MIL-P-7105 Revision B:1965
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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PIPE THREADS, TAPER, AERONAUTICAL NATIONAL FORM, SYMBOL ANPT, GENERAL REQUIREMENTS FOR (S/S BY SAE-AS71051)
Available format(s)
PDF
Published date
01-06-1965
Publisher
Superseded date
07-16-1999
Superseded by
US$20.00
Excluding Tax where applicable
Specifies aeronautical pipe gages and threads and gaging methods.
| DocumentType |
Standard
|
| Pages |
29
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| 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Superseded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, De-Frosting, De-Icing, Defogging, General Specification For |
| MIL-W-87105-1 Base Document:1977 | WAVEGUIDE ASSEMBLIES (3.5 TO 8.2 GHZ) |
| MIL-S-38399 Revision A:1975 | Starter, Pneumatic, Aircraft Engine General Specification For (No S/S Document) |
| MIL-P-9388 Revision B:1986 | Pump, Pressure, Oil Free Air Type MA-2 (No S/S Document) |
| MIL-C-7135 Revision F:1967 | Compressor, Pneumatic, 3,000 PSI -- 2 SCFM Aero 2A (*), Aero 2A-1 (*), Aero 2B (*), and Aero 2B-1 (*) |
| MIL-M-7255 Revision B:1969 | Manometer, Pressure, Differential and Absolute, Type E-1 (No S/S Document) |
| MIL-T-7305 Revision C:1987 | TRANSMITTER, PRESSURE, TORQUE, TYPE D-5 (NO S/S DOCUMENT) |
| MIL V 27166 : D | VALVE, PRESSURE EQUALIZING, GASEOUS PRODUCTS |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-I-8846 Revision D:1994 | Inserts, Screw-Thread, Helical Coil (S/S by NASM8846) |
| MIL-I-6447 Revision C:1974 | Indicator, True Airspeed, Type M-1A (No S/S Document) |
| MIL-G-25507 Revision B:1991 | Gage, Pressure, Dial Indication, Oxygen 0-2000 PSI, Type MF-2 |
| MIL R 83178 : A | REGULATOR, OXYGEN, DILUTER DEMAND, AUTOMATIC PRESSURE BREATHING, GENERAL SPECIFICATION FOR |
| MIL-I-25091 Revision B:1985 | Indicator, Cabin Air Pressure, Pressurized Aircraft, 1-7/8 Inch Dial, Type MA-2 |
| MIL-R-81553 Revision B:1992 | Regulator, Chest Mounted, Oxygen, Positive Pressure, CRU-79/P |
| MIL-C-9082 Revision H:1986 | Converter, Oxygen, Aircraft, Liquid to Gaseous, General Specification for (No S/S Document) |
| MIL I 38715 : B | INDICATOR, COMBUSTIBLE GAS AND TOXIC GAS |
| MIL-S-83129 Revision A:1972 | SPECTROMETER, FLUID ANALYSIS A/E35U-3 (NO S/S DOCUMENT) |
| SAE AS6625A | Spray Equipment, Aircraft Windshield, Anti-Icing |
| MIL-B-26793 Revision B:1958 | Blower, Gasoline Engine Driven, Type A-1 (No S/S Document) |
| MIL-V-8610 Revision B:1984 | Valve, Fuel Shutoff Solenoid Operated, 28 Volt DC |
| MIL V 8057 : F | VALVE, OXYGEN, PRESSURE BUILDUP AND VENT |
| MIL-V-5461 Revision C:1977 | VALVE, VACUUM BREAKING (NO S/S DOCUMENT) |
| MIL-F-5509 Revision D:1978 | Fitting, Flared Tube, Fluid Connection (see Notice 2 for Additional Superseding Information) |
