Model: 7082M24P04

Turbine Engine Pad

Properties:

End Application
Aircraft eng j-79
General Description
Steel ams 5510 or 5645, 1.840 min in. 1.880 max in. Sq, 0.250-28unf-3b for 4 holes, 0.380 min in. 0.384 max in. Diameter of center hole
NSN
2840-01-133-5999
Part Number
7082M24P04
Description
Pad,turbine Engine
CAGE

Material Classification

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

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