Model: ARM2008T3-5

Solid Rivet

Properties:

Fastener Length

Between 0.302 inches and 0.322 inches

Head Style

Flush (flat) countersunk (included angle - less than 135 degrees w or w/o chamfer)

Shank Diameter

Between 0.093 inches and 0.097 inches

Shank Style

Straight w/radius chamfered tip

Head Major Diameter

0.183 inches

Shear Strength

50000 single pounds per square inch

Countersink Angle

Between 99.5 degrees and 100.5 degrees

Heat Treatment

Annealed

Material

Titanium alloy uns r58450

Material Specification

Ams 4982 assn standard single material response

NSN

5320-01-234-3152

Part Number

ARM2008T3-5

Description

Rivet,solid

CAGE

64728

A headed fastening device having a smooth solid shank designed to have the shank end upset after insertion.

Part ARM2008T3-5 NSN 5320-01-234-3152

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

00861

FIIG:

A040A0

Concept No.:

App. Key:

Cond. Code:

Status:

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators

HMIC

PMIC

ESD/EMI

ENAC

MMAC

CRITL

HMIC:

PMIC:

ESD:

MMAC:

CRITL:

Packaging & Shipping

Est. Pack Size

Est. Pack Weight

Est. Item Weight

Est. Item Dim.

Pack Size:

Paclk Weight:

1.0000lbs

Item Weight:

Item Dim:

OPI

SPI No.

SPI Rev.

SPC Mkg.

LVL A

LVL B

OPI:

SPI No.:

SPI Rev.:

SPC Mkg:

LVL_A:

LVL_B:

Freight Classification

NMFC

UFC

LTL

LCL

WCC

TCC

SHC

ACC

NMFC:

096320

UFC:

50430

LTL:

77.5

LCL:

WCC:

713

TCC:

SHC:

ACC:

Construction Materials

End Items End applications NSN 5320-01-234-3152 is a component of

Hornet F/a-18 Aircraft
Harrier Av-8b Aircraft
Airlifter C-17a Aircraft
Pw-100 (c-17a) Aircraft F-117 Engine
B-2 Bomber (atb) Aircraft
F-22 Raptor Air Dominance Fighter
Hornet F/a-18 (e/f) Aircraft

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Schedule B and Export

Schedule B: 8108908000
SITC: 69985
End Use: Nonferrous metals, other
NAICS: 331491
USDA: 1

Freight Class: Other wrought titanium, nesoi