MIL N 25027 : G
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F
Available format(s)
PDF
Language(s)
English
Publisher
Superseded date
08-15-1997
Superseded by
US$20.00
Excluding Tax where applicable
Covers self-locking nuts for use in these specified temperatures. Includes applicable documents, materials, qualification, design, bearing surface, threads, zinc plated nuts, aluminum alloy nuts, lubrication, dry film lubricant, wrench torque, locking torque, maximum locking torque, permanent set, stress corrosion, workmanship, vibration, magnetic permeability, copper base alloy nuts, and stress embrittlement.
| Committee |
FSC 5310
|
| DocumentType |
Standard
|
| Pages |
38
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-V-25023 Revision B:1967 | Valve, Fuel Drain, Self-Locking |
| MIL-C-5809 Revision G:1987 | Circuit Breakers, Trip-Free, Aircraft, General Specification for (S/S by SAE-AS58091) |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MIL-STD-7080 Base Document:1994 | Selection and Installation of Aircraft Electric Equipment |
| MIL-C-8605 Revision B:1990 | Cap; Pressure Fuel Servicing |
| MIL-N-25027-1 Revision A:1995 | Nut, Self-Locking, Heavy Hex, (Non-Metallic Insert) 250 Degrees and 450 Degrees F, UNJC-3B, 1/4 Through 2-1/2 Inch Nominal Diameters, Nickel-Copper Alloy (S/S by MIL-DTL-32258) |
| MIL-V-81356 Revision B:1992 | Valve, Fuel System Pressurization And Vent |
| ASTM F 1718 : 2001 : R2019 | Standard Specification for Rotary Positive Displacement Distillate Fuel Pumps |
| ASTM F 1718 : 2001 : R2013 | Standard Specification for Rotary Positive Displacement Distillate Fuel Pumps |
| MIL-N-45938 Revision A:1995 | NUT, PLAIN, CLINCH AND NUT, SELF-LOCKING, CLINCH, GENERAL SPECIFICATION FOR (S/S BY NASM45938) |
| MIL-N-85353 Base Document:1981 | NUTS (FASTENERS) INTERNALLY THREADED, PRELOAD LOCKING 450 DEG F 800 DEG F,1200 DEG F, GENERAL SPECIFICATION FOR |
| MIL-C-19179 Revision B:1963 | Coupling Assembly, Quick-Disconnect, Fuel (S/S by MIL-C-24788) |
| MIL-HDBK-2193 Base Document:1994 | Hydraulic System Components, Ship (S/S by MIL-STD-2193) |
| MIL-A-81973 Base Document:1974 | Aircrew Automated Escape Systems, Test Vehicles for Ground Track Performance Testing, Rocket and/or Jet Engine Propelled, General Specification for (No S/S Document) |
| DOD-P-24562 Revision A:1982 | Propeller, Ship, Controllable Pitch (Metric) |
| MIL-STD-242-12 Revision H:1984 | ELECTRONIC EQUIPMENT PARTS SELECTED STANDARDS HARDWARE & INSULATORS PART 12 (NO S/S DOCUMENT) |
| MIL-I-45934 Base Document:1971 | Insert, Screw Thread, Keyring Locked, Self Locking and Non Self Locking, 125, 180, and 220 KSI FTU: General Specification for (No S/S Document) |
| MIL-G-24260 Base Document:1967 | Generator Set, Diesel Engine, 100 KW, 120-Volt Direct Current, 1800 RPM (No S/S Document) |
| MIL-T-17523 Revision D:1976 | Turbine, Steam, Auxiliary (and Reduction Gear) Mechanical Drive |
| MIL-A-19736 Revision A:1960 | Air Refueling Systems, General Specification for |
| MIL-G-22997 Revision A:1965 | Generator Set, Diesel Engine, 100 KW, 450-Volt A.C., 60-Cycle, 1800 R.P.M. (No S/S Document) |
| MIL-B-24781 Base Document:1993 | Batterboard Systems, Synthetic (S/S by A-A-59001) |
| MIL-I-23870 Base Document:1963 | Indicator, Fuel Rate of Flow, 0 to 15 GPM (No S/S Document) |
| MIL-S-6150 Revision D:1987 | STARTER: ENGINE, ELECTRICAL, DIRECT CRANKING AIRCRAFT, 28 VOLTS DC (NO S/S DOCUMENT) |
| MIL-C-38373 Revision B:1975 | Cap, Fluid Tank Filler (No S/S Document) |
| MIL-S-8710 Revision B:1969 | Strainer, Airframe Fuel System, General Specification for |
| MIL-A-6425 Revision B:1959 | Adapter, Pressure Fuel Servicing, Aircraft, General Specification for (S/S by MIL-A-25896) |
