-490 Revision A:1985 | SpecificationPractices (S/S by MIL-STD-961) |
| MIL C 8188 : C | CORROSION PREVENTIVE OIL, GAS TURBINE ENGINE, AIRCRAFT SYNTHETIC BASE |
| MIL C 6021 : H NOTICE 1 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| MIL-E-7080 Revision B:1962 | Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080) |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
Summarise
US$20.00
Excluding Tax where applicable