MS33656 Revision J:1987
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 FLARED TUBE CONNECTION AND GASKET SEAL
Available format(s)
PDF
Superseded date
18-10-1993
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.| Committee |
FSC 4730
|
| DocumentType |
Standard
|
| Pages |
3
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
|
| SupersededBy |
| SAE AS1248A | Minimum Standard for Gaseous Oxygen Pressure Reducers |
| MIL-T-5842 Revision B:1985 | TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
| MIL-P-81655 Base Document:1970 | PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
| MIL F 27272 : B | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL H 26626 : D | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, OXYGEN |
| MIL-P-9388 Revision B:1986 | PUMP, PRESSURE, OIL FREE AIR TYPE MA-2 |
| MIL-T-5483 Revision D:1964 | TRANSMITTER, PRESSURE, SYNCHRO AIRCRAFT 165 DEGREE MOVEMENT |
| MIL-T-27305 Revision C:1987 | TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
| MIL-C-7135 Revision F:1967 | Compressor, Pneumatic, 3,000 PSI -- 2 SCFM Aero 2A (*), Aero 2A-1 (*), Aero 2B (*), and Aero 2B-1 (*) |
| SAE AS1472A | Hose Assembly, Low Pressure, Potable Water |
| MIL P 83207 : B | PITOT STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| 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-H-25475 Revision B:1971 | HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR |
| MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| MIL-STD-1655 Base Document:1975 | FITTINGS, FLARELESS, CLASSIFICATION OF DEFECTS OF |
| MIL-C-7413 Revision B:1970 | COUPLING, QUICK DISCONNECT, AUTOMATIC SHUTOFF, GENERAL SPECIFICATION FOR |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL-G-23337 Base Document:1962 | GAGE - PRESSURE, DIAL INDICATING |
| MIL-T-26017 Revision C:1972 | TEST STAND, HYDRAULIC SYSTEM COMPONENTS, TYPE MK-3A (STAND, TEST, AIRCRAFT HYDRAULIC SYSTEM, ELECTRIC MOTOR DRIVEN, TYPE MK-3A) |
| MIL-P-8564 Revision D:1970 | PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
| MIL-C-25973 Revision B:1971 | CONVERTER, LIQUID OXYGEN, GCU-12A/A |
| MIL H 38390 : C | HOSE ASSEMBLY, TETRAFLUOROETHYLENE PNEUMATIC, HIGH PRESSURE |
| MIL-H-38360 Revision B:1966 | HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC |
| MIL-I-18802 Revision A:1962 | INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
| MIL-DTL-25666-3 Base Document:1995 | CONVERTER, LIQUID OXYGEN GCU-10/A |
| MIL-I-85487 Base Document:1981 | IGNITER, ROCKET MOTOR, MARK 297 MOD 1 |
| MIL F 83296 : 0 | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC) |
| MIL V 87223 : 0 | VALVE, PRESSURE, ANTI-G SUIT, MXU-804/A AND MXU-805/A |
| MIL-G-5514 Revision G:1993 | GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR |
| MIL C 52716 : A NOTICE 1 | COMPRESSOR AIR, RECIPROCATING ELECTRIC MOTOR DRIVEN 4 CFM 3100 PSIG (NOMINAL) |
| MIL-F-5509 Revision D:1978 | FITTING, FLARED TUBE, FLUID CONNECTION |
| MIL-R-47321 Base Document:1987 | REGULATOR, PRESSURE |
| MIL-A-47309 Revision A:1991 | AMPLIFIER, PNEUMATIC |
| MIL-O-87226 Base Document:1985 | OXYGEN SYSTEMS, AIRCRAFT |
| MIL H 26633 : C | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, OXYGEN |
| AN919 Revision 9:1983 | REDUCER - EXTERNAL THREAD FLARED TUBE |
| SAE AS1896A | Coupling Assembly, Self-Sealing, One Side Only, Hydraulic |
| MIL-P-25632 Revision B:1960 | PITOT STATIC TUBE, ELECTRICALLY HEATED, TEMPERATURE CONTROLLED, 115 VOLT, 4OO HZ, TYPE MA-1 |
| MIL-C-85247 Base Document:1982 | COMPUTER, AIR DATA CP-1005A/A |
| MIL-DTL-25666-4 Base Document:1971 | Converter, Liquid Oxygen, GCU-12A/A |
| SAE AS6302A | Transmitter, Pressure, Fuel, 0-600 psi |
| MIL-F-27656 Revision C:1987 | Filter Unit, Fluid, Pressure, MXU-408/M, Absolute, 5 Micron, Hydraulic |
| SAE AS18802 | Fuel and Oil Lines, Aircraft, Installation of |
| MIL-E-24572 Revision B:1992 | EXTINGUISHER, FIRE, BROMOTRIFLUOROMETHANE (HALON 13O1) SYSTEMS (FIXED PIPE, PNEUMATICALLY ACTUATED, NAVAL SHIPBOARD USE) |
| MIL-P-9389 Revision A:1987 | PUMP PRESSURE, OIL AND FREE AIR, TYPE MA AND 3 |
| MIL P 83206 : B | PITOT STATIC TUBE, L SHAPED, COMPENSATED, GENERAL SPECIFICATION FOR |
| SAE AIR 825/2 : 2012 | EFFECTS OF ACUTE ALTITUDE EXPOSURE IN HUMANS: REQUIREMENTS FOR PHYSIOLOGICAL PROTECTION |
| MIL V 87255 : 0 | VALVE, PRESSURE, ANTI-G SUIT, HIGH FLOW |
| MIL-P-85573 Base Document:1983 | POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
| MIL-E-18927 Revision E:1983 | ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| SAE AS4897 | Hose Assembly, Polytetrafluoroethylene (PTFE), Low Pressure, 450 °F and Fireproof, Procurement Specification for |
| MIL-D-19326 Revision H:1990 | Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for |
| MIL-F-8615 Revision D:1976 | FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
| MIL S 8932 : A | SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
| MIL H 26666 : D (1) | HOSE ASSEMBLY, PNEUMATIC, HIGH PRESSURE |
| MIL J 5513 : C | JOINT, HYDRAULIC SWIVEL |
| MIL-T-6302 Revision B:1964 | TRANSMITTER, PRESSURE, FUEL 0-600 PSI |
| MIL-P-38136 Revision A:1969 | PITOT STATIC TUBE COMPENSATED TRU 62/A |
| MIL-A-83039 Revision B:1971 | AIR CONDITIONER A/M32C-10A AIR CYCLE FOR AIRCRAFT GROUND SUPPORT |
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