MIL-H-8890 Base Document:1961
Current
Current
The latest, up-to-date edition.
Hydraulic Components, Type III (-65 Degrees to Plus 450 Degrees F) General Specification for (ASG)
Available format(s)
PDF
Published date
01-11-1961
Publisher
£13.91
Excluding VAT
Covers requirements common to hydraulic components conforming to Specification MIL-H-8891.
| DevelopmentNote |
NOTICE 1 - Notice of Inactivation for New Design. NOTICE 2 - Notice of Validation but remains Inactive for New Design. (02/2008)
|
| DocumentType |
Standard
|
| Pages |
23
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers general requirements common to hydraulic components used in type III hydraulic systems (-65 degrees to + 450degrees F) conforming to Specification MIL-H-8891. For types I and II components, see Specification MIL-H-8875.
| SAE AS7997 | Motors, Aircraft Hydraulic, Constant Displacement General Specification For |
| SAE ARP94910 | Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For |
| 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)/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)/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)/13(2014) : 2014 | 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 |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-H-8891 Revision A:1978 | Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation and Data Requirements for, General Specification for |
| MIL-DTL-5513 Revision D:2012 | Swivel Joint, Hydraulic |
| MIL-P-5994 Revision D:1972 | Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery, General Specification for (No S/S Document) |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| MIL-S-8812 Revision D:1975 | Steering System, Aircraft General Requirements for |
| MIL-M-7997 Revision C:1981 | Motor, Aircraft Hydraulic, Constant Displacement General Specification for |
| MIL-P-19692 Revision E:1994 | PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR (S/S BY SAE-AS19692) |
| SAE AS19692B | Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
| MIL-DTL-9490 Revision E:2008 | Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specification for |
| SAE AS94900 | Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For |
| MIL V 25675 : B | VALVE, CHECK, MINIATURE, HYDRAULIC, AIRCRAFT AND MISSILE |
| MIL J 5513 : C | JOINT, HYDRAULIC SWIVEL |
| SAE AS5994A | Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery |
| SAE ARP24E | Determination of Hydraulic Pressure Drop |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540) |
| MIL F 25682 : LATEST | FILTER & FILTER ELEMENT, FLUID PRESSURE, HYDRAULIC, ABSOLUTE, 25 MICRON, MINUS 65 DEG. TO PLUS 450 & PLUS 600 DEG. F |
| MIL-H-8891 Revision A:1978 | Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation and Data Requirements for, General Specification for |
| MIL I 6866 : B | INSPECTION, PENETRANT METHOD OF |
| MIL-D-70327 Base Document:1959 | DRAWINGS, ENGINEERING AND ASSOCIATED LISTS |
| 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-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 T 9107 : LATEST | TEST REPORTS, PREPARATION OF |
| MIL-S-4040 Revision G:2012 | Solenoid, Electrical General Specification for (No S/S Document) |
| 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 F 8815 : D | FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
| MIL-STD-202 Revision H:2015 | Electronic and Electrical Component Parts |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
Summarise
£13.91
Excluding VAT
Please Login or Create an Account so you can add users to your Multi user PDF Later.
Important note : All end users must be registered with an Account prior to user licenses being assigned.
Users cannot be edited or removed once added to your Multi user PDF.