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5120-00-226-2316
Prick Punch
5120002262316 002262316 PWA17363
A round knurled, square, hexagonal or octagonal bodied hand tool having a round tapered section terminating in a tapered needlelike point which is ground to an included angle of approximately 25 degrees to 30 degrees. Excludes PUNCH, CENTER, SOLID; PUNCH, COPPERING. View more Prick Punch
January 2023
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Restrictions 5120-00-226-2316
IUID Required
5120-00-226-2316 is a Prick Punch 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 5120-00-226-2316
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5120-00-226-2316
- US Air Force (FXX4)
- Effective Date:
- 1 Apr 1991
Approved Sources 5120-00-226-2316
- Part Number
- Manufacturer
- Status
- PWA17363
- Manufacturer
- 77445 - Rtx Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 5120-00-226-2316
- Characteristic
- Specifications
- FIIG
- Specifications
- A531R0
- End Item Identification [AGAV]
- Tf33 Engine
- Overall Length [ABHP]
- 6.625 Inches Maximum
- Part Name Assigned By Controlling Agency [CXCY]
- Punch, Flaring Compressor Blade Pin Retaining Rivet
- Special Features [FEAT]
- Overall Diameter: 0.375 In. Nominal
Management Data 5120-00-226-2316
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Mar 2006
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
Air Force
- Budget:
- Y
- Centrally procured equipment items. They are separate, primary end items (other than the weapon system itself) needed by a user to perform an assigned mission. They are non-expendable items (ERRC NF or ND) which are not consumed in use, and they do not lose their original identity during periods of use by incorporation into, or attachment to another assembly
- Aggregation Code:
- RV
- PRATT & WHITNEY JET ENGINES & COMPONENTS TF-33
- Price Validation Code:
- X
- The current standard price has been validated and the previous price was erroneous.
The item was overpriced and the contractor has refunded the overcharge or DoD activities did not actually pay the previous price. The price paid is within the analyzed acceptable range.
If the difference from the previous price exceeds $99.99 or if the price change exceeds 500 percent and the extended value of any affected transaction exceeds $99.99, then reverse-post procedures will apply where the stock fund has overcharged unit O&M Funds. These corrections will be limited to the current fiscal year.
ZOP or Standard Price challenges are permissible but should be supported by adequate justification.
- Expendability
Recoverability
Repairability: - U
- Reparable. Condemn at Intermediate. AF Equipment Management System (AFEMS).
NATO Stock Numbers Related to 5120-00-226-2316
Freight Information 5120-00-226-2316
5120-00-226-2316 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 186620. A Sub NMFC of Z. It has a NMFC Description of TOOLS, NOI HAND OTHER THAN POWER. 5120-00-226-2316 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5120-00-226-2316 is rated as class 70 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 91810 which rates the freight between FCL and LCL. It has a Water Commodity Code (WCC) of 732 for ocean manifesting and military sealift. 5120-00-226-2316 is not classified as a special type of cargo when transported by water. 5120-00-226-2316 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.
Packaging Data 5120-00-226-2316
- Responsible Activity
- Packaging Data Source
- Primary Inventory Control Activity (PICA)
- Packaging Data does not meet current MIL-STD-2073-1E
Item Pack Level (Unpackaged)
- Item Size
- Item Weight
- Characteristics
- Weight/Dimensions Category
- Fragility
- Item Preservation
- Item Weight
- --
- --
- --
- --
- --
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- 1
- --
- --
- --
- Preservative Coating Only
- Any Suitable Process
- --
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- MIL-PRF-6529, Type II, Corrosion Preventive, Ready Mixed, for Reciprocating Aircraft Engines
- A-A-3174, Plastic Sheet, Polyolefin, 2mil
- No Requirement
- Not Applicable
- --
- No special marking
- A-A-3174, Plastic Sheet, Polyolefin, 2mil
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- ASTM-D5118, Type CF, Class Domestic, Corrugated Fiberboard Box