Model: 746106

Turbine Compressor Stator Flange

Properties:

General Description
Steel ams 5613, rockwell b scale hardness 90 max, 20.530 in.Min 20.570 in. Max od, 19.380 in. Min 19.400 in. Max id, 1.105 in.Min 1.155 in. Max thk
Fsc Application Data
Tf 30 turbine engine, acft
NSN
2840-00-563-9609
Part Number
746106
Description
Flange,compressor Stator,turbine
CAGE
77445

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:
PQ
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
593
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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