MIL-H-8775 Revision D:1976
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR
Available format(s)
PDF
Superseded date
01-07-1998
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Covers requirements common to most hydraulic components used in aeronautical hydraulic systems.
| DocumentType |
Standard
|
| Pages |
35
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL C 25427 : A | COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT |
| MIL-V-29592 Base Document:1993 | VALVE, AIR VENT, AUTOMATIC, HYDRAULIC, LOW PRESSURE TYPE II SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL V 81940 : B | VALVE, SAMPLING AND BLEED, HYDRAULIC, TYPE LI SYSTEMS |
| 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 |
| DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL-V-47308 Revision A:1991 | VALVE, SERVO, HYDRAULIC FLOW CONTROL |
| DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL F 83861 : B | FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE, TYPE 1I, SYSTEMS GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| 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)/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 V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| 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 |
| DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL F 83870 : A | FILTER ELEMENT, FLUID PRESSURE, TRANSMISSION, AIRCRAFT DISPOSABLE, 20 MICRON ABSOLUTE |
| MIL-V-19067 Revision A:1957 | VALVE, CHECK, CONTROLLABLE, HYDRAULIC, AIRCRAFT TYPE 11 SYSTEMS |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-R-8931 Revision A:1994 | RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE |
| MIL-P-5994 Revision D:1972 | PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR |
| MIL F 83860 : C | FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 MICRON ABSOLUTE, TYPE II, SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL V 19068 : A | VALVE, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 11 SYSTEMS |
| MIL-F-24666 Base Document:1986 | FILTER ELEMENT, SHIP FUEL SYSTEM PREFILTER, NONCLEANABLE, HIGH EFFICIENCY |
| DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
| SAE AS838A | Aircraft Hydraulic Starter/Pumps |
| SAE AS55151A | Pump, Hydraulic, Ram, Hand Driven |
| SAE AS25427 | Coupling Assembly, Hydraulic, Self-Sealing, Quick Disconnect |
| MIL F 5508 : B | FUSE, AIRCRAFT AUTOMATIC QUANTITY MEASURING HYDRAULIC |
| 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 |
| DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| SAE AS4251 | Coupling Assemblies, Non-Locking Probe Style, Self-Aligning, Self-Sealing Disconnects |
| SAE AS7997 | Motors, Aircraft Hydraulic, Constant Displacement General Specification For |
| MIL-R-5520 Revision C:1964 | RESERVOIRS, AIRCRAFT, HYDRAULIC, NON-SEPARATED TYPE |
| SAE AS6026A | Control Unit, Pressure Generating, Manually Operated, Aircraft Hydraulic Brake System |
| SAE AS1896A | Coupling Assembly, Self-Sealing, One Side Only, Hydraulic |
| MIL-V-19069 Revision B:1986 | Valve, Check, Hydraulic, Aircraft, Type II Systems |
| MIL-P-19692 Revision E:1994 | PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT |
| MIL-T-18232 Revision B:1968 | TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
| MIL A 8897 : A | ACCUMULATORS, HYDRAULIC CYLINDRICAL, 3,000 PSI AIRCRAFT TYPE 11 SYSTEMS |
| MIL A 5503 : E | ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL A 5498 : D | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| MIL F 81836 : A SUPP 1 | FILTER AND DISPOSABLE ELEMENT, FLUID PRESSURE, HYDRAULIC, 3 MICRON ABSOLUTE |
| DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL R 25534 : A NOTICE 1 | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL-F-5504 Revision B:1958 | Filters and Filter Elements, Fluid Pressure, Hydraulic Micronic Type |
| MIL-T-25307 Revision D:1985 | TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1 |
| MIL R 25532 : A | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL J 5513 : C | JOINT, HYDRAULIC SWIVEL |
| MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AIR4543C | Aerospace Hydraulics and Actuation Lessons Learned |
| SAE AS5994A | Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery |
| MS28772 Revision B:1971 | PACKING D, RING, SHOCK STRUT |
