MIL-P-85573 Base Document:1983
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The latest, up-to-date edition.
POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR
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Outlines features of the gas turbine auxiliary power unit.
| DocumentType |
Standard
|
| Pages |
175
|
| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540) |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| DOD STD 100 : C NOTICE 6 | ENGINEERING DRAWING PRACTICES |
| MS14169 Revision C:1980 | Circular Spline and Adapter Details Engine Driven Accessories |
| SAE AS1055D | Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components |
| MIL STD 470 : B | MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MS33656 Revision J:1987 | FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL (S/S BY SAE-AS4395) |
| MS3336 Base Document:1970 | Accessory Drives Aircraft Engine, Reference Chart for |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| MIL-STD-1390 Revision D:1993 | LEVEL OF REPAIR ANALYSIS (LORA) (S/S BY MIL-PRF-49506) |
| MS33537 Revision E:1974 | INSERT, SCREW THREAD, HELICAL COIL, INCH SERIES, COARSE AND FINE THREAD, STANDARD ASSEMBLY DIMENSIONS FOR (S/S BY NASM33537) |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL-STD-461 Revision G:2015 | Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment |
| MS33587 Revision B:1972 | Transmitter Installation Clearance, Fuel and Oil Pressure |
| MIL-STD-1523 Revision A:1984 | AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIEL (FOR AEROSPACE APPLICATIONS) (S/S BY SAE-AS1933 AND SAE-ARP5316) |
| ANSI N2.1 : 1989 | RADIATION SYMBOL |
| MIL-STD-1472 Revision G:2012 | Human Engineering |
| MS14184 Revision A:1980 | Nonmetallic Shaft-Coupling Details, Engine Driven Accessories |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNTIC INTERFERENCE CHARACTERISTICS (S/S BY MIL-STD-461) |
| SAE AS681K | Gas Turbine Engine Performance Presentation for Computer Programs |
| MIL-STD-1629 Revision A:1980 | PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS (NO S/S DOCUMENT) |
| MS33666 Revision C:1975 | PACKING, PREFORMED - AERONAUTICAL ELASTOMERIC, RANGE OF SIZES (S/S BY SAE-AS568) |
| MS33514 Revision G:1990 | FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (S/S BY SAE-AS33514) |
| MIL-STD-785 Revision B:1980 | RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
| MS33668 Revision B:1975 | PACKING, PREFORMED, ELASTOMERIC, TUBE FITTING, RANGE OF SIZES (S/S BY SAE-AS568) |
| MS21209 Revision E:1978 | INSERT, SCREW THREAD, COARSE AND FINE, SCREW LOCKING, HELICAL COIL, CRES (S/S BY NASM21209) |
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