NASM 23460 : 2004
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
PIN, QUICK-RELEASE, SELF-RETAINING, POSITIVE-LOCKING
Hardcopy
01-11-2004
English
01-01-2004
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Defines positive-locking, single and double acting quick-release pins to be used on aircraft.
Committee |
FSC 5315
|
DevelopmentNote |
Supersedes MIL P 23460. (05/2000)
|
DocumentType |
Standard
|
Pages |
19
|
PublisherName |
Aerospace Industries Association
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
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, AIRCRAFT QUALITY [ASG] |
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 |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
MIL-H-6875 Revision H:1989 | HEAT TREATMENT OF STEEL RAW MATERIALS |
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 |
MIL-B-1083 Revision D:1987 | BALLS, BEARING, FERROUS AND NON-FERROUS (FOR USE IN BEARINGS, VALVES AND BEARING APPLICATIONS) GENERAL SPECIFICATION FOR |
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 |
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 |
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 |
PPP-H-1581 Revision A:1977 | HARDWARE (FASTENERS AND RELATED ITEMS) PACKAGING OF |
MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
QQ-A-591 Revision F:1981 | ALUMINUM ALLOY DIE CASTINGS |
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) |
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) |
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 |
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 |
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