MIL-I-83294 Base Document:1971
Withdrawn
Withdrawn
Installation Requirement, Aircraft Propulsion Systems, General Specification for (No S/S Document)
Available format(s)
PDF
Language(s)
English
Published date
04-05-1971
Publisher
Withdrawn date
07-23-2013
US$20.00
Excluding Tax where applicable
General requirements for aircraft propulsion systems installation.
| DocumentType |
Standard
|
| Pages |
44
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
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| MIL-F-87154 Base Document:1980 | FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
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| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
| MIL-E-22285 Base Document:1959 | Extinguishing System, Fire, Aircraft, High-Rate Discharge Type, Installation and Test of |
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| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-H-38360 Revision B:1966 | Hose Assemblies, Tetrafluoroethylene, High-Temperature, High Pressure, 3000 PSI, Hydraulic and Pneumatic (S/S by SAE-AS604 and SAE-AS1339) |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL A 8064 : B NOTICE 1 | ACTUATOR AND ACTUATING SYSTEMS, AIRCRAFT ELECTROMECHANICAL, GENERAL REQUIREMENTS FOR |
| MIL-D-8181 Revision B:1965 | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification for (S/S by SAE-AS8181) |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MIL E 5009 : D | |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| MIL C 27536 : B | COUPLING, CLAMP, GROOVED, V-BAND |
| 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-STD-882 Revision E:2012 | System Safety |
| TT-P-59 Revision E:1975 | PAINT, READY MIXED, INTERNATIONAL ORANGE (NOT FOR RESIDENTIAL USE) (NO S/S DOCUMENT) |
| MIL-STD-203 Revision G:1991 | Aircrew Station Controls and Displays: Location, Arrangement and Actuation of, for Fixed Wing Aircraft |
| MIL S 23586 : E | SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED |
| MIL-STD-250 Revision D:1974 | AIRCREW STATION CONTROLS AND DISPLAYS FOR ROTARY WING AIRCRAFT (NO S/S DOCUMENT) |
| MIL F 38363 : B (3) | FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| 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-C-7413 Revision B:1970 | Coupling, Quick Disconnect, Automatic Shutoff, General Specification for (S/S by SAE-AS7413) |
| MIL-D-17984 Revision A:1956 | Data Presentation Requirements, Installed Performance And Air Induction Systems (No S/S Document) |
| MS33611 Revision A:1983 | TUBE BEND RADII (S/S BY SAE-AS33611) |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MIL C 7958 : A | CONTROL, PUSH PULL, FLEXIBLE AND RIGID |
| MIL H 8795 : D | HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT |
| MIL-A-9482 Base Document:1954 | Anti-Icing Equipment for Aircraft, Heated Surface Type, General Specification for (No S/S Document) |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
| MS33790 Base Document:1958 | BEND DATA, MINIMUM, HYDRAULIC, PNEUMATIC, FUEL AND OIL HOSE (NO S/S DOCUMENT) |
| MS33602 Base Document:1967 | BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR (S/S BY NASM33602) |
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