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5340-01-526-1004
Clamp Bolt Assembly
5340015261004 015261004 HD12026-106
A threaded item having an eye on one end designed to accommodate a hinge pin, or a pin inserted at right angles to the shank. It must have an adjusting nut assembled on the threads. The end of the threads may be headed, or a cap nut or similar device attached to prevent disassembly of the adjusting nut. It may also have a washer, collar or retainer assembled between the nut and hinge mounted end. Includes items having a bracket or lug mounting. It is used to rigidly clamp items to a structure, instrument, or the like. View more Clamp Bolt Assembly
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Restrictions 5340-01-526-1004
5340-01-526-1004 is a Clamp Bolt 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 may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.
Import and Export 5340-01-526-1004
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5340-01-526-1004
- US Air Force (FBB5)
- Effective Date:
- 1 Dec 2004
Approved Sources 5340-01-526-1004
- Part Number
- Manufacturer
- Status
- HD12026-106
- Manufacturer
- 0CBU7 - Howmet Global Fastening Systems Inc (Active)
- Primary Buy
- Primary Buy
Datasheet 5340-01-526-1004
- Characteristic
- Specifications
- FIIG
- Specifications
- A03100
- Material [MATT]
- Aluminum Alloy 2024 Nut
- Material Document And Classification [MDCL]
- Qq-A-200/3 Fed Spec Single Material Response Nut
- Surface Treatment [SFTT]
- Anodize Nut
- Surface Treatment Document And Classification [STDC]
- Mil-A-8625,Type Iii,Class 1 Mil Spec Single Treatment Response Nut
- Style Designator [STYL]
- Wing No. 5
- Mounting Method [AXGY]
- Pin
- Mounting Facility Quantity [AKPV]
- 1
- Mounting Facility Diameter [CLMQ]
- 0.160 Inches Nominal
- Thread Series Designator [THSD]
- Unf
- Nominal Thread Size [CQJX]
- 0.312 Inches
- Thread Quantity Per Inch [CMLP]
- 24
- Thread Class [AAJD]
- 2A
- Thread Direction [AAJF]
- Right-Hand
- Thread Length [AASA]
- 2.910 Inches Nominal
- Overall Diameter [CSZK]
- 1.000 Inches Nominal
- Special Features [FEAT]
- Clevis Bolt Made Of 17-4 Cres,Lock Down Nut Has Racheting Locking Teeth
- End Item Identification [AGAV]
- C-17A Spt Equip
Management Data 5340-01-526-1004
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Dec 2004
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- BA
- C-17 PROGRAM
- 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).
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Freight Information 5340-01-526-1004
5340-01-526-1004 has freight characteristics.. 5340-01-526-1004 has a variance between NMFC and UFC when transported by rail and the description should be consulted.