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5310-00-619-1940
Plate Self-Locking Nut
5310006191940 006191940 K2400-08 NAS682A08
A nut with a flanged base of varied shapes which may be plain or mounted by rivets, bolts, welding or integral prongs. An integral feature is incorporated for locking on the threads of a mating member. View more Plate Self-Locking Nut
January 2023
37
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Updated Every Day Related Documents 5310-00-619-1940 5+ Documents (More...)
Plate Self-Locking Nut 5310006191940 5310-00-619-1940 5310006191940 006191940 is a nut with a flanged
Plate Self-Locking Nut 5310006191940 5310-00-619-1940 5310006191940 006191940 is a nut with a flanged
/fsg-45/fsc-4520/uk
Plate Self-Locking Nut 5310006191940 5310-00-619-1940 5310006191940 006191940 is a nut with a flanged
Plate Self-Locking Nut 5310006191940 5310-00-619-1940 5310006191940 006191940 is a nut with a flanged
NAS682A08 NUT,SELF-LOCKING,PLATE 50 EA NS Request Quotation Subscribe to View Vendor Details...
NAS682A08 NUT,SELF-LOCKING,PLATE 1 EA NS Request Quotation Subscribe to View Vendor Details...
Restrictions 5310-00-619-1940
5310-00-619-1940 is a Plate Self-Locking Nut 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. The precious metals content of this item is unknown.
Import and Export 5310-00-619-1940
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5310-00-619-1940
- Brazil (YA01)
- Effective Date:
- 1 Jun 2014
- Columbia (YC01)
- Effective Date:
- 1 Jul 2015
- Israel (YD)
- Israel (YD01)
- Effective Date:
- 1 Apr 1991
- Singapore (YJ)
- Singapore (YJ01)
- Effective Date:
- 1 Apr 1991
- Belgium (ZB)
- Belgium (ZB01)
- Effective Date:
- 1 Sep 2000
- New Zealand (ZE)
- New Zealand (ZE01)
- Effective Date:
- 1 Apr 1991
- France (ZF)
- France (ZF01)
- Effective Date:
- 1 Apr 1991
- Portugal (ZP)
- Portugal (ZP01)
- Effective Date:
- 1 Apr 1991
- Italy (ZR)
- Italy (ZR01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW)
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 5310-00-619-1940
- Part Number
- Manufacturer
- Status
- NAS682A08
- Manufacturer
- 80205 - National Aerospace Standards (Active)
- Primary Buy
- Primary Buy
- K2400-08
- 15653 - Howmet Global Fastening Systems Inc (Active)
- Primary Buy
- Primary Buy
- K2400-08
- R1120 - Satair A/S (Active)
- Secondary Buy
- Secondary Buy
- K2400-08
- 75237 - Howmet Global Fastening Systems Inc. (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- K2400-08
- F7652 - Klx Aerospace Solutions Ii Sas (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- K2400-08
- F6033 - Tecnotec Sarl (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- K2400-08
- FB009 - Boeing Distribution Services Inc (Active)
- Advisory Reference
- Advisory Reference
Datasheet 5310-00-619-1940
- Characteristic
- Specifications
- FIIG
- Specifications
- A021A0
- Center To Center Distance Between Mounting Holes Along Length [ADFY]
- 0.310 Inches Minimum And 0.314 Inches Maximum
- Counterbore Diameter [AAWY]
- 0.168 Inches Minimum Nut
- Distance From Aperture Center To Mounting Hole Center [ADFW]
- 0.339 Inches Minimum And 0.349 Inches Maximum
- Material [MATT]
- Steel Overall
- Mounting Hole Diameter [ABTB]
- 0.098 Inches Minimum And 0.103 Inches Maximum
- Mounting Hole Arrangement Style [ADFU]
- 2 Holes
- Nominal Thread Size [CQJX]
- 0.164 Inches
- Nut Counterbore Depth [ADFK]
- 0.062 Inches Minimum Nut
- Nut Height [ADEA]
- 0.250 Inches Maximum
- Nut Mounting Provision [ADFP]
- Straight Holes
- Nut Style [ACTA]
- Plate
- Nut Length [ACVN]
- 0.935 Inches Maximum
- Locking Feature [AAUM]
- Prevailing Torque All Metal Design
- Lubrication [ABAJ]
- Dry Film Lubricant
- Plate Thickness [ADEB]
- 0.047 Inches Maximum
- Plate Width [ADEC]
- 0.297 Inches Maximum
- Specification/Standard Data [ZZZK]
- 80205-Nas682 Professional/Industrial Association Standard
- Surface Treatment Document And Classification [STDC]
- Qq-P-416 Fed Spec Single Treatment Response Overall
- Surface Treatment [SFTT]
- Cadmium Overall
- Temp Rating [AZKQ]
- 450.0 Deg Fahrenheit Nominal
- Thread Class [AAJD]
- 3B
- Thread Direction [AAJF]
- Right-Hand
- Thread Quantity Per Inch [CMLP]
- 32
- Thread Series [BZRR]
- Unjc
NATO Stock Numbers Related to 5310-00-619-1940
Freight Information 5310-00-619-1940
5310-00-619-1940 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 093486. A Sub NMFC of Z. It has a NMFC Description of BOLTS,NUTS OR SCREWS, NOI (SUB 3). 5310-00-619-1940 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5310-00-619-1940 is rated as class 50 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 48950 which rates the freight between FCL and LCL. 5310-00-619-1940 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 573 for ocean manifesting and military sealift. 5310-00-619-1940 is not classified as a special type of cargo when transported by water. 5310-00-619-1940 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.