• MIL-D-19326 Revision H:1990

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    DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR

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    Abstract - (Show below) - (Hide below)

    Details requirements for the design and installation of liquid oxygen 70 and 300 psig (483 kPa and 2068 kPa) systems in aircraft.

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    Committee FSC 1660
    Development Note INACTIVE FOR NEW DESIGN
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Current

    Standards Referenced By This Book - (Show below) - (Hide below)

    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)/17(2016) : 2016 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)/13(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)/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)/10(2013) : 2013 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
    STANAG 7056 : 0 FUNCTIONAL REQUIREMENTS FOR PHYSIOLOGICAL PROTECTION DURING HIGH ALTITUDE PARACHUTING OPERATIONS
    DEFSTAN 00-970(PT13)/2(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
    MIL-O-87226 Base Document:1985 OXYGEN SYSTEMS, AIRCRAFT
    AIR825/5A : 2003(R 2018) LIQUID OXYGEN SYSTEMS
    MIL STD 1288 : NOTICE 4 AIRCREW PROTECTION REQUIREMENTS NONNUCLEAR WEAPONS THREAT
    MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    JSSG-2010-10 Base Document:1998 Crew Systems Oxygen Systems Handbook
    MIL C 25666 : E (1) CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR
    MIL-DTL-25666 Revision F:1995 CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL-E-87235 Base Document:1985 EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503
    MS22061 Revision D:1982 Oxygen System, Portable, 96 CU Inch High Pressure, Aircraft
    MIL-STD-1359 Revision B:1987 CLEANING METHODS AND PROCEDURES FOR BREATHING OXYGEN EQUIPMENT
    MIL T 38170 : F TANK, MOBILE STORAGE, LIQUID OXYGEN TMU 27/M
    MIL D 26392 : C DUMMY CONVERTERS, LIQUID OXYGEN INDICATOR SYSTEM 10 LITER CRU-23/A AND 25 LITER CRU-24/A
    MS22062 Revision F:1991 Regulator, Oxygen, Diluter Demand, Automatic, Pressure Breathing
    MIL-STD-970 Base Document:1987 STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF
    MS22068 Revision E:1990 Coupling Assemblies, Quick Disconnect, Aircraft Liquid Oxygen Systems
    MIL-D-26393 Revision B:1980 DUMMY CONVERTER, LIQUID OXYGEN INDICATOR SYSTEM, 25 LITER, CRU-24/A
    MIL G 27617 : E GREASE, AIRCRAFT AND INSTRUMENT, FUEL AND OXIDIZER RESISTANT
    MS22055 Revision F:1994 Hose Assemblies-Oxygen Breathing, Connector to Regulator
    MIL O 27210 : F OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS
    MIL-R-25410 Revision G:1991 REGULATORS, OXYGEN, DILUTER-DEMAND AUTOMATIC-PRESSURE BREATHING
    MIL L 25567 : D LEAK DETECTION COMPOUND, OXYGEN SYSTEMS (METRIC)
    DOD STD 100 : C NOTICE 6 ENGINEERING DRAWING PRACTICES
    MIL-H-22343 Revision A:1968 Hose Assemblies, Metal, Liquid Oxygen
    AN929 Revision 14:2017 CAP INSERT, ASSEMBLY, PRESSURE SEAL, FLARED TUBE FITTING
    MS33739 Revision G:1987 AIRCRAFT MARKINGS, SERVICING AND PRECAUTIONING (ASG)
    MIL-V-25513 Revision F:1994 VALVE, CHECK, FOR 3OO PSI LIQUID OXYGEN CONVERTER SYSTEMS, TYPE MH-1
    MIL R 83178 : A REGULATOR, OXYGEN, DILUTER DEMAND, AUTOMATIC PRESSURE BREATHING, GENERAL SPECIFICATION FOR
    MIL-O-27335 Revision B:1986 OXYGEN SYSTEM, SURVIVAL CONTAINER AND OXYGEN KIT, GENERAL SPECIFICATION FOR
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MIL-T-8506 Revision A:1966 TUBING, STEEL, CORROSION-RESISTANT (304) ANNEALED SEAMLESS AND WELDED
    MIL V 7908 : C (2) VALVE, CHECK, AIRCRAFT LOW PRESSURE OXYGEN SYSTEMS
    AND10104 : REV 5 TUBING, STEEL, CORROSION RESISTANT, ROUND, STANDARD DIMENSIONS FOR
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    MS33656 Revision J:1987 FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
    MIL-A-23121 Revision C:1970 AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR
    MIL-I-81388 Revision A:1971 INDICATOR REPEATERS, LIQUID OXYGEN QUANTITY
    MIL C 25666 : E (1) CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR
    MIL S 8805/3 : H SWITCH, PUSH, 10 AMPERES AND LOW LEVEL, DUST-TIGHT
    MIL C 25516 : D CONNECTOR, ELECTRICAL, MINIATURE, COAXIAL, ENVIRONMENT RESISTANT TYPE, GENERAL SPECIFICATION FOR
    MIL V 25962 : C VALVE, LIQUID OXYGEN DRAIN
    SAE AMS 4071 : 2017 ALUMINUM ALLOY, DRAWN, ROUND, SEAMLESS HYDRAULIC TUBING, 2.5MG - 0.25CR (5052-O), ANNEALED
    MS33583 Revision C:1993 TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR
    MIL-STD-203 Revision G:1991 AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT
    MIL H 81581/5 : A HOSE ASSEMBLY, BREATHING OXYGEN, LOW PRESSURE, CONNECTOR TO REGULATOR
    MIL-S-81018 Revision C:1980
    MIL-I-25645 Revision D:1970 INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR
    MS90457 Revision A:1981 HOSE ASSY METAL LIQUID OXYGEN
    MS22032 Revision B:1966 Recharger Assembly, Portable Oxygen (ASG)
    MS33584 Revision C:1990 TUBING END, STANDARD DIMENSIONS FOR FLARED
    MIL C 19328 : E CONVERTER, LIQUID OXYGEN, 5 LITER, MBA-5A
    MS33611 Revision A:1983 TUBE BEND RADII
    MS90341 Revision B:1985 MOUNTING BRACKET CONFIGURATION MATING PORTION FOR 5 AND 10 LITER LIQUID OXYGEN CONVERTERS
    MIL-I-81387 Revision A:1971 INDICATOR, LIQUID OXYGEN QUANTITY
    MIL H 87961 : NOTICE 2 HOSE AND HOSE ASSEMBLIES, AIR DUCT, AIR BREATHING, OXYGEN SYSTEM GENERAL SPECIFICATION FOR
    MS27599 Base Document:1988 REGULATOR, OXYGEN, DILUTER DEMAND
    MIL V 9050 : E (1) VALVE, OXYGEN, PRESSURE RELIEF, AIRCRAFT
    MIL-STD-1247 Revision D:2009 MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS
    MIL-T-27730 Revision A:1964 TAPE, ANTISEIZE, POLYTETRAFLUOROETHYLENE, WITH DISPENSER
    MIL-B-5087 Revision B:1964 BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
    MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
    MIL H 26626 : D HOSE ASSEMBLY, TETRAFLUOROETHYLENE, OXYGEN
    MS22059 Revision D:1982 OXYGEN SYSTEM, PORTABLE, 295 CU. IN HIGH PRESSURE AIRCRAFT
    MIL-R-81553 Revision B:1992 REGULATOR, CHEST MOUNTED, OXYGEN, POSITIVE PRESSURE, CRU-79/P
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