MIL-P-8564 Revision D:1970
Current
Current
The latest, up-to-date edition.
Pneumatic System Components, Aeronautical, General Specification for
Available format(s)
PDF
Published date
18-11-1970
Publisher
€16.67
Excluding VAT
Covers requirements for pneumatic components used in aircraft systems conforming to MIL-P-5518.
| DevelopmentNote |
D NOTICE 1 - Notice of Inactivation for New Design. D NOTICE 2 - Notice of Validation but remains Inactive for New Design. (02/2008)
|
| DocumentType |
Standard
|
| Pages |
28
|
| ProductNote |
NEW CHILD NOT 3 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers the general requirements for pneumatic components (see 6.2) used in aircraft systems conforming to Specification Mil-P-5518.
| 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)/14(2014) : 2014 | 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)/13(2014) : 2014 | 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)/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 |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-T-25363 Revision D:1973 | Accumulator, Pneumatic, Aircraft, Glass Fiber (S/S by MIL-R-8573) |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| SAE AS1297B | Reducers, Pneumatic Pressure, Missile |
| MIL-S-8812 Revision D:1975 | Steering System, Aircraft General Requirements for |
| MIL-V-19593 Base Document:1956 | VALVE-CONTROL, AIRCRAFT PNEUMATIC 28 VOLT D-C SOLENOID OPERATED (NO S/S DOCUMENT) |
| MIL-D-8804 Revision B:1993 | Deicing System, Pneumatic Boot, Aircraft, General Specification for (S/S by SAE-AS8804) |
| MIL-DTL-9490 Revision E:2008 | Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specification for |
| MIL-R-8573 Revision A:1957 | Reservoir, Air, Nonshatterable Steel |
| SAE AIR4994A | High Pressure Pneumatic Compressors Users Guide For Aerospace Applications |
| MIL R 8572 : 0 | REDUCERS, PNEUMATIC PRESSURE AIRCRAFT |
| SAE ARP1070D | Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility |
| MIL-P-87210 Base Document:1984 | Pneumatic Power Systems, High Pressure (No S/S Document) |
| MIL R 25534 : A NOTICE 1 | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL R 25532 : A | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MS28772 Revision B:1971 | PACKING,PREFORMED (\"D\" RING, SHOCK STRUT) (S/S BY SAE-AS28772) |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540) |
| 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 C 26500 : E | CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE, CIRCULAR, ENVIRONMENT RESISTING, GENERAL SPECIFICATION FOR |
| MS9058 Revision D:1997 | RING BACK UP, BOSS CONNECTION, AMS 3652, AMS 3656, AMS 3660, AMS 3667 (S/S BY SAE-AS9058) |
| MIL I 6866 : B | INSPECTION, PENETRANT METHOD OF |
| MS33515 Revision J:1973 | FITTING END, STANDARD DIMENSIONS FOR BULKHEAD FLARELESS TUBE CONNECTIONS (S/S BY SAE-AS33515) |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| MS28774 Revision M:2009 | Retainer, Packing Backup, Single Turn, Polytetraflouroethylene |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MS28778 Revision C:1984 | PACKING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS (S/S BY SAE-AS28778) |
| MS33656 Revision J:1987 | FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL (S/S BY SAE-AS4395) |
| QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-C-320) |
| MS33566 Revision B:1975 | FITTINGS, INSTALLATION OF FLARELESS TUBE, STRAIGHT-THREADED CONNECTORS (S/S BY SAE-AS33566) |
| MS28782 Revision E:2006 | Retainer, Packing, Back-up, Teflon |
| MIL-T-10727 Revision C:1989 | TIN PLATING: ELECTRODEPOSITED OR HOT-DIPPED, FOR FERROUS AND NONFERROUS METALS (S/S BY ASTM-B545, ASTM-B339) |
| QQ-S-365 Revision D:1985 | SILVER PLATING, ELECTRODEPOSITED, GENERAL REQUIREMENTS FOR (USERS MAY CONSULT ASTM-B700) |
| MIL-G-5514 Revision G:1993 | Gland Design; Packings, Hydraulic, General Requirements for |
| MS20995 Revision E:1974 | WIRE, SAFETY OR LOCK (S/S BY NASM20995) |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL-M-8609 Revision B:1965 | Motor, DC, 28 Volt System, Aircraft, General Specification for |
| MIL-I-6868 Revision E:1976 | Inspection Process, Magnetic Particle (S/S by MIL-STD-1949) |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MS28783 Revision F:2006 | Ring, Gasket, Back-up, PTFE |
| MIL-P-6906 Revision B:1969 | Plates, Identification, Aircraft |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL C 5015 : G | CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR |
| AND10476 : 0002 | WASHER - LIMITATIONS ON USAGE OF LOCK |
| MIL C 26074 : E | COATINGS, ELECTROLESS NICKEL, REQUIREMENTS FOR |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MS33514 Revision G:1990 | FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (S/S BY SAE-AS33514) |
| MIL-G-4343 Revision C:1978 | Grease, Pneumatic System (S/S by SAE-AMS-G-4343) |
| QQ-N-290 Revision A:1971 | NICKEL PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-N-290) |
| MS33547 Revision C:1957 | PINS, SPRING, FUNCTIONAL LIMITATIONS OF (S/S BY NASM33547) |
| AN6230 Revision 9:1982 | GASKET, \"O\" RING HYDRAULIC (S/S BY MS28775) |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
Summarise
Access your standards online with a subscription
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.
Important note : Users cannot be edited or removed once added to your Multi user PDF.