5340-01-687-3282
Find complete technical information, availability, and procurement data for: 5340-01-687-3282
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An auxiliary longitudinal member of the structural framework of a fuselage, nacelle, empennage, wing, and the like. It is designed to stiffen and/or support the skin by attachment of bulkheads, formers, frames, ribs, and the like.
0.797 inches minimum and 0.827 inches maximum overall width, 3.04 inches minimum and 3.10 inches maximum distance between mounting hole centers, f/a-18 hornet end item identification, 0.040 inches nominal material thickness, 2.10 inches minimum and 2.40 inches maximum overall length
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- Overall Length
- 2.10 inches minimum and 2.40 inches maximum
- Overall Width
- 0.797 inches minimum and 0.827 inches maximum
- Material Thickness
- 0.040 inches nominal
- Distance Between Mounting Hole Centers
- 3.04 inches minimum and 3.10 inches maximum
- End Item Identification
- f/a-18 hornet
- Cushioning Material
- unable to decode
- Cushion
- included
- Mounting Pad
- included
- Mounting Hole Size
- 0.204 inches nominal
- Distance Between Base And Inside Of Arch
- 0.9465 inches nominal
- Inside Diameter/Arch Length
- 1.360 inches minimum and 1.390 inches maximum
- Part Name Assigned By Controlling Agency
- strap,retaining
- Material
- steel comp 321 or steel comp 302 or steel comp 304
- Surface Treatment
- passivate
- Style Designator
- saddle arch
Related Parts
This NSN group includes multiple components designed to meet specific performance and operational standards. Each listing provides detailed specs, functionality data, and replacement compatibility information:
| Part Number | Name |
|---|---|
| NAS1677C13W36N | Retaining Strap |
FAQs
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