5305-01-537-3411
Find complete technical information, availability, and procurement data for: 5305-01-537-3411
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A self-contained, dead-reckoning system that senses acceleration along the pitch, yaw and roll axis of land vehicle, watercraft or aircraft and calculates the distance from a reference point. They can include inertial navigation unit(s); platform, inertial; power supplies; subsystems; mode selectors; and control displays.
0.134 inches minimum and 0.138 inches maximum head height, hexagon head style, 3a thread class, right-hand thread direction, 0.552 inches minimum and 0.572 inches maximum fastener length
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
- Fastener Length
- 0.552 inches minimum and 0.572 inches maximum
- Head Style
- hexagon
- Head Height
- 0.134 inches minimum and 0.138 inches maximum
- Width Between Flats
- 0.244 inches minimum and 0.250 inches maximum
- Internal Drive Style
- hexagon
- End Item Identification
- f-22 raptor (emd)
- Material Accommodated Thickness
- 0.240 inches minimum and 0.260 inches maximum
- Nominal Thread Diameter
- 0.138 inches
- Thread Quantity Per Inch
- 32
- Part Name Assigned By Controlling Agency
- screw,cap, hexagon head
- Material
- iron alloy 660 overall
- Material Document And Classification
- ams 5731 national std/spec 1st material response or ams 5737 national std/spec 2nd material response overall
- Surface Treatment
- passivate overall
- Surface Treatment Document And Classification
- ams qq-p-35 national std/spec all treatment responses overall
- Thread Series Designator
- unjc
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|---|---|
| CA2290-06-8-9 | Panel Screw Assembly |
FAQs
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When the NSN 5305-01-537-3411 was assigned to the Federal Catalog?
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