MIL-P-23460 Revision E:1991
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
PIN, QUICK-RELEASE, SELF-RETAINING, POSITIVE-LOCKING (S/S BY NASM23460)
Available format(s)
PDF
Published date
20-11-1991
Publisher
Superseded date
31-03-2000
£13.91
Excluding VAT
Covers both single and double acting quick-release pins for use on aircraft
| DocumentType |
Standard
|
| Pages |
24
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| PREN 6068 : 200P2 | AEROSPACE SERIES - PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, SINGLE ACTING, BUTTON HANDLE |
| MIL-A-23121 Revision C:1970 | Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document) |
| 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) |
| MIL-D-23615 Revision C:1993 | Design and Evaluation of Cartridge Actuated Devices |
| MIL-C-83124 Base Document:1969 | Cartridge Actuated Devices/Propellant Actuated Devices General Design Specification for |
| PREN 6067 : 200P2 | AEROSPACE SERIES - PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, DOUBLE ACTING, BUTTON HANDLE |
| NASA KSC STD P 0006 : 1995 | QUICK RELEASE PINS AND PIN TETHERS, STANDARD FOR |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| SAE AMS5659S | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-T-6736 Revision B:1965 | TUBING, CHROME-MOLYBDENUM, 4130 STEEL, SEAMLESS AND WELDED, AIRCRAFT QUALITY (USERS MAY REFER TO SAE-AMS-T-6736) AS A POSSIBLE REPLACEMENT) |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| QQ-P-35 Revision C:1988 | Passivation Treatments for Corrosion-Resistant Steel (S/Sby ASTM-A967or SAE-AMS-QQ-P-35) |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-H-6875 Revision H:1989 | Heat Treatment of Steel, Process for (S/S by SAE-AMS-H-6875) |
| SAE AMS5643U | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb (Nb) - 4.0Cu Solution Heat Treated, Precipitation Hardenable |
| QQ-A-200-8 Revision F:1983 | Aluminum Alloy 6061, Bar, Rod, Shapes, Tube and Wire, Extruded (Refer to ASTM-B241/B241M, ASTM-B221 and SAE-AMS-QQ-A-200/8) |
| MIL-B-1083 Revision D:1987 | Balls, Bearing, Ferrous and Non-Ferrous (For Use in Bearings, Valves and Bearing Applications) General Specification For (See Notice 3 for replacement information) |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| SAE AMS 6530 : H NONCURRENT | STEEL TUBING, SEAMLESS, 0.50Ni 0.55Cr 0.20Mo (0.28-0.33C) |
| QQ A 225/6 : E | ALUMINUM ALLOY BAR, ROD, AND WIRE, ROLLED, DRAWN OR COLD FINISHED, 2024 |
| MIL-B-007883 Revision C:1968 | Brazing of Steels, Copper, Copper Alloys, Nickel Alloys, Aluminum and Aluminum Alloys (Future Acquisitions should specify one AWS-C3.4, AWS-C3.5, AWS-C3.6 and AWS-C3.7) |
| MIL T 6735 : A | TUBING, CHROME-MOLYBDENUM, 4135 STEEL, SEAMLESS AIRCRAFT QUALITY |
| QQ-A-225-3 Revision D:1971 | Aluminum Alloy Bar, Rod, and Wire; Rolled, Drawn, or Cold Finished, 2011(S/S by SAE-AMS-QQ-A-225 and ASTM-B211) |
| SAE AMS5880E | Steel, Corrosion-Resistant, Bars, Wire, and Forgings 17Cr 0.52Mo (0.95 1.20C) (SAE 51440C) for Bearing Applications |
| MIL-STD-2219 Revision A:2005 | Fusion Welding for Aerospace Applications (S/S by AWS-D17.1) |
| PPP-H-1581 Revision A:1977 | Hardware (Fasteners and Related Items), Packaging of (S/S by ASTM-D3951 or Mil-Std-2073-) |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| QQ-A-591 Revision F:1981 | Aluminum Alloy Die Castings (S/S by Appropriate Portions of the Document ASTM-B85, ASTM-B26, ASTM-B108 and SAE-J452, SAE-J453, SAE-AMS4290, SAE-AMS4291) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| SAE AMS5630L | Steel, Corrosion-Resistant, Bars, Wire, and Forgings 17Cr - 0.52Mo (0.95 - 1.20C) (440C) |
| MIL-S-6758 Revision B:1993 | STEEL, CHROME-MOLYBDENUM (4130) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) (S/S BY SAE-AMS-S-6758) |
| MIL G 23827 : B | GREASE, AIRCRAFT AND INSTRUMENT, GEAR AND ACTUATOR SCREW |
| SAE AMS5678F | Steel, Corrosion Resistant, Wire 17Cr - 7.1Ni - 1.1Al Cold Drawn, Precipitation-Hardenable |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| QQ A 225/8 : E | ALUMINUM ALLOY 6061, BAR, ROD, WIRE & SPECIAL SHAPES, ROLLED, DRAWN OR COLD FINISHED |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
| QQ A 225/5 : E | ALUMINUM ALLOY 2017, BAR, ROD AND WIRE; ROLLED DRAWN OR COLD FINISHED |
| MIL T 31000 : 0 | TECHNICAL DATA PACKAGES - GENERAL SPECIFICATION FOR |
Summarise
£13.91
Excluding VAT
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