5305-01-521-5514
Find complete technical information, availability, and procurement data for: 5305-01-521-5514
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A preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. It may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. It may be mounted by means of fasteners, bonding or welding. Excludes:panel, interior lining, aircraft; cover access; cover, access, aircraft; floor (1), aircraft; core material, cellular, structural.
cone point (type bp) nonmachine thread style, 13.0 millimeters nominal fastener length, family of medium and light tactical vehicles (fmtv); high-mobility artillery rocket system (himars) end item identification, steel overall material, cross recess type 1 internal drive style
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- Fastener Length
- 13.0 millimeters nominal
- Internal Drive Style
- cross recess type 1
- End Item Identification
- family of medium and light tactical vehicles (fmtv); high-mobility artillery rocket system (himars)
- Nonmachine Thread Style
- cone point (type bp)
- Material
- steel overall
- Surface Treatment
- zinc alloy overall
- Test Data Document
- d8286-din7981 standard (includes industry or association standards, individual manufactureer standards, etc.).
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|---|---|
| 12414310-034 | Tapping Screw |
FAQs
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When the NSN 5305-01-521-5514 was assigned to the Federal Catalog?
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