Premium Information is available for this item - Upgrade for $1 a day
5305-01-488-3747
Close Tolerance Screw
5305014883747 014883747 CA21351-6-14RS
A SCREW, MACHINE or SCREW, CAP, SOCKET HEAD whose unthreaded portion is of specified grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001 IN.) (0.025 mm) or less of a specific diameter for items (1.000 IN.) (25 mm) or less in diameter. Items over (1.000 IN.) (25 mm) in diameter shall have a tolerance of fifteen ten thousandths (0.0015 IN.) (0.038 mm) or less. The nominal major diameter of the threads shall be at least one thousandth (0.001 IN.) (0.025 mm) below the minimum shank diameter, but not below the minimum major diameter for applicable class of fit, as shown in the Screw Thread Standards, FED STD H28 and/or other nationally recognized standards. The head is designed to be held or driven with an inserted driver. It is not designed for rotation by the thumb and fingers. A locking feature may be incorporated in the design of the head or threads. View more Close Tolerance Screw
January 2023
1
Marketplace 5305-01-488-3747
Request a Quotation from participating marketplace vendors
Restrictions 5305-01-488-3747
5305-01-488-3747 is a Close Tolerance 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. This item does not contain a precious metal.
Import and Export 5305-01-488-3747
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5305-01-488-3747
- US Air Force (FLL5)
- Effective Date:
- 1 Aug 2001
Approved Sources 5305-01-488-3747
- Part Number
- Manufacturer
- Status
- CA21351-6-14RS
- Manufacturer
- 92215 - Howmet Global Fastening Systems Inc (Active)
- Primary Buy
- Primary Buy
Datasheet 5305-01-488-3747
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- End Item Identification [AGAV]
- F-22 Raptor
- Countersink Angle [CRSQ]
- 99.0 Degrees Minimum And 100.0 Degrees Maximum
- Fastener Length [AASB]
- 1.895 Inches Nominal
- Grip Diameter [AAUR]
- 0.374 Inches Nominal
- Grip Length [ANEE]
- 0.991 Inches Minimum And 1.130 Inches Maximum
- Head Diameter [AASL]
- 0.672 Inches Nominal
- Head Style [AASK]
- Flat Countersunk
- Material [MATT]
- Iron Alloy 660 Overall
- Minimum Tensile Strength [CQBC]
- 7360 Pounds Per Square Inch
- Nominal Thread Diameter [AHYM]
- 0.375 Inches
- Locking Feature [AAUM]
- Detent Ring Locking Feature
- Material Document And Classification [MDCL]
- Ams 5731 National Std/Spec 1St Material Response Overall Or Ams 5737 National Std/Spec 2Nd Material Response Overall
- Point Chamfer Angle [CWDK]
- 45.0 Degrees Nominal
- Point Diameter [AAVA]
- 0.330 Inches Minimum And 0.335 Inches Maximum
- Point Length [AAUY]
- 0.100 Inches Nominal
- Point Style [ABQJ]
- Chamfer Dog
- Single Shear Strength [AAWU]
- 9400 Pounds Per Square Inch
- Part Name Assigned By Controlling Agency [CXCY]
- Stud Bolt
- Special Features [FEAT]
- Drive Style Is: Radial-Slot Recess/ Fairchild Areospace, Not Listed This Fiig. Bored Hole, Threaded End, 0.130 In Dia, 0.620 In Dp; Wire Form Hold-Out Spring Inserted; 2 Lead Thread.
- Thread Series Designator [THSD]
- Unf
- Thread Quantity Per Inch [CMLP]
- 24
- Supplementary Features [SUPP]
- Stud Bolts Shall Have Polyproplene Head Protective Ring Installed For Shipping, Customer To Remove Ring Before Installing
- Surface Treatment Document And Classification [STDC]
- Ams Qq-P-35 National Std/Spec All Treatment Responses Overall
- Surface Treatment [SFTT]
- Passivate Overall
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
- Thread Length [AASA]
- 0.665 Inches Minimum And 0.804 Inches Maximum
Management Data 5305-01-488-3747
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Dec 2011
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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 5305-01-488-3747
Freight Information 5305-01-488-3747
5305-01-488-3747 has freight characteristics.. 5305-01-488-3747 has a variance between NMFC and UFC when transported by rail and the description should be consulted.