| MIL-V-24439 Revision A:1984 | VALVE, OXYGEN, HELIUM AND HELIUM OXYGEN MIXTURE, HIGH PRESSURE FOR GAS SERVICES |
| MIL E 17807 : C | ELEVATOR, WEAPON AND CARGO, ELECTROMECHANICAL (SHIPBOARD) |
| MIL-C-85528 Base Document:1983 | CONNECTOR, ELECTRICAL, MOUNTING DEVICE, FLANGE TYPE, GENERAL SPECIFICATION FOR |
| MIL-DTL-27536 Revision C:1995 | Coupling, Clamp, Grooved, V-Band (S/S by SAE-AS5355) |
| MIL I 18373 : B | INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
| SAE ARP1616B | Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems |
| ASTM F 1718 : 2001 : R2006 | Standard Specification for Rotary Positive Displacement Distillate Fuel Pumps |
| NASA MSFC STD 486 : 1992 | STANDARD, THREADED FASTENERS, TORQUE LIMITS FOR |
| MIL G 6162 : B | GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
| MIL-A-23622 Base Document:1963 | Actuator, Aircraft, Electro-Mechanical, Linear, Direct Current |
| MIL-R-24358 Base Document:1968 | RESTORATION SHIPBOARD ELECTRONIC EQUIPMENT F, 1N AND 2N COGNIZANCE (S/S BY MIL-STD-2110) |
| MIL C 8783 : A | CLAMP, HOSE, FLAT BAND 500 DEG. F |
| DOD-B-24541 Revision A:1982 | Battery Cells and Elements, Lead-Acid, Main Storage, Submarine; General Specification for (Metric) (See Notice 3 for Replacement Information) |
| DOD-B-24200 Revision B:1978 | BATTERY CELLS AND ELEMENTS, LEAD ACID, LEAD-ANTIMONY, MAIN STORAGE, SUBMARINE; GENERAL SPECIFICATION FOR (METRIC) (NO S/S DOCUMENT) |
| MIL C 27715 : 0 | CIRCUIT BREAKER, TRIP-FREE, HIGH TEMPERATURE, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-A-25896 Revision E:1983 | Adapter, Pressure Fuel Servicing, Nominal 2.5-Inch Diameter |
| MIL-D-8181 Revision B:1965 | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification for (S/S by SAE-AS8181) |
| SAE AS8181A | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification For |
| MIL-R-24414 Revision D:1991 | Reels and Guides, Hose, Firefighting, Manually Operated |
| MIL-F-8378 Revision B:1975 | Frequency Meters, Aircraft 380 to 420 Hertz and 350 to 450 Hertz (No S/S Document) |
| MIL-T-17600 Revision D:1968 | Turbine, Steam, Propulsion Naval Shipboard |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| MIL-B-18558 Revision B:1988 | Bearing, Propulsion Line Shaft, Oil Disc Lubricated |
| MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
| MIL C 25531 : D | COUPLING HALF, QUICK DISCONNECT, PNEUMATIC STARTER, EXTERNAL, LOW PRESSURE, DIRECT RELEASE |
| MIL-D-23140 Revision D:1992 | Drawings, Installation Control, for Electronic Equipment |
| MIL-C-85049-94 Base Document:1993 | Connector Accessories, Electrical, Mounting Device Flange Type, Full Mounting Perimeter Device, Type I (Heavy Duty)(S/S by SAE-AS 85049/94) |
| MIL-C-7079 Revision A:1965 | Circuit Breakers, Non Trip-Free, General Specification for (No S/S Document) |
| ASTM F 1718 : 2001 | Standard Specification for Rotary Positive Displacement Distillate Fuel Pumps |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| QQ-P-35 Revision C:1988 | Passivation Treatments for Corrosion-Resistant Steel (S/Sby ASTM-A967or SAE-AMS-QQ-P-35) |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (SEE NAS410 AS A POSSIBLE REPLACEMENT) |
| AN503 Revision 5:1953 | SCREW - MACHINE, DRILLED FILLISTER HEAD, COARSE THREAD |
| TT-E-751 Revision C:1967 | Ethyl Acetate, Technical |
| MIL-STD-753 Revision C:1990 | CORROSION-RESISTANT STEEL PARTS: SAMPLING, INSPECTION AND TESTING FOR SURFACE PASSIVATION (S/S BY SAE-AMS-STD-753) |
| TT-I-735 Revision A:1963 | Isopropyl Alcohol |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-STD-1291 Revision A:1984 | IDENTIFICATION SYMBOLS FOR AEROSPACE FASTENER MANUFACTURERS (S/S BY MIL-HDBK-57) |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
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