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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Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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Superseded date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Superseded by

SAE AS 4395 : 2013

€17.95
Excluding VAT

Committee
FSC 4730
DocumentType
Standard
Pages
3
PublisherName
US Military Specs/Standards/Handbooks
Status
Superseded
SupersededBy

SAE AS 1248 : 2012 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 AS 1472 : 2013 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 AS 1896 : 2013 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 AS 6302 : 2016 TRANSMITTER, PRESSURE, FUEL, 0-600 PSI
MIL-F-27656 Revision C:1987 Filter Unit, Fluid, Pressure, MXU-408/M, Absolute, 5 Micron, Hydraulic
SAE AS 18802 : 2013 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 AS 4897 : 1994 HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), LOW PRESSURE, 450 DEGREES 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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