• Shopping Cart
    There are no items in your cart
We noticed you’re not on the correct regional site. Switch to our AMERICAS site for the best experience.
Dismiss alert
Meet Inform Select. Always-on access to the Standards your organisation relies on. Explore Inform Select

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

£13.91
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

£13.91
Excluding VAT