MIL-S-7839 Revision B:1973
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
SCREW, STRUCTURAL, AIRCRAFT (S/S BY NASM7839)
Available format(s)
PDF
Published date
21-12-1973
Publisher
Superseded date
01-12-1999
€16.67
Excluding VAT
Covers aircraft structural screws.
| DevelopmentNote |
B Notice 1 - Notice of validation - remains inactive for new design. B Notice 2 - Notice of reactivation - and may be used for either new of existing design acquisition. B Notice 3 - Notice of cancellation/superseded by NASM 7839.
|
| DocumentType |
Standard
|
| Pages |
21
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
This specification covers aircraft structural screws.
| MIL S 81733 : C | SEALING AND COATING COMPOUND CORROSION INHIBITIVE |
| SAE AMS3259B | Sealing Compound, Polythioether Nonchromated, Corrosion Inhibiting for Intermittent Use to 360°F (182°C) |
| MIL-PRF-81733 Revision D:1998 | Sealing and Coating Compound, Corrosion Inhibitive |
| QQ-P-35 Revision C:1988 | Passivation Treatments for Corrosion-Resistant Steel (S/Sby ASTM-A967or SAE-AMS-QQ-P-35) |
| MS24694 Revision C:1969 | Screw, Machine, Flat Countersunk Head, 100 Deg., Structural, Cross Recessed, UNC-3A and UNF-3A (S/S by NASM24694) |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (SEE NAS410 AS A POSSIBLE REPLACEMENT) |
| MIL-H-6875 Revision H:1989 | Heat Treatment of Steel, Process for (S/S by SAE-AMS-H-6875) |
| MIL I 6866 : B | INSPECTION, PENETRANT METHOD OF |
| AN525 Revision 2:1985 | SCREW - WASHER HEAD (S/S BY NASM525) |
| MS9006 Revision C:1963 | RECESSES-CROSS, LOW TORQUE DRIVE, DIMENSIONS AND GAGE DIMENSIONS FOR (S/S BY NASM9006) |
| QQ A 225/6 : E | ALUMINUM ALLOY BAR, ROD, AND WIRE, ROLLED, DRAWN OR COLD FINISHED, 2024 |
| MIL-S-18732 Revision D:1968 | Steel Bars, Wire, Forging Stock, Forgings Tubing (431), Special Quality |
| AN503 Revision 5:1953 | SCREW - MACHINE, DRILLED FILLISTER HEAD, COARSE THREAD |
| SAE AMS6300G | Steel Bars and Forgings 0.25Mo (0.35 - 0.40C) (SAE 4037) |
| PPP-H-1581 Revision A:1977 | Hardware (Fasteners and Related Items), Packaging of (S/S by ASTM-D3951 or Mil-Std-2073-) |
| AN502 Revision 6:1953 | Screw - Machine, Drilled Fillister Head, Fine Thread |
| MIL-I-6868 Revision E:1976 | Inspection Process, Magnetic Particle (S/S by MIL-STD-1949) |
| MIL-S-8879 Revision C:1991 | Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879) |
| MIL-S-6050 Revision A:1967 | Steel, Chrome-Nickel-Molybdenum (8630) Bars and Reforging Stock (Aircraft Quality) (Future acquisitions for this material should refer to SAE-AMS6280) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| QQ-S-763 Revision F:1996 | STEEL BARS, WIRE, SHAPES, AND FORGINGS; CORROSION RESISTANT (S/S BY SAE-AMS-QQ-S-763) |
| MIL-S-6758 Revision B:1993 | STEEL, CHROME-MOLYBDENUM (4130) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) (S/S BY SAE-AMS-S-6758) |
| MIL-H-6088 Revision G:1991 | Heat Treatment of Aluminum Alloys (S/S by SAE-AMS-H-6088) |
| MIL-S-6098 Revision A:1967 | STEEL, CHROME-NICKEL-MOLYBDENUM (8735) BARS AND REFORGING STOCK (AIRCRAFT) (S/S BY SAE-AMS-S-6098) |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| QQ-B-728 Base Document:1961 | Bronze Manganese; Rod, Shapes, Forgings, and Flat Products (Flat Wire, Strip, Sheet, Bar, and Plates) (S/S by ASTM-B138) |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
| MIL-S-6049 Revision A:1967 | STEEL, CHROME-NICKEL-MOLYBDENUM (8740) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) (S/S BY SAE-AMS6322, SAE-AMS6325 AND SAE-AMS6327) |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
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