MIL O 27210 : F
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
OXYGEN, AVIATOR'S BREATHING, LIQUID AND GAS
Available format(s)
PDF
Language(s)
English
Publisher
Superseded date
04-04-1997
Superseded by
£13.91
Excluding VAT
Details requirements for two types of aviator's breathing oxygen.
| DocumentType |
Standard
|
| Pages |
16
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-M-87113 Revision A:1993 | MASK, OXYGEN, MBU-10/P |
| MIL H 26385 : E | HOSE, OXYGEN AND PRESSURIZATION, OZONE RESISTANT |
| MIL-A-27420 Base Document:1970 | Air, Liquid, for Breathing Purposes (No S/S Document) |
| ASTM G 74 : 2013 : REDLINE | Standard Test Method for Ignition Sensitivity of Nonmetallic Materials and Components by Gaseous Fluid Impact |
| DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL-O-23678 Revision B:1982 | Oxygen Systems, Portable, High Pressure, Aircraft |
| MIL H 26626 : D | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, OXYGEN |
| MIL-V-21701 Revision B:1969 | Valve, Check, Oxygen Mask, Inlet |
| 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)/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)/13(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)/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 |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL V 7891 : E | VALVE, OXYGEN FILLER, LOW AND PRESSURE |
| MIL-M-19417 Revision D:1992 | Mask Assemblies, Oxygen and Smoke, Full Face |
| DEFSTAN 00-970(PT7)SEC2/SUPP4/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
| MIL R 83178 : A | REGULATOR, OXYGEN, DILUTER DEMAND, AUTOMATIC PRESSURE BREATHING, GENERAL SPECIFICATION FOR |
| MIL-R-81553 Revision B:1992 | Regulator, Chest Mounted, Oxygen, Positive Pressure, CRU-79/P |
| MIL-C-9082 Revision H:1986 | Converter, Oxygen, Aircraft, Liquid to Gaseous, General Specification for (No S/S Document) |
| MIL-C-21049 Revision F:1990 | Coupling Assemblies, Quick Disconnect, Aircraft Liquid Oxygen Systems |
| MIL C 38271 : B | CONNECTOR, OXYGEN MASK TO REGULATOR CRU-60/P |
| DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
| SAE ARP1109B | Dynamic Testing Systems for Oxygen Breathing Equipment |
| DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL-M-27274 Revision E:1993 | Mask, Oxygen MBU-5/P (No S/S Document) |
| MIL V 8057 : F | VALVE, OXYGEN, PRESSURE BUILDUP AND VENT |
| MIL-DTL-7560 Revision D:1997 | Valve Assembly, Oxygen Cylinder, Bailout |
| MIL-M-85522 Revision A:1991 | Monitor, Oxygen, CRU-91/A |
| MIL-STD-1359 Revision B:1987 | CLEANING METHODS AND PROCEDURES FOR BREATHING OXYGEN EQUIPMENT (S/S BY SAE-ARP1176) |
| MIL C 7905 : G | CYLINDERS, STEEL COMPRESSED GAS, NONSHATTERABLE, SEAMLESS 1800 PSI AND 2100 PSI |
| MIL-O-87226 Base Document:1985 | Oxygen Systems, Aircraft, General Specification for (S/S by AFGS-87226) |
| MIL V 7560 : C | VALVE ASSEMBLY, OXYGEN CYLINDER, BAILOUT |
| MIL C 19328 : E | CONVERTER, LIQUID OXYGEN, 5 LITER, MBA-5A |
| MIL-STD-1551 Revision C:1990 | QUALITY CONTROL OF GASEOUS AND LIQUID AVIATOR\'S BREATHING OXYGEN AT AIRCRAFT CONTRACTOR FACILITIES (NO S/S DOCUMENT) |
| DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL-DTL-19328 Revision F:1996 | Converter, Liquid Oxygen, 5 Liter, MB-5A |
| MIL C 83867 : B | CONNECTOR, OXYGEN MASK HOSE NON-EJECTION TYPE |
| MIL-C-19064 Revision B:1964 | CONNECTOR, OXYGEN HOSE TO REGULATOR |
| MIL-V-27296 Revision C:1993 | Valve, Oxygen Mask, Combination Inhalation and Exhalation |
| MIL-V-8965 Revision B:1990 | Valve Core, Oxygen, High Pressure |
| MIL C 19246 : C | CONNECTOR, OXYGEN MASK HOSE, TYPE MC-3A |
| MIL-PRF-8622 Revision C:1997 | Valve, High-Pressure, Oxygen-Cylinder, Automatic Opening |
| MIL V 9050 : E (1) | VALVE, OXYGEN, PRESSURE RELIEF, AIRCRAFT |
| MIL STD 862 : 0 | TEST PROCEDURES FOR RECEIVING INSPECTION OF AIRCRAFT LIQUID OXYGEN EQUIPMENT |
| MIL-E-18927 Revision E:1983 | Environmental Control Systems, Aircraft, General Requirements for |
| MIL-D-19326 Revision H:1990 | Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for |
| MIL V 9439 : D | VALVE, OXYGEN, CYLINDER, HIGH PRESSURE |
| MIL-R-25410 Revision G:1991 | Regulators, Oxygen, Diluter-Demand, Automatic-Pressure Breathing |
| MIL-V-18318 Revision B:1966 | VALVE, PRESSURE REGULATING, OXYGEN SYSTEM |
| MIL-A-27471 Revision C:1993 | Adapter, Pressure-Reducer, In-Line DAPTER, CRU-43/A (No S/S Document) |
| MIL H 87961 : NOTICE 2 | HOSE AND HOSE ASSEMBLIES, AIR DUCT, AIR BREATHING, OXYGEN SYSTEM GENERAL SPECIFICATION FOR |
| MIL C 25666 : E (1) | CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
| MIL V 25961 : F | VALVE, FILL-BUILDUP-VENT, LIQUID OXYGEN CONVERTER, CRU-5O/A |
| MIL V 8622 : B | VALVE, HIGH-PRESSURE, OXYGEN-CYLINDER AUTOMATIC OPENING |
| MIL-DTL-25666 Revision F:1995 | Converter, Liquid Oxygen, Capacitance Type Gauging, General Specification for |
| ASTM F 307 : 2013 : REDLINE | Standard Practice for Sampling Pressurized Gas for Gas Analysis |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-101 Revision C:2014 | Color Code for Pipelines and for Compressed Gas Cylinders |
| MIL-STD-1411 Revision B:2010 | Inspection and Maintenance of Compressed Gas Cylinders |
| MIL V 2/39 : B | VALVE CYLINDER GAS OXYGEN OUTLET 541 |
| MIL-STD-1564 Revision A:1975 | Procedure for Calibration and Analysis of Trace Contaminants in Aviator\'s Breathing Oxygen by Infrared Spectroscopy (S/S by CGA-G4.3) |
| MIL-C-83690 Base Document:1969 | Cylinder, Sampling (No S/S Document) |
| MIL S 27626 : F | SAMPLER, CRYOGENIC LIQUID |
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Excluding VAT
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