5310-14-405-2016

Flat Washer

5310144052016 144052016 E27611D50AEUL 401088 4111-21 4111-2100

A washer having a centrally located hole with a solid or laminated cross-section and two flat parallel bearing surfaces. The hole must be 75 percent or less than the largest dimension and the bearing surface finish is greater than 32 microinch (0.8 micrometer). The thickness cannot exceed 25 percent of the largest outside dimension. When the largest outside dimension is less than 1/4 inch or 6mm, the thickness must be 0.006 inches (0.15mm) or greater and for items 1/4 inch (6mm) or larger, the thickness must be 0.016 inches (0.4mm) or greater. The maximum tolerance is applied to dimensions and used as a determining factor. Items with separable lamination use SHIM. For items fabricated from ceramic or electrically rated materials by specification or industry standards use INSULATOR (1), WASHER. Excludes DISK, VALVE, graphite impregnated and lubricated items. View more Flat Washer

5310-14-405-2016 WASHER,FLAT 5310144052016 144052016

Managed by France
NSN Created on 27 Nov 1985
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
5310-14-405-2016 WASHER,FLAT 5310144052016 144052016 1/1
NSN 5310-14-405-2016 (Generic Image) 1/1

5310-14-405-2016 Stock and Availability Marketplace 5310-14-405-2016

Need Help?
Request a Quotation from participating marketplace vendors
eBay Updated Every Day
5310-14-405-2016 RQST NE eBay
eBay Updated Every Day
5310-14-405-2016 RQST eBay
Amazon Updated Every Day
5310-14-405-2016 RQST NE Amazon

5310-14-405-2016 Related Documents Related Documents 5310-14-405-2016 5+ Documents (More...)

1560-01-621-1158 1560016211158 016211158 is a device of various shapes to be permanently attached to the structure of an aircraft. it is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. it may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. excludes items which are primarily designed for dampening shock and/or vibration. excludes bracket, angle; bracket, double angle; bracket, shelf; bracket, mounting; bracket (1), structural component, aircraft; and radius block.
1560-01-656-1051 1560016561051 016561051 is a preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. it is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. it may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. it may be mounted by means of fasteners, bonding or welding. excludes panel, interior lining, aircraft; cover access; cover, access, aircraft; floor (1), aircraft; core material, cellular, structural.
enable JavaScript in your web browser . 1660-14-217-3505Bouchon Prise De Pr1660142173505 142173505 401088
your web browser . 4520-23-114-2143Immersion Type Electrical Heating Element4520231142143 231142143 401088
JavaScript in your web browser . 4710-00-246-5717Metal Tube Assembly4710002465717 002465717 CV21-401088
your web browser . 4520-23-114-2143Immersion Type Electrical Heating Element4520231142143 231142143 401088
JavaScript in your web browser . 4710-00-246-5717Metal Tube Assembly4710002465717 002465717 CV21-401088
Approved Sources 4710-00-246-5717 Part NumberManufacturerStatusCV21-401088-1 80378 - Triumph Aerostructures
$1 a day Upgrade your Account Upgrade 5985-00-773-6169Electrical Dummy Load5985007736169 007736169 401088
JavaScript in your web browser . 4710-00-246-5717Metal Tube Assembly4710002465717 002465717 CV21-401088
-1 Approved Sources 4710-00-246-5717 Part NumberManufacturerStatusCV21-401088-1 80378 - Triumph Aerostructures

5310-14-405-2016 Related Items NATO Stock Numbers Related to 5310-14-405-2016