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5325-01-541-2008
Panel Fastener Insert
5325015412008 015412008 NAS1834 NAS1834C3-420
An insert which must have a hole that may be internally threaded with a flange on one end. It may have an undercut on the end opposite the flange to provide a shoulder to allow for mating with another insert. Pre-assembled items will consist of an expansion sleeve and a body which may be flared. Internally threaded items may have a self-locking feature. Excludes INSERT, SCREW THREAD. View more Panel Fastener Insert
November 2023
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NAS1834-4-562 INSERT,PANEL FASTENER 9 EA NS Request Quotation Subscribe to View Vendor Details...
NAS1834-4-562 INSERT,PANEL FASTENER 25 EA NS Request Quotation FedMall Updated Every 15 Minutes 5325-
-3-795 An insert which must have a hole that may be internally threaded with a flange on one NAS1834-
3-386 An insert which must have a hole that may be internally threaded with a flange on one - NAS1834
NAS1834-3K386 An insert which must have a hole that may be internally threaded with a flange on one
-3-795 An insert which must have a hole that may be internally threaded with a flange on one NAS1834-
NAS1834-3K386 An insert which must have a hole that may be internally threaded with a flange on one
-3-795 An insert which must have a hole that may be internally threaded with a flange on one NAS1834-
Restrictions 5325-01-541-2008
5325-01-541-2008 is a Panel Fastener Insert that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 5325-01-541-2008
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5325-01-541-2008
- Germany (ZG01)
- Effective Date:
- 1 Jun 2006
Approved Sources 5325-01-541-2008
- Part Number
- Manufacturer
- Status
- NAS1834
- Manufacturer
- 80205 - National Aerospace Standards (Active)
- Incomplete Reference
- Incomplete Reference
- NAS1834C3-420
- 80205 - National Aerospace Standards (Active)
- Primary Buy
- Primary Buy
Datasheet 5325-01-541-2008
- Characteristic
- Specifications
- FIIG
- Specifications
- A05400
- End Item Identification [AGAV]
- Helicopter Seaking Mk41
- Flange Diameter [ABKK]
- 0.550 Inches Minimum And 0.560 Inches Maximum
- Flange Thickness [CWTF]
- 0.060 Inches Nominal
- Hole Diameter [CWYP]
- 0.195 Inches Minimum And 0.201 Inches Maximum
- Hole Type [BQDM]
- Plain
- Material [MATT]
- Steel Overall
- Insert Style [CWXS]
- Protruding Flange
- Shoulder Diameter [AAXB]
- 0.550 Inches Minimum And 0.560 Inches Maximum
NATO Stock Numbers Related to 5325-01-541-2008
Freight Information 5325-01-541-2008
5325-01-541-2008 has freight characteristics.. 5325-01-541-2008 has a variance between NMFC and UFC when transported by rail and the description should be consulted.