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3120-01-563-8845
Sleeve Bushing
3120015638845 015638845 MS14237A05P031 AS14237
A tubular shaped unthreaded item with or without a flange at one end designed to be inserted into a hole to reduce the inside diameter of the hole and to protect the surrounding body structure from damage resulting from stress, strain, and/or vibration. The overall length must exceed 25 percent of the outside diameter or the shortest distance between peripheral flats of the body. Includes items which are divided into two or more segments which includes 180 degrees (3.141 radians) or less of the bearing periphery. For items made of rubber, see BUSHING, NONMETALLIC. See also BEARING, SLEEVE; BUSHING, TAPERED; SPACER, SLEEVE; INSULATOR, BUSHING; and BUSHING, ELECTRICAL CONDUCTOR. Excludes BUSHING, DRILL, JIG. View more Sleeve Bushing
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Related Documents 3120-01-563-8845 5+ Documents (More...)
/fsg-31/fsc-3120/us
AS14237 BUSHING,SLEEVE 280 EA NS Request Quotation Updated Every Day 3120-01-563-8845 RQST NE Updated
Every Day 3120-01-563-8845 RQST Updated Every Day 3120-01-563-8845 RQST NE Related Documents 3120-01
/fsg-31/fsc-3120/us
MS14237C07-042 AS14237 A tubular shaped unthreaded item with or without a flange at one end designed
MS14237B04P017 A tubular shaped unthreaded item with or without a flange at one end designed SAE-AS14237
/fsg-31/fsc-3120/us
MS14237C07P044 AS14237 A tubular shaped unthreaded item with or without a flange at one end designed
MS14237B04P017 A tubular shaped unthreaded item with or without a flange at one end designed SAE AS14237
/fsg-31/fsc-3120/us
MS14237A07D023 AS14237 A tubular shaped unthreaded item with or without a flange at one end designed
MS14237B04P017 A tubular shaped unthreaded item with or without a flange at one end designed SAE-AS14237
/fsg-31/fsc-3120/us
AS14237 MS14237C03-100 A tubular shaped unthreaded item with or without a flange at one end designed
MS14237B04P017 A tubular shaped unthreaded item with or without a flange at one end designed SAE-AS14237
Restrictions 3120-01-563-8845
3120-01-563-8845 is a Sleeve Bushing 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 3120-01-563-8845
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 3120-01-563-8845
- US Air Force (FBB5)
- Effective Date:
- 1 May 2008
Approved Sources 3120-01-563-8845
- Part Number
- Manufacturer
- Status
- AS14237
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- MS14237A05P031
- 0U583 - Sae International (Active)
- Primary Buy
- Primary Buy
- AS14237
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- MS14237A05P031
- 96906 - Military Standards (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- MS14237A05P031
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 3120-01-563-8845
- Characteristic
- Specifications
- FIIG
- Specifications
- A045A0
- End Item Identification [AGAV]
- C-17A Aircraft
- Body Inside Diameter [ADAS]
- 0.2990 Inches Minimum And 0.3070 Inches Maximum
- Body Outside Diameter [ADAR]
- 0.4388 Inches Minimum And 0.4393 Inches Maximum
- Corner Shape [BZLX]
- Chamfered All Corners
- Material Document And Classification [MDCL]
- Qq-C-530, Condition H.T. Fed Spec Single Material Response Overall
- Material [MATT]
- Copper Alloy Overall
- Overall Length [ABHP]
- 0.3050 Inches Minimum And 0.3100 Inches Maximum
- Style Designator [STYL]
- Solid, Plain, No Outside Flanges
- Surface Finish [CSYM]
- 125.0 Microinches Overall
- Surface Treatment Document And Classification [STDC]
- Qq-P-416, Type Ii, Class 2 Fed Spec Single Treatment Response Overall
- Surface Treatment [SFTT]
- Cadmium Overall
Management Data 3120-01-563-8845
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Nov 2018
- 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 3120-01-563-8845
3120-01-563-8845 has freight characteristics.. 3120-01-563-8845 has a variance between NMFC and UFC when transported by rail and the description should be consulted.