MIL-D-19326 Revision H:1990
Current
Current
The latest, up-to-date edition.
Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for
Available format(s)
PDF
Published date
31-08-1990
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.Details requirements for the design and installation of liquid oxygen 70 and 300 psig (483 kPa and 2068 kPa) systems in aircraft.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN
|
| DocumentType |
Standard
|
| Pages |
69
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers the general requirements for the design and installation of liquid oxygen (70 and 300 pounds per square inch gauge) (psig) (483KPa and 2068 kPa) systems in aircraft.
| 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 |
| 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 300 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 |
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.