FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR

Amended by

MIL-DTL-8815 Revision D Notice 1 - Validation:2019

Available format(s)

PDF

Superseded date

12-02-2014

Publisher

US Military Specs/Standards/Handbooks

Covers hydraulic line filter assemblies and elements which retain all particles larger than 15 microns and 5 microns.

Committee	FSC 1650
DocumentType	Standard
Pages	47
ProductNote	NEW CHILD NOT 1 2019 IS NOW ADDED.
PublisherName	US Military Specs/Standards/Handbooks
Status	Superseded

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
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
BS ISO 14085-3:2015	Aerospace series. Hydraulic filter elements. Test methods Filtration efficiency and retention capacity
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
MIL H 27267 : B	HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE
DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F)
SAE MA 1975 : 2015	HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 135 DEGREE C, STANDARD DUTY, 28000/21000 KPA, HYDRAULIC, AIRCRAFT SYSTEMS
DEFSTAN 00-970(PT0)/9(2012) : 2012	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
MIL H 25579 : E	HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
DEFSTAN 00-970(PT0)/17(2016) : 2016	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)/11(2013) : 2013	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)/13(2014) : 2014	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/15(2015) : 2015	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)/16(2015) : 2015	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
DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
SAE AIR 4543/1A : 2017	AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED
MIL-H-8891 Revision A:1978	HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR
MIL-DTL-5513 Revision D:2012	SWIVEL JOINT, HYDRAULIC
MIL-P-24423 Base Document:1970	PROPULSION AND AUXILIARY CONTROL CONSOLES AND ASSOCIATED CONTROL AND INSTRUMENTATION EQUIPMENT, NAVAL SHIPBOARD USE, BASIC DESIGN REQUIREMENTS
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-DTL-8815-32 Base Document:2010	FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3000 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F, H-60 AIRCRAFT
MIL-P-19692 Revision E:1994	PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR
MIL-P-5994 Revision D:1972	PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR
MIL-V-24272 Revision B:1985	Valve Manifold, High-Pressure Gas Reducing
MIL F 83860 : C	FILTER ELEMENTS, NONCLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 MICRON ABSOLUTE, TYPE II, SYSTEMS, GENERAL SPECIFICATION FOR
DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
MIL-H-8890 Base Document:1961	HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG]
DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
ISO 14085-3:2015	Aerospace series Hydraulic filter elements Test methods Part 3: Filtration efficiency and retention capacity
SAE AS 1975 : 2016	Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems
SAE AS 5994A:2000(S2013)	PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY
MIL-H-38360 Revision B:1966	HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC
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
MIL F 83296 : 0	FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC)
SAE AS 7997:1999	MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR
SAE AS 19692 : 2016	Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump
SAE AS 4388 : 2013	HOSE ASSEMBLY PTFE HEAVY DUTY, -65 TO 400 DEGREES F (-55 TO 204 DEGREES C) 8000 PSI (56000 KPA) HYDRAULIC AND PNEUMATIC
SAE AS 2078 : 2015	TEST METHODS, HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE (PTFE)
SAE AS 838 : 2013	AIRCRAFT HYDRAULIC STARTER/PUMPS
SAE AIR 1922 : 2017	AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE
SAE ARP 4386 : 2017	TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES
13/30271035 DC : 0	BS ISO 14085-3 - AEROSPACE SERIES - HYDRAULIC FILTER ELEMENTS - TEST METHODS - PART 3: FILTRATION EFFICIENCY AND RETENTION CAPACITY
JSSG-2009 Revision A:2013	Air Vehicle Subsystems
DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT
SAE ARP 5454 : 2014	MULTI-PASS METHOD FOR EVALUATING FILTRATION PERFORMANCE OF FINE LUBE FILTER ELEMENTS UTILIZED IN AEROSPACE POWER AND PROPULSION LUBRICATION SYSTEMS
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
MIL V 25675 : B	VALVE, CHECK, MINIATURE, HYDRAULIC, AIRCRAFT AND MISSILE
SAE AS 595 : 2015	AEROSPACE - CIVIL TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED, HYDRAULIC PUMP
SAE MA 2007A : 2015	HOSE ASSEMBLY, TETRAFLUOROETHYLENE, LIGHTWEIGHT, 204 DEGREE C, 21000 KPA HYDRAULIC, METRIC
SAE J 2312 : 2013	AUTOMATIC TRANSMISSION INTAKE FILTER TEST PROCEDURE
MIL H 85800 : 0	HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID FIBER REINFORCED, 5000 & 8000 PSI, GENERAL SPECIFICATION FOR
MIL H 83298 : A	HOSE, TETRAFLUOROETHYLENE, HIGH TEMPERATURE, HIGH PRESSURE (3000 PSI) HYDRAULIC AND PNEUMATIC
DOD-STD-35-41 Revision A:1979	AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, FILTER, MECHANICAL LIQUID GAS/AIR
MIL J 5513 : C	JOINT, HYDRAULIC SWIVEL
MIL-DTL-8815-33 Base Document:2011	FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3500 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F, AVIATION GROUND POWER UNIT (AGPU)
SAE AIR 887 : 2013	LIQUID FILTER RATINGS, PARAMETERS AND TESTS
SAE ARP 4925 : 2014	AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS
SAE ARP 4943 : 2008	GROUND SUPPORT EQUIPMENT HYDRAULIC SYSTEMS, DESIGN AND INSTALLATION, RECOMMENDED PRACTICES FOR
SAE AIR 1666 : 2014	PERFORMANCE TESTING OF LUBRICANT FILTER ELEMENTS UTILIZED IN AIRCRAFT POWER AND PROPULSION LUBRICATION SYSTEMS
SAE AIR 4543 : 2017	AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED
SAE ARP 4752 : 2013	AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS
SAE J 2333 : 2013	SHIP SYSTEMS AND EQUIPMENT - HYDRAULIC SYSTEMS - FILTER SELECTION PARAMETERS

ANSI Y14.5 : 1973	DIMENSIONING AND TOLERANCING FOR ENGINEERING DRAWINGS
MIL-B-117G:1993	BAG, SLEEVE AND TUBING
MIL-STD-129 Revision R:2014	Military Marking for Shipment and Storage
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
PPP-B-636 Revision J:1981	BOX, SHIPPING, FIBERBOARD
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
PPP-B-566 Revision E:1974	BOX, FOLDING, PAPERBOARD
NAS1638:2011	CLEANLINESS REQUIREMENTS OF PARTS USED IN HYDRAULIC SYSTEMS
AN929 Revision 14:2017	CAP INSERT, ASSEMBLY, PRESSURE SEAL, FLARED TUBE FITTING
AN815 Revision 10:2015	UNION - FLARED TUBE
PPP-B-676 Revision E:1992	BOXES SET-UP
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-H-8775 Revision D:1976	HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR
MIL-STD-794 Revision E:1982	PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF
MIL-P-116 Revision J:1988	PRESERVATION, METHODS OF
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-C-5501 Revision G:1989	CAP AND PLUG, PROTECTIVE, DUST AND MOISTURE SEAL
MIL-STD-105 Revision E:1989	SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES