MS33656 Revision J:1987

Superseded

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FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL

Available format(s)

PDF

Superseded date

18-10-1993

Publisher

US Military Specs/Standards/Handbooks

Committee	FSC 4730
DocumentType	Standard
Pages	3
PublisherName	US Military Specs/Standards/Handbooks
Status	Superseded
SupersededBy	SAE AS 4395 : 2013

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-4O8/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