MIL-C-6818 Revision D:1973
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
Clamp, Instrument Mounting, Aircraft (S/S by NASM6818)
Available format(s)
PDF
Published date
08-03-1973
Publisher
Superseded date
29-05-1998
€16.67
Excluding VAT
Describes aircraft instrument mounting clamps in various sizes.
| DocumentType |
Standard
|
| Pages |
10
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
This specification covers aircraft instrument mounting clamps.
| MIL I 18373 : B | INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
| MIL-L-5057 Revision F:1981 | Lights, Instrument, Individual, General Specification for (S/S by SAE-AS50571) |
| MS28042 Revision F:1982 | CLAMP, INSTRUMENT MOUNTING, AIRCRAFT (S/S BY NASM28042) |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| 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) |
| QQ-A-250-11 Revision F:1982 | Aluminum Alloy 6061, Plate and Sheet (See Notice 3 for Replacement Information) |
| MS24693 Revision K:1995 | SCREW, MACHINE, FLAT COUNTERSUNK HEAD, 100 DEG., CROSS RECESSED, UNC-2A AND UNF-2A (S/S BY NASM24693) |
| PPP-H-1581 Revision A:1977 | Hardware (Fasteners and Related Items), Packaging of (S/S by ASTM-D3951 or Mil-Std-2073-) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MS35215 Revision C:1987 | SCREW, MACHINE-PAN HEAD, CROSS-RECESSED, BRASS, UNF-2A (S/S BY NASM35215) |
| MS33639 Revision D:1988 | Cases, Instrument, Clamp - Mounted, Aircraft |
| MS35214 Revision D:1987 | SCREW, MACHINE-PAN HEAD, CROSS-RECESSED, BRASS, UNC-2A (S/S BY NASM35214) |
| MIL L 46010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
| MIL-C-6390 Revision B:1959 | Clamps and Instruments, Aircraft, Installation of |
| QQ-A-200-3 Revision F:1983 | Aluminum Alloy 2024, Bar, Rod, Shapes, Tube and Wire, Extruded (Refer to ASTM-B221, ASTM-B241/B241M and SAE-AMS-QQ-A-200/3) |
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