| MIL-V-8712 Revision A:1965 | VALVE, AIR RELIEF, LOW PRESSURE8(ASG) (S/S BY SAE-AS8712) |
| MIL-R-47321 Base Document:1987 | REGULATOR, PRESSURE, WATER PUMPED NITROGEN (NO S/S DOCUMENT) |
| MIL-S-6625 Revision A:1953 | SPRAY EQUIPMENT, AIRCRAFT WINDSHIELD, ANTI-ICING (S/S BY SAE-AS6625) |
| MIL-A-47309 Revision A:1991 | Amplifier, Pneumatic (S/S by SAE-ARP763) |
| MIL-T-21578 Revision A:1966 | TEST EQUIPMENT, HAZARDOUS LOCATION, INSTALLED, BASIC REQUIREMENTS FOR |
| MIL-G-10944 Revision B:1965 | Gage, Dimensional Control |
| MIL-DTL-19328 Revision F:1996 | Converter, Liquid Oxygen, 5 Liter, MB-5A |
| MIL C 25478 : B | COOLER, LUBRICATING OIL, AIRCRAFT ENGINE, SYNTHETIC OIL, GENERAL SPECIFICATION FOR |
| MIL-R-23057 Base Document:1961 | Regulator, Compressed Air, High Pressure (3500 PSI) |
| MIL H 22279 : C | HOSE ASSEMBLIES, RUBBER, AIRCRAFT FUELING, COLLAPSIBLE, BY NEGATIVE PRESSURE |
| MIL R 83055 : 0 | RAIN REPELLENT DISPENSING SYSTEMS, AIRCRAFT WINDSHIELD, GENERAL SPECIFICATION FOR |
| MIL-C-7488 Revision A:1974 | Cooler, Oil, Plate, Aircraft (S/S by MIL-PRF-25478) |
| MIL-P-9389 Revision A:1987 | PUMP, PRESSURE, OIL FREE AIR TYPE MA-3 (NO S/S DOCUMENT) |
| MIL V 9050 : E (1) | VALVE, OXYGEN, PRESSURE RELIEF, AIRCRAFT |
| MIL-A-27198 Revision B:1987 | Altimeter, Pressure AAU-7/A |
| MIL-C-9075 Revision A:1968 | Computer and Transmitter, True Airspeed, Pitot-Static, 150-900 Knots, Type MA-1 (No S/S Document) |
| MIL-I-23062 Base Document:1961 | Igniter, Mark 247 Mod O |
| MIL-W-18326 Revision A:1956 | WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR (S/S BY MIL-STD-2219) |
| SAE AS8712 | Valve; Air Relief, Low Pressure |
| MIL-D-6728 Revision A:1956 | Damper, Engine Exhaust Flame and Glare (No S/S Document) |
| MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
| MIL-V-18318 Revision B:1966 | VALVE, PRESSURE REGULATING, OXYGEN SYSTEM |
| MIL G 6019 : C | GAGE, PRESSURE, DIAL INDICATING, LOW-PRESSURE OXYGEN |
| MIL-P-5315 Revision B:1964 | PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT (S/S BY SAE-AMS-P-5315) |
| MIL C 25666 : E (1) | CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
| MIL R 25532 : A | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL V 25961 : F | VALVE, FILL-BUILDUP-VENT, LIQUID OXYGEN CONVERTER, CRU-5O/A |
| MIL-C-5191 Revision B:1953 | Computer and Transmitter, True Airspeed Pitot Static, Type A-2 (No S/S Document) |
| MIL-DTL-25666 Revision F:1995 | Converter, Liquid Oxygen, Capacitance Type Gauging, General Specification for |
| MIL M 5388 : B | MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B |
| AND10053 : 0006 | BOSS, PIPE-THREAD, INTERNAL - STANDARD DIMENSIONS FOR |
| AND10052 Revision 2:1954 | BOSSES - STANDARD DIMENSIONS FOR EXTERNAL PIPE THREAD (S/S BY SAE-AS5201) |
| MIL-G-10944 Revision B:1965 | Gage, Dimensional Control |
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