MS33584 Revision C:1990
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
TUBING END STANDARD DIMENSIONS FOR FLARED (S/S BY SAE-AS4330)
Available format(s)
PDF
Published date
10-12-1990
Publisher
Superseded date
01-12-2001
Superseded by
$33.64
Including GST where applicable
| DocumentType |
Standard
|
| Pages |
3
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-H-25475 Revision B:1971 | Hydraulic Systems, Missile Design, Installation and Tests, General Requirements for (No S/S Document) |
| MIL-H-8891 Revision A:1978 | Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation and Data Requirements for, General Specification for |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| SAE AS18802 | Fuel and Oil Lines, Aircraft, Installation of |
| ASTM F 1949 : 1999 | Standard Specification for Medical Oxygen Delivery Systems for EMS Ground Vehicles |
| MIL-I-18802 Revision A:1962 | Installation of Fuel and Oil Lines, Aircraft (S/S by SAE-AS18802) |
| MIL-T-7081 Revision D:1965 | TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN 6061, AIRCRAFT HYDRAULIC QUAL ITY (S/S BY SAE-AMS-T-7081) |
| MIL-F-45764 Revision C:1990 | Fluid Lines and Fittings for Missiles and Related Ground Equipment: Fabrication and Installation of (No S/S Document) |
| MIL-O-87226 Base Document:1985 | Oxygen Systems, Aircraft, General Specification for (S/S by AFGS-87226) |
| MIL-T-6845 Revision D:1985 | TUBING, STEEL, CORROSION-RESISTANT (S30400), AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION (S/S BY SAE-AMS-T-6845) |
| MIL-T-8808 Revision B:1981 | TUBING, STEEL, CORROSION-RESISTANT (18-8 STABILIZED), AIRCRAFT HYDRAULIC QUALITY (USE SAE-AMS5556 AND SAE-AMS5557) |
| NASA STD 8719.24 : 2011 | NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
| MIL-DTL-19328 Revision F:1996 | Converter, Liquid Oxygen, 5 Liter, MB-5A |
| MIL P 25508 : F | PROPELLANT, OXYGEN |
| MIL-D-9898 Revision C:1986 | Drawing, Tube Bend |
| MIL F 38363 : B (3) | FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| ASTM F 1949 : 1999 : R2007 | Standard Specification for Medical Oxygen Delivery Systems for EMS Ground Vehicles |
| MIL-D-19326 Revision H:1990 | Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for |
| MIL-T-8506 Revision A:1966 | TUBING, STEEL, CORROSION-RESISTANT, (304) ANNEALED, SEAMLESS AND WELDED (S/S BY SAE-AMS-T-8506) |
| ASTM F 1949 : 1999 : R2013 | Standard Specification for Medical Oxygen Delivery Systems for EMS Ground Vehicles (Withdrawn 2022) |
| 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 Gauging, General Specification for |
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