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5305-00-271-3621
Machine Screw
5305002713621 002713621 AN520C10-7
An externally threaded fastener whose threaded portion is of one nominal diameter, No 0 (0.060 in./1.5 mm) or larger, designed to be held or driven with either a wrench or an inserted driver or both (excluding internal socket or internal multiple spline types), in sizes below No. 10 (0.190 in./5 mm). No. 10 and larger sizes must have a head designed for any type inserted driver (excluding internal socket or internal multiple spline types), but may also be designed for external wrenching. A locking feature may be incorporated in the design of the head or threads. Excludes BOLT, CLEVIS; BOLT, EXTERNALLY RELIEVED BODY; SCREW, EXTERNALLY RELIEVED BODY; and SCREW, ASSEMBLED WASHER. See also, SCREW, INSTRUMENT; BOLT, MACHINE; BOLT, INTERNAL WRENCHING; and SCREW, CAP SOCKET HEAD. View more Machine Screw
January 2023
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Restrictions 5305-00-271-3621
5305-00-271-3621 is a Machine Screw 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 5305-00-271-3621
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5305-00-271-3621
- Brazil (YA01)
- Effective Date:
- 1 Jan 2011
- France (ZF01)
- Effective Date:
- 1 Apr 1991
- Italy (ZR01)
- Effective Date:
- 1 Apr 1991
Approved Sources 5305-00-271-3621
- Part Number
- Manufacturer
- Status
- AN520C10-7
- Manufacturer
- 88044 - Aeronautical Standards Group (Active)
- Definitive Standard
- Definitive Standard
Datasheet 5305-00-271-3621
- Characteristic
- Specifications
- FIIG
- Specifications
- A500D0
- Fastener Length [AASB]
- 0.438 Inches Nominal
- Head Diameter [AASL]
- 0.334 Inches Minimum And 0.359 Inches Maximum
- Head Height [AASU]
- 0.137 Inches Maximum
- Head Style [AASK]
- Round
- Nominal Thread Diameter [AHYM]
- 0.190 Inches
- Internal Drive Style [ABQZ]
- Slot
- Screw Material Document And Classification [CYAW]
- Qq-S-763,Cl Iv Fed Spec All Material Responses Or Mil-S-7720,Comp Fm Or G Mil Spec All Material Responses
- Screw Surface Treatment [CYBA]
- Passivate
- Screw Material [CYAU]
- Steel Comp 430 Or Steel Comp 302
- Thread Class [AAJD]
- 2A
- Thread Direction [AAJF]
- Right-Hand
- Thread Length [AASA]
- 0.438 Inches Nominal
- Thread Quantity Per Inch [CMLP]
- 32
- Thread Series Designator [THSD]
- Unf
NATO Stock Numbers Related to 5305-00-271-3621
Freight Information 5305-00-271-3621
5305-00-271-3621 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). 5305-00-271-3621 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5305-00-271-3621 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. 5305-00-271-3621 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. 5305-00-271-3621 is not classified as a special type of cargo when transported by water. 5305-00-271-3621 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.