| MIL HDBK 5 : G_VOL2 | METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR |
| 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 F 81836 : A SUPP 1 | FILTER AND DISPOSABLE ELEMENT, FLUID PRESSURE, HYDRAULIC, 3 MICRON ABSOLUTE |
| MIL-H-25475 Revision B:1971 | HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL I 6866 : B | INSPECTION, PENETRANT METHOD OF |
| NAS1638:2011 | CLEANLINESS REQUIREMENTS OF PARTS USED IN HYDRAULIC SYSTEMS |
| MS27595 Revision E:2006 | RETAINER, PACKING BACKUP, CONTINUOUS RING, POLYTETRAFLUOROETHYLENE |
| MS33515 Revision J:1973 | FITTING END, STANDARD DIMENSIONS FOR BULKHEAD FLARELESS TUBE CONNECTIONS |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| MS28774 Revision M:2009 | RETAINER, PACKING BACKUP, SINGLE TURN, POLYTETRAFLUOROETHYLENE |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| MS28778 Revision C:1984 | PACKING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS |
| MS28775 Revision E:1984 | PACKING, PREFORMED, HYDRAULIC, PLUS 275 DEG. F. (O RING) |
| MS33656 Revision J:1987 | FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL |
| QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) |
| MS28782 Revision E:2006 | RETAINER, PACKING, BACK-UP, TEFLON |
| MIL C 38999 : J | CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS |
| MIL-T-10727 Revision C:1989 | TIN PLATING, ELECTRODEPOSITED OR HOT-DIPPED FOR FERROUS AND NONFERROUS METALS |
| QQ-S-365 Revision D:1985 | SILVER PLATING, ELECTRODEPOSITED, GENERAL REQUIREMENTS FOR |
| MIL-G-5514 Revision G:1993 | GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR |
| MS20995 Revision E:1974 | WIRE, SAFETY OR LOCK |
| MIL-R-8791 Revision D:1982 | RETAINER, PACKING, HYDRAULIC, AND PNEUMATIC, TETRAFLUOROETHYLENE RESIN |
| MIL H 83282 : C | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537 |
| MIL H 6083 : E | HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
| MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
| MIL-C-83982 Base Document:1974 | COMPOUND, SEALING, FLUID RESISTANT |
| MIL-M-8609 Revision B:1965 | MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL-I-6868 Revision E:1976 | INSPECTION PROCESS, MAGNETIC PARTICLE |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL-S-8879 Revision C:1991 | SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MS21343 Base Document:1971 | BOSS SPACING HYDRAULIC DESIGN STANDARD FOR |
| MS28783 Revision F:2006 | RING, GASKET, BACK-UP, PTFE |
| MIL S 81733 : C | SEALING AND COATING COMPOUND CORROSION INHIBITIVE |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL-STD-490 Revision A:1985 | SPECIFICATION PRACTICES |
| MIL C 5015 : G | CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
| AND10476 : 0002 | WASHER - LIMITATIONS ON USAGE OF LOCK |
| MIL C 26074 : E | COATINGS, ELECTROLESS NICKEL, REQUIREMENTS FOR |
| MIL-C-5501 Revision G:1989 | CAP AND PLUG, PROTECTIVE, DUST AND MOISTURE SEAL |
| QQ-P-416 Revision F:1991 | PLATING, CADMIUM (ELECTRODEPOSITED) |
| MIL-P-83461 Revision B:1980 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C) |
| FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
| MS33514 Revision G:1990 | FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG) |
| MIL G 81322 : E | GREASE, AIRCRAFT, GENERAL PURPOSE, SIDE TEMPERATURE RANGE, NATO CODE NUMBER G-395 |
| MIL-F-27656 Revision C:1987 | Filter Unit, Fluid, Pressure, MXU-408/M, Absolute, 5 Micron, Hydraulic |
| MIL-STD-785 Revision B:1980 | RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
| QQ-N-290 Revision A:1971 | NICKEL PLATING (ELECTRODEPOSITED) |
| MS33547 Revision C:1957 | PIN, SPRING, FUNCTIONAL LIMITATIONS OF (ASG) |
| AN6230 Revision 9:1982 | GASKET "O"-RING HYDRAULIC |
| MIL-HDBK-221 Base Document:1965 | FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES |
| MS21344 Revision A:2016 | FITTING INSTALLATION OF FLARED TUBE STRAIGHT THREADED CONNECTORS DESIGN STANDARD FOR |
| MIL-STD-463 Revision A:1977 | DEFINITION AND SYSTEM OF UNITS, ELECTROMAGNETIC INTERFERENCE TECHNOLOGY |
| MS21209 Revision E:1978 | INSERT SCREW THREAD COARSE AND FINE SCREW LOCKING HELICAL COIL CRES |
| MIL-STD-961 Revision E:2003 | DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT |
Access your standards online with a subscription
Features
-
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.