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3110-00-142-4315

Airframe Ball Bearing

3110001424315 001424315 AN200KS5 KS5 AN200KS5MILG3278A AN200KS5ANG25 KS5ANG25 KS5FS160 N16B5007-20

A cylindrical item in which the inner or outer ring turns upon row(s) of hardened BALL, BEARING which roll on a raceway, thus minimizing friction. These items are characterized by their noncorrosive qualities, lightness of weight, inch dimensions rather than metric, inner rings generally projecting beyond the faces of the outer ring, or a very narrow width inner ring having an outside diameter slightly larger than the bore diameter. Designed primarily for use in aircraft assemblies, such as control systems and surfaces of aircraft. Excludes BEARING, BALL, ANNULAR. View more Airframe Ball Bearing

3110-00-142-4315 BEARING,BALL,AIRFRAME 3110001424315 001424315

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
November 2023
NATO Update Count
37
NATO Data Quality
STYL Style 198 for 3110-00-142-4315 1/1
NSN 3110-00-142-4315 (Identification) 1/1

3110-00-142-4315 Stock and Availability Marketplace 3110-00-142-4315

3110-00-142-4315 Related Documents Related Documents 3110-00-142-4315 5+ Documents (More...)

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AN200KS5 26DR543 A cylindrical item in which the inner or outer ring turns upon row(s) of hardened BALL
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619-1295 Airframe Ball Bearing 3110996191295 996191295 Active) Canceled/Obsolete RNCC 5 RNVC 9 DAC X KS5
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Airframe Ball Bearing 3110001424315 001424315 030-1471 Part NumberManufacturerStatus16223-KS5 https

3110-00-142-4315 Demil Restrictions 3110-00-142-4315

DEMIL: A | DEMILI: | CRITICALITY: X | HMIC: N | PMIC: U | EDC: | ADPEC:

3110-00-142-4315 is a Airframe Ball Bearing that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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.

3110-00-142-4315 HTS and ScheduleB Import and Export 3110-00-142-4315

3110-00-142-4315 End Users End Users 3110-00-142-4315

Brazil (YA01)
Effective Date:
1 Jan 2011
Israel (YD01)
Effective Date:
1 Apr 1991
Singapore (YJ01)
Effective Date:
1 Apr 1991
Malaysia (YW01)
Effective Date:
1 Aug 1997
Thailand (YY01)
Effective Date:
1 Feb 2015
New Zealand (ZE01)
Effective Date:
1 Apr 1991
Republic of Korea (ZH01)
Effective Date:
1 Apr 1991
United Kingdom (ZK01)
Effective Date:
1 Nov 1994
Netherlands (ZN01)
Effective Date:
1 Apr 1991
Portugal (ZP01)
Effective Date:
1 Apr 1991
Italy (ZR01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Apr 1991
Turkey (ZW01)
Effective Date:
1 Nov 1998

3110-00-142-4315 Manufacturers Approved Sources 3110-00-142-4315

3110-00-142-4315 Technical Data Datasheet 3110-00-142-4315

Characteristic
Specifications
FIIG
A044A0
Alignment Type [AGZA]
Self-Aligning
Bore Diameter [ABXV]
0.3120 Inches Minimum And 0.3125 Inches Maximum
Material [MATT]
Steel Comp E52100 Overall
Outer Ring Width [AGVT]
0.3700 Inches Minimum And 0.3750 Inches Maximum
Inner Ring Width [AGVU]
0.5530 Inches Minimum And 0.5580 Inches Maximum
Load Direction [AGZC]
Radial
Lubrication Material Document And Classification [LMDC]
Mil-G-3278 Mil Spec Single Material Response
Lubrication Material [ADZG]
Grease
Self-Alignment Location [AHAW]
Internal
Shield Quantity [AGYK]
2
Special Features [FEAT]
10.0 Degree Self Alignment In Either Direction
Overall Outside Diameter [ADGA]
1.2495 Inches Minimum And 1.2500 Inches Maximum
Style Designator [STYL]
Single Row Self Aligning Single Row Inner Ring Extended Both Sides
Surface Treatment [SFTT]
Cadmium All External/Exposed Metal Surfaces

3110-00-142-4315 Related Items NATO Stock Numbers Related to 3110-00-142-4315

3110-00-142-4315 Freight Data Freight Information 3110-00-142-4315

3110-00-142-4315 has freight characteristics.. 3110-00-142-4315 has a variance between NMFC and UFC when transported by rail and the description should be consulted.