12 December 2011
6 December 1965
DETAIL SPECIFICATION SHEET
CLIP ASSEMBLY, COCKPIT UTILITY LIGHT
Inactive for new design after 31 August 2006.
This specification is approved for use by all Departments and Agencies of the Department of
The requirements for acquiring the product described herein shall consist of this specification sheet and MIL-DTL-6484, "Lights, Cockpit Utility, Aircraft General Specification for".
1. The clip assembly is designed for use with MS17246-1, "Mounting base, cockpit utility", as an aid to cockpit personnel for holding maps and other in-flight references.
1.1 Clip halves. Clip halves shall be manufactured from steel conforming to
ASTM A606/A606M, "Standard Specification for Steel, Sheet and Strip, High-Strength, Low- Alloy, Hot-Rolled and Cold-Rolled, with Improved Atmospheric Corrosion Resistance", type 2 or type 4, cold-rolled, condition as-rolled.
1.2 Spring. The spring shall be manufactured from steel wire conforming to
ASTM A228/A228M, "Standard Specification for Steel Wire, Music Spring Quality".
1.3 Shaft. The shaft shall be manufactured from brass, C36000 or C36010, temper HO2, conforming to ASTM B16/B16M, "Standard Specification for Free-Cutting Brass Rod, Bar and Shapes for Use in Screw Machines".
2. Finish. Material finish shall be best practice for application. If desired, cadmium plating conforming to type I, class A, of SAE AMS QQ P 416, "Plating, Cadmium (Electrodeposited)", may be used.
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