MS33514 Revision G:1990
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG)
Available format(s)
PDF
Superseded date
16-08-1998
Publisher
DevelopmentNote |
Supersedes NAS 1214. (04/2005)
|
DocumentType |
Standard
|
Pages |
4
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
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MIL-HDBK-1655 Base Document:1997 | CLASSIFICATION OF DEFECTS OF FLARELESS AND BEAM SEAL FITTINGS |
MIL-T-27305 Revision C:1987 | TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
SAE AS 1472 : 2013 | HOSE ASSEMBLY, LOW PRESSURE, POTABLE WATER |
SAE AS 4098 : 2013 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HEAVY DUTY, METALLIC REINFORCED, 400 DEGREE F, 5000 PSI HYDRAULIC AND PNEUMATIC |
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MIL F 83798 : B | FITTING, RUBBER HOSE, LIGHTWEIGHT MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
MIL F 8789 : D | FITTING END, ATTACHABLE HYDRAULIC, HIGH PRESSURE HOSE |
MIL-STD-1655 Base Document:1975 | FITTINGS, FLARELESS, CLASSIFICATION OF DEFECTS OF |
MIL-PRF-25675 Revision C:1997 | VALVES, CHECK, MINIATURE, HYDRAULIC, AIRCRAFT AND MISSILE |
MS21907 Revision G:1991 | ELBOW, BULKHEAD UNIVERSAL, 45 DEGREE, FLARELESS TUBE |
MIL-P-8564 Revision D:1970 | PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
MIL-H-38360 Revision B:1966 | HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC |
SAE AS 18802 : 2013 | FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF |
MIL-I-18802 Revision A:1962 | INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
SAE AS 1896 : 2013 | COUPLING ASSEMBLY, SELF-SEALING, ONE SIDE ONLY, HYDRAULIC |
MIL F 83296 : 0 | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC) |
MIL-G-5514 Revision G:1993 | GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR |
MIL T 62410 : LATEST | TUBE ASSEMBLY METAL, SWAGED HYDRAULIC, (M1 TANK) |
SAE AIR 825/2 : 2012 | EFFECTS OF ACUTE ALTITUDE EXPOSURE IN HUMANS: REQUIREMENTS FOR PHYSIOLOGICAL PROTECTION |
MIL-P-85573 Base Document:1983 | POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
MIL F 38363 : B (3) | FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
SAE AS 4897 : 1994 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), LOW PRESSURE, 450 DEGREES F AND FIREPROOF, PROCUREMENT SPECIFICATION FOR |
SAE AS 18280 SUP1 : 2007 | FITTINGS, 24 DEGREES CONE FLARELESS, FLUID CONNECTION, 3000 PSI (SUPPLEMENT 1) |
SAE AS 4444 : 2013 | FITTINGS, 24 DEGREE CONE FLARELESS, FLUID CONNECTION, 5000 PSI |
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MIL J 5513 : C | JOINT, HYDRAULIC SWIVEL |
SAE ARP 4943 : 2008 | GROUND SUPPORT EQUIPMENT HYDRAULIC SYSTEMS, DESIGN AND INSTALLATION, RECOMMENDED PRACTICES FOR |
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