FTE7026-4-3-5V

Headless Shoulder Pin

NSN 5315-01-494-5131

DEMIL
Shelf Life
UOM
NIIN
Demil:
NO
Shelf Life:
N/A
UOM:
1 EA
NIIN:
014945131

Product Features

Heat treat to 160 ksi min

Product Technical Spec.

First End Style:
Chamfered
Second End Style:
Chamfered
Thread Class:
3a
Thread Direction:
Right-hand
Thread Length:
0.370 inches
Shank Length:
0.430 inches
Shoulder Width Across Flats:
0.375 inches
Shank Diameter:
Between 0.214 inches and 0.219 inches
Overall Length:
Between 1.127 inches and 1.132 inches
End Application:
F-22 raptor
First End Taper Length:
0.170 inches
Second End Relationship With First End:
Not identical
Thread Size:
0.190 inches
Second Shank Diameter:
Between 0.187 inches and 0.189 inches
First End Location:
Tapered end
First End Tip Radius:
0.070 inches
Second End Taper Angle:
45.0 degrees
Second Shank Length:
0.188 inches
Part Name Assigned By Controlling Agency:
Index pin, 10-32unjf-3a
Material:
Titanium alloy uns r56400
Material Specification:
Ams 4928 assn standard single material response or ams 4967 assn standard single material response
Style Designator:
Shoulder
Thread Series Designator:
Unjf
NSN:
5315-01-494-5131
Item Name:
Pin,index
Cage Code:
58974

Cross Referenced Parts

No other part numbers with same form, fit, and function found.

Part Identification

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
16749
FIIG:
A212A0
Concept No.:
App. Key:
AR
Cond. Code:
1
Status:
A

Part Materials

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
FR
CRITL:
X

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Index Pin"

A cylindrically-shaped headless item, having a shank at one or both ends. It is used for aligning, fastening, or transfer of torque and/or thrust by fitting into corresponding holes of another item. It may be threaded on one end.

MOE Major Organizational Entities

Entity
DSOR
User:
DEPARTMENT OF THE AIR FORCE Dept. of the Air Force
DSOR:

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