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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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Superseded date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
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.| DevelopmentNote |
Supersedes NAS 1214. (04/2005)
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| DocumentType |
Standard
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| Pages |
4
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| SAE AS1248A | Minimum Standard for Gaseous Oxygen Pressure Reducers |
| MIL F 27272 : B | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| 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 AS1472A | Hose Assembly, Low Pressure, Potable Water |
| SAE AS4098A | Hose Assembly, Polytetrafluoroethylene, Heavy Duty, Metallic Reinforced, 400 °F, 5000 psi Hydraulic and Pneumatic |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| 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 AS18802 | Fuel and Oil Lines, Aircraft, Installation of |
| MIL-I-18802 Revision A:1962 | INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
| SAE AS1896A | 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 AS4897 | Hose Assembly, Polytetrafluoroethylene (PTFE), Low Pressure, 450 °F and Fireproof, Procurement Specification for |
| SAE AS 18280 SUP1 : 2007 | FITTINGS, 24 DEGREES CONE FLARELESS, FLUID CONNECTION, 3000 PSI (SUPPLEMENT 1) |
| SAE AS4444 | Fittings, 24° Cone Flareless, Fluid Connection, 5000 psi |
| MS21909 Revision G:1990 | TEE, BULKHEAD AND UNIVERSAL, FLARELESS TUBE |
| 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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