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5306-00-488-6528
Internal Wrenching Bolt
5306004886528 004886528 64404-3-84 111-0115-002
An externally threaded fastener whose threaded portion is of one nominal diameter, No. 10 (0.190 IN.) (5 mm) or larger. It is designed with an internal socket or internal multiple spline for use with an internal driver. The head is beveled (conical) or cylindrical in shape. Items with cylindrical shaped heads must have an externally relieved body. A locking feature may be incorporated in the design of the head or threads. See also SCREW, CAP, SOCKET HEAD. Excludes SETSCREW; SCREW, SHOULDER; BOLT, SHOULDER; SCREW, EXTERNALLY RELIEVED BODY; BOLT, EXTERNALLY RELIEVED BODY; and SCREW, MACHINE. View more Internal Wrenching Bolt
May 2023
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Restrictions 5306-00-488-6528
5306-00-488-6528 is a Internal Wrenching Bolt 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 5306-00-488-6528
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5306-00-488-6528
- US Air Force (FUGI)
- Effective Date:
- 1 Aug 2005
- Former MOE Rule:
- FUKZ
Approved Sources 5306-00-488-6528
- Part Number
- Manufacturer
- Status
- 64404-3-84
- Manufacturer
- 56878 - Sps Technologies, Llc (Active)
- Primary Buy
- Primary Buy
- 111-0115-002
- 94756 - The Boeing Company (Active)
- Secondary Buy
- Secondary Buy
Datasheet 5306-00-488-6528
- Characteristic
- Specifications
- FIIG
- Specifications
- A003B0
- Fastener Length [AASB]
- 5.673 Inches Minimum And 5.703 Inches Maximum
- Head Diameter [AASL]
- 0.318 Inches Minimum And 0.328 Inches Maximum
- Head Height [AASU]
- 0.190 Inches Nominal
- Material Document And Classification [MDCL]
- Nas621,Comp 6Al-4V Assn Std Single Material Response Overall
- Material [MATT]
- Titanium Alloy Overall
- Minimum Tensile Strength [CQBC]
- 160000 Pounds Per Square Inch
- Nominal Thread Diameter [AHYM]
- 0.190 Inches
- Internal Drive Style [ABQZ]
- Hexagon
- Width Across Flats [ASDB]
- 0.156 Inches Minimum And 0.158 Inches Maximum
- Surface Finish [CSYM]
- 63.0 Microinches Bearing Surface Of Head
- Surface Finish [CSYM]
- 63.0 Microinches Grip
- Thread Class [AAJD]
- 3A
- Thread Direction [AAJF]
- Right-Hand
- Thread Length [AASA]
- 0.413 Inches Minimum And 0.463 Inches Maximum
- Thread Quantity Per Inch [CMLP]
- 32
- Thread Series Designator [THSD]
- Unf
DLA Procurement Analysis 5306-00-488-6528
Management Data 5306-00-488-6528
Air Force
- Fund:
- SF
- Stock fund applicable to items managed for the Air Force by the respective Inventory Control Point
- Budget:
- 9
- 57X4921.070 - General Support DIV - Air Force decentralized managed expense items (ERRC XB3, XF3) with a unit cost of less than $250,000 that are requisitioned/procured at base (retail) level from DLA, GSA, Army, Navy, Depot Maintenance Service, Air Force Industrial Fund (AFMC), local manufacture and commercial vendors
- Aggregation Code:
- AH
- LGM-30 MINUTEMAN
- Price Validation Code:
- N
- The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of āLā or āFā, then it must be evaluated locally where purchased or fabricated.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
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Freight Information 5306-00-488-6528
5306-00-488-6528 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). 5306-00-488-6528 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5306-00-488-6528 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. 5306-00-488-6528 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. 5306-00-488-6528 is not classified as a special type of cargo when transported by water. 5306-00-488-6528 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.
Contracting Technical Data File (CTDF) 5306-00-488-6528 February 2021
Criticality and Quality
- Critical Item Code:
- X
- Flight Safety:
- Life Support:
- Certified Samples:
- Serialization:
- First Article Test (FAT):
- Certificate of Quality Compliance:
- Production Lot Testing:
- Special Testing:
- Qualified Products List (QPL):
Commercial Properties
- Government Furnished Material:
- Government Furnished Tooling:
- Government Furnished Property:
- Price Evaluation Code:
- Diminshing Manufacturing Sources:
- Warranty:
- Commerical Off The Shelf (COTS):
- End Item Application:
- Auctioning Candidate:
- Source of Procurement:
- Contract Option:
Restrictions
- Boeing Rights Guard:
- Export Controlled:
- Controlled Technical Data Package (TDP):
- Restricted Technical Data Package (TDP):
- Contains Classified Material
- Weapons System Indicator Code (WSIC):
- F
Packaging Requirements
- Packaging Determination Table:
- Packaging Review Code:
- N
- Special Packaging Instruction Number (SPIN):
- Special Packaging Instruction Number Revision:
- Special Packaging Instruction Number Date:
- Pallet Reference Number Required: