MIL-H-8775 Revision D:1976

Superseded

View Superseded by

HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR

Available format(s)

PDF

Superseded date

01-07-1998

Publisher

US Military Specs/Standards/Handbooks

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Status	Superseded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	SAE AS 8775 : 1998

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 AS 838 : 2013	AIRCRAFT HYDRAULIC STARTER/PUMPS
SAE AS 55151 : 2001	PUMP, HYDRAULIC, RAM, HAND DRIVEN
SAE AS 25427 : 2015	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 AS 4251 : 2013	COUPLING ASSEMBLIES, NON-LOCKING PROBE STYLE, SELF-ALIGNING, SELF-SEALING DISCONNECTS
SAE AS 7997:1999	MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR
MIL-R-5520 Revision C:1964	RESERVOIRS, AIRCRAFT, HYDRAULIC, NON-SEPARATED TYPE
SAE AS 6026 : 2013	CONTROL UNIT, PRESSURE GENERATING, MANUALLY OPERATED, AIRCRAFT HYDRAULIC BRAKE SYSTEM
SAE AS 1896 : 2013	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 AIR 4543 : 2017	AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED
SAE AS 5994A:2000(S2013)	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-4O8/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