5305-01-536-1816
Find complete technical information, availability, and procurement data for: 5305-01-536-1816
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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.
0.350 inches minimum and 0.400 inches maximum thread length, 1.548 inches minimum and 1.578 inches maximum fastener length, right-hand thread direction, flat countersunk head style, 3a thread class
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- Thread Class
- 3a
- Thread Direction
- right-hand
- Thread Length
- 0.350 inches minimum and 0.400 inches maximum
- Fastener Length
- 1.548 inches minimum and 1.578 inches maximum
- Head Style
- flat countersunk
- Hole Diameter
- 0.076 inches minimum and 0.086 inches maximum
- Grip Diameter
- 0.311 inches minimum and 0.312 inches maximum
- Internal Drive Style
- cross recess type 1
- End Item Identification
- u-2
- Nominal Thread Diameter
- 0.312 inches
- Grip Length
- 1.178 inches minimum and 1.198 inches maximum
- Thread Quantity Per Inch
- 24
- Part Name Assigned By Controlling Agency
- screw
- Material
- iron alloy overall
- Surface Treatment
- cadmium overall
- Thread Series Designator
- unjf
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|---|---|
| LA-NAS1205-19D | Close Tolerance Screw |
FAQs
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When the NSN 5305-01-536-1816 was assigned to the Federal Catalog?
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