1560-01-708-7014

Find complete technical information, availability, and procurement data for: 1560-01-708-7014
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Federal Supply Group

Aerospace Craft and Structural Components

Federal Supply Classification

1560 Airframe Structural Components

National Stock Number

1560-01-708-7014

Item Name Code

31495

Assigment Date

04/18/2023 (3 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.

27.900 inches nominal overall length, pressure seal and emp shield lower aft avionic door aircraft location, feat criticality code justification, b1-b aircraft end item identification, retainer part name assigned by controlling agency

Product Characteristics

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

Overall Length: 27.900 inches nominal
End Item Identification: b1-b aircraft
Criticality Code Justification: feat
Part Name Assigned By Controlling Agency: retainer
Aircraft Location: pressure seal and emp shield lower aft avionic door
Aircraft Mission Design Series: b1-b aircraft
Special Features: this drawing contains hardness critical item(hci)or hardness critical processes(hcp)all changes to items or processes annotated on the drawing or parts list must be evaluated for hardness impact;finish-003 through-010 aluminum alloy details per l0000024 11ab;
Material: aluminum alloy 2024

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
L3010232-006	Aircraft Structural Plate
PL L3010232	Aircraft Structural Plate

FAQs

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

What is the FSCG of the NSN 1560-01-708-7014?

The FSCG of the NSN 1560-01-708-7014 is 1560

Does the NSN 1560-01-708-7014 have a Schedule B code assigned?

Yes, the Schedule B code is 8803909060

Does NSN 1560-01-708-7014 require demilitarization?

Usml or ccl military items - demil required. Destroy item and components to prevent restoration or repair to a usable condition. (note 5).

Does NSN 1560-01-708-7014 contain precious materials?

Item does not contain precious metal.

Does NSN 1560-01-708-7014 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 1560-01-708-7014 was assigned to the Federal Catalog?

It was assigned 3 years ago, on Tue, Apr 18, 2023