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5305-01-490-2960
Panel Screw Assembly
5305014902960 014902960 CA22051-6T22-19
A headed, threaded fastening device over which may be assembled; (1) a stand-off; (2) a flanged bushing with washer(s) and/or a shouldered bushing without a flange, or it may have an internally threaded sleeve that is an integral part of the screw; a washer and an externally thread self-locking bushing that is driven by an inserted driver. Attached to panel by threaded bushing or by flaring end of stand-off, or bushing. Used in conjunction with a speed nut, nut plate, or driven into a threaded hole in the item that the panel is fastened to. May be spring loaded. View more Panel Screw Assembly
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Panel Screw Assembly 5305014902960 014902960 5305-01-490-2960 5305014902960 014902960 is a headed
Restrictions 5305-01-490-2960
5305-01-490-2960 is a Panel Screw Assembly 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 5305-01-490-2960
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5305-01-490-2960
- US Air Force (FLL5)
- Effective Date:
- 1 Sep 2001
Approved Sources 5305-01-490-2960
- Part Number
- Manufacturer
- Status
- CA22051-6T22-19
- Manufacturer
- 29372 - Howmet Global Fastening Systems Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 5305-01-490-2960
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- End Item Identification [AGAV]
- F-22 Raptor
- Fastener Length [AASB]
- 1.178 Inches Minimum And 1.198 Inches Maximum
- Head Height [AASU]
- 0.188 Inches Minimum And 0.209 Inches Maximum
- Head Style [AASK]
- Hexagon
- Material [MATT]
- Nickel Alloy 718 Overall
- Nominal Thread Diameter [AHYM]
- 0.375 Inches
- Internal Drive Style [ABQZ]
- Torx
- Material Accommodated Thickness [AGSM]
- 0.688 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Screw
- Thread Series Designator [THSD]
- Unjf
- Thread Quantity Per Inch [CMLP]
- 24
- Width Between Flats [AATB]
- 0.554 Inches Minimum And 0.564 Inches Maximum
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
Management Data 5305-01-490-2960
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- FR
- F-22 AIRCRAFT
- Price Validation Code:
- E
- The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
NATO Stock Numbers Related to 5305-01-490-2960
Freight Information 5305-01-490-2960
5305-01-490-2960 has freight characteristics.. 5305-01-490-2960 has a variance between NMFC and UFC when transported by rail and the description should be consulted.