Marketing Masters, Inc. - Press Fit Inserts
Home
About Us
Contact Us
Online Catalog
Tel. 425.454.5610
Self-Locking Corrosion Free Composite Clip Nuts
General Uses for Corrosion Free Clip Nuts
Clip Nuts Catalog
Benefits of Torlon® Clip Nuts
Styles, Specs & Approvals of Clip Nuts
Clip Nuts Part Number Cross Reference
Corrosion Free Composite Inserts
General Uses for Composite Inserts
Composite Inserts Catalog
Styles of Composite Inserts
Press Fit Style Inserts
Press Fit Inserts Catalog
Potted-In Style Inserts
Potted-In Inserts Catalog
Inserts Part Number Cross Reference
Torlon Engineered Plastics
Torlon Industry Approvals
Data Sheets
Search Catalog
By Keyword
By Item #
All Categories
Press Fit Inserts
All Categories
>
"NAS 1833 Type" Thru Threaded Insert
>
Press Fit Inserts
>
View Items
Printable Page
Email This Page
Save To Favorites
Press Fit Inserts
Check up to five results to perform an action.
Marketing Masters Composite Press Fit Inserts:
Used with honeycomb sandwich panels.
Lightweight, Torlon®, non-metallic inserts for a myriad of applications where traditional metal inserts were previously used.
Commonly referred to as "Floor Panel Inserts" because they are widely used in aircraft flooring to fasten the panels to the aircraft structure.
Can be used anywhere a through hole fastener is desired, where very high load carrying capabilities are considered necessary and insert protrusion out of the panel is not a problem.
The flanges of a press-fit / adhesive bonded Torlon® insert are glued to the top and bottom skins of the panel and are therefore not considered "flush" with the panel skins.
Each insert is capable of carrying over a 2,000-lb load, depending on the panel type.
Our standard press-fit insert requires a 7/16" hole to be drilled in the panel and it has a 7/8" diameter flange that will be glued to the panel skin. As shown in the figure on the right, the top flange incorporates a beveled edge, providing for a very low profile insert. A hole is drilled through the panel and the insert is placed into the hole where the plug and sleeve are pressed together. The flanges of the inserts are glued to the panel skin, providing a fixed through hole in the panel.
larger image
larger image
Results per Page :
25
50
100
200
Results 1 - 25 of 43
1
2
Item #
Press Fit Style
Panel Thickness (in.)
Thru Hole Diameter (in.)
Thru Bolt Size Reference (in.)
Bolt CSK
Installation Hole Size
G2001A-3P
Airbus Style
.375
.196
.1900
100° x .385 ø
15mm
G2002A-3S
Airbus Style
.375
.196
.1900
N/A
15mm
G2101A-3P-375
Airbus Style
.375
.196
.1900
100° x .385 ø
15mm
G2101A-3P-500
Airbus Style
.500
.196
.1900
100° x .385 ø
15mm
G2102A-3S
Airbus Style
.375 / .500
.196
.1900
N/A
15mm
G2001B-08P
Boeing Style
.400
.169
.1640
100° x .335 ø
7/16"
G2001B-3P
Boeing Style
.400
.196
.1900
100° x .385 ø
7/16"
G2001BF-3P
Boeing Style
.400
.196
.1900
NO CSK
7/16"
G2001BR-3P
Boeing Style
.400
.196
.1900
100° x .305 ø
7/16"
G2001B-3P Black
Boeing Style
.400
.196
.1900
100° x .385 ø
7/16"
G2002B-08S
Boeing Style
.400
.169
.1640
N/A
7/16"
G2002B-3S
Boeing Style
.400
.196
.1900
N/A
7/16"
G2002B-3S Black
Boeing Style
.400
.196
.1900
N/A
7/16"
9D0316-3P
Boeing Style
.400
.196
.1900
100° x .305 ø
7/16"
9D0316-3S
Boeing Style
.400
.196
.1900
N/A
7/16"
G2001B-3P-230
Boeing Style
.230
.196
.1900
100° x .385 ø
7/16"
G2001BF-3P-230
Boeing Style
.230
.196
.1900
NO CSK
7/16"
G2002B-3S-230
Boeing Style
.230
.196
.1900
N/A
7/16"
G2001B-3P-280
Boeing Style
.280
.196
.1900
100° x .385 ø
7/16"
G2002B-3S-280
Boeing Style
.280
.196
.1900
N/A
7/16"
G2001B-3P-300
Boeing Style
.300
.196
.1900
100° x .385 ø
7/16"
G2002B-3S-300
Boeing Style
.300
.196
.1900
N/A
7/16"
G2001B-3P-320
Boeing Style
.320
.196
.1900
100° x .385 ø
7/16"
G2002B-3S-320
Boeing Style
.320
.196
.1900
N/A
7/16"
G2001B-3P-375
Boeing Style
.375
.196
.1900
100° x .385 ø
7/16"
Results 1 - 25 of 43
1
2
Site Map
| Site Credits:
Ecreativeworks