|
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 |