Model: 7082M24P04
Turbine Engine PadProperties:
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 indicatorsHMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
PL
CRITL:
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