Premium Information is available for this item - Upgrade for $1 a day

5305-00-422-4221

Tapping Screw

5305004224221 004224221 274875

A hardened externally threaded fastener whose thread extends to the bearing surface of the head. The thread may be fluted or otherwise designed to cut or form its own mating thread. Excludes SCREW, ASSEMBLED WASHER. View more Tapping Screw

5305-00-422-4221 SCREW,TAPPING 5305004224221 004224221

Managed by United States
NSN Created on 2 Feb 1972
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
5305-00-422-4221 SCREW,TAPPING 5305004224221 004224221 1/1
NSN 5305-00-422-4221 (Generic Image) 1/1

5305-00-422-4221 Stock and Availability Marketplace 5305-00-422-4221

Need Help?
Request a Quotation from participating marketplace vendors
eBay Updated Every Day
5305-00-422-4221 RQST NE eBay
eBay Updated Every Day
5305-00-422-4221 RQST eBay
Amazon Updated Every Day
5305-00-422-4221 RQST NE Amazon

5305-00-422-4221 Related Documents Related Documents 5305-00-422-4221 5+ Documents (More...)

(CAGE Code 1LW55) DAC: 5 13 Dec 1968 5305-00-422-4221 Tapping Screw 274875RNCC: C | RNVC: 1 | DAC: 5
FUEHRUNG https//www.nsnlookup.com /cage General Motors Corp (CAGE Code 16764) DAC: 5 6 Jun 1968 5305-00-422-4221
5305-00-855-0967 5305008550967 008550967 is a hardened externally threaded fastener whose thread extends to the bearing surface of the head. the thread may be fluted or otherwise designed to cut or form its own mating thread. excludes screw, assembled washer.
Jul 1971 5910-00-132-2503 Electrica Capacitor 1963559RNCC: 3 | RNVC: 2 | DAC: 5 13 Dec 1968 5305-00-422-4221
browser . 2840-00-696-9594Aircraft Gas Turbine Engine Compressor Vane Assembly2840006969594 006969594 274875
how to enable JavaScript in your web browser . 5305-14-234-6155Vis Speciale5305142346155 142346155 274875
NumberManufacturerStatus274875 F6137 - Safran Landing Systems (Active) Primary Buy RNCC 3 RNVC 2 DAC 5 274875
1968 6105-21-001-4940 Alternating Current Motor A5200B4-41RNCC: 3 | RNVC: 2 | DAC: 5 6 Jun 1968 5305-00-422-4221

5305-00-422-4221 Demil Restrictions 5305-00-422-4221

DEMIL: A | DEMILI: 1 | CRITICALITY: N | HMIC: N | PMIC: A | EDC: | ADPEC:

5305-00-422-4221 is a Tapping Screw 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.

5305-00-422-4221 End Users End Users 5305-00-422-4221

US Air Force (FUU5)
Effective Date:
1 Sep 2000
Former MOE Rule:
FEE5
US Marine Corps (MF6F)
Effective Date:
1 Sep 2000

5305-00-422-4221 Manufacturers Approved Sources 5305-00-422-4221

5305-00-422-4221 Technical Data Datasheet 5305-00-422-4221

Characteristic
Specifications
Fastener Length [AASB]
0.590 Inches Minimum And 0.620 Inches Maximum
Head Diameter [AASL]
0.306 Inches Minimum And 0.322 Inches Maximum
Head Height [AASU]
0.085 Inches Minimum And 0.095 Inches Maximum
Head Style [AASK]
Pan No. 2
Material [MATT]
Steel Overall
Nonmachine Nominal Thread Diameter [CTYF]
0.164 Inches
Nonmachine Thread Style [CRGF]
Thru Slot (Type 6)
Internal Drive Style [ABQZ]
Slot
Material Document And Classification [MDCL]
G-6010M,Fscm 16764 Mfr Ref Single Material Response Overall
Surface Treatment Document And Classification [STDC]
G-4841M,Fscm 16764 Mfr Ref Single Treatment Response Overall
Surface Treatment [SFTT]
Cadmium Overall

5305-00-422-4221 Management Data Management Data 5305-00-422-4221

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Aug 2017
Department of the Air Force (DF)
EA
Subscribe
May 2017
US Marine Corps (DM)
EA
Subscribe
Oct 2005
Department of the Army (DA)
EA
Subscribe
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Air Force (DF)
I
V
Discontinued Without Replacement

Army Army

Materiel Category and Inventory Manager:
K
Tactical and Support Vehicles, Combat and Automotive Materiel
Appropriation and Budget Activity:
2
Stock Fund Secondary Items
Management Inventory Segment:
2
Non-Repairable Items(Exclusive of Insurance and Provisioning Items)
This code will be used to identify items, which are not reparable.
Weapons System / End Item / Homogeneous Group:
IE
Construction Equipment
Cranes, Wheel
Accounting Requirements:
X
Expendable item.An item of Army property coded with an ARC of X in the AMDF. Expendable items require no formal accountability after issue from a stock record account.Commercial and fabricated items similar to items coded X in the AMDF are considered expendable items.

Marine Corps Marine Corps

Stores Account:
1
Stock Fund Account Item
Combat Essentiality:
2
Non-Critical Repair Part
Echelon Management:
56
Operational Test:
No Special Procedures

5305-00-422-4221 Related Items NATO Stock Numbers Related to 5305-00-422-4221

5305-00-422-4221 Freight Data Freight Information 5305-00-422-4221

5305-00-422-4221 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). 5305-00-422-4221 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5305-00-422-4221 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. 5305-00-422-4221 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 713 for ocean manifesting and military sealift. 5305-00-422-4221 is not classified as a special type of cargo when transported by water. 5305-00-422-4221 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.