16W187-23

View detailed technical data, stock status, and sourcing information for: 16W187-23
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Federal Supply Group

Aerospace Craft and Structural Components

Federal Supply Classification

1560 Airframe Structural Components

National Stock Number

1560-01-438-7355

Item Name Code

32243

Assigment Date

11/18/1996 (29 years ago)

A high strength, 160,000 pounds per square inch (1100 megapascals) minimum tensile strength externally threaded fastener designed for use in applications involving great shear stress. The head is designed to accommodate an external wrench or driver. The head is not designed to be held or driven with an inserted driver, nor is it designed for rotation by the thumb and fingers. The unthreaded portion is of specific grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001) of an inch (0.025 mm) or less of a specific diameter for items one inch (25 mm) or less in diameter. Items over one inch (25 mm) in diameter shall have a tolerance of fifteen ten thousandths (0.0015) of an inch (0.038 mm) or less. The nominal major diameter of the threads shall be at least one thousandth (0.001) of an inch (0.025 mm) below the minimum shank diameter, but not below the minimum major diameter for applicable class of fit, as shown in the screw thread standards, fed std h28 and/or other nationally recognized standards. A locking feature may be incorporated in the design of the head or threads. See bolt, machine and bolt, clevis.

0.063 inches nominal material thickness, 5.000 inches nominal overall width, 82.000 inches nominal overall length, wing root aircraft location, left side side for which designed

Product Characteristics

Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.

Overall Length: 82.000 inches nominal
Overall Width: 5.000 inches nominal
Material Thickness: 0.063 inches nominal
Side For Which Designed: left side
Aircraft Location: wing root
Aircraft Mission Design Series: f-16 c/d
Special Features: nha 16w2050;dwg. name,support,details,fairing-wing root,bl41.5
Material: aluminum alloy 2024
Material Document And Classification: qq-a-250/4-t62 fed spec 1st material response

Related Parts

This NSN group includes multiple components designed to meet specific performance and operational standards. Each listing provides detailed specs, functionality data, and replacement compatibility information:

Part Number	Name
16W187-23	Air Structural Component Support

FAQs

Find helpful answers about installation, operation, maintenance, compliance, and troubleshooting.

What is the FSCG of the NSN 1560-01-438-7355?

The FSCG of the NSN 1560-01-438-7355 is 1560

Does the NSN 1560-01-438-7355 have a Schedule B code assigned?

Yes, the Schedule B code is 8807909060

Does NSN 1560-01-438-7355 require demilitarization?

"commerce control list items (ccli) - mut to the point of scrap required outside the united states. Inside the united states, mut is required when the demil integrity code (ic) is "3" and mut is not required when the demic is "6" (note 8)"

Does NSN 1560-01-438-7355 contain precious materials?

Item does not contain precious metal.

Does NSN 1560-01-438-7355 contain hazardous materials?

Indicates there is no information in the hmirs. The nsn is in a fsc in table ii of fed std 313 and a msds may be required by the user. The requirement for a msds is dependent on a hazard determination of the supplier or the intended end use of item.

When the NSN 1560-01-438-7355 was assigned to the Federal Catalog?

It was assigned 29 years ago, on Mon, Nov 18, 1996