Model: 6895010

Turbine Support Assembly

Properties:

General Description
Cres ams5383 and ams5512, 5 struts, 8.420 in. Min, 8.500 in. Max od front flange, 24 holes 0.217 in. Min, 0.225 in. Max diameter equally spaced on 7.750in. Nom bolt circle dia, 5 bosses equally spaced on 3.830 in. Nom dia, 8.170in. Nom od rear flange, 23 holes 0.217in. Min, 0.225 in. Max diameter equally spaced on the basis of 24 holes on 7.940 in. Nom bolt circle dia, 1 hole 0.194 in. Min, 0.196 in. Max dia, 5 holes 0.210 in. Min, 0.215 in. Max diameter equally spaced on 3.900 in. Nom bolt circle dia
NSN
2840-01-034-4328
Part Number
6895010
Description
Support Assembly,turbine
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:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
139780
UFC:
70190
LTL:
125.0
LCL:
125.0
WCC:
576
TCC:
Z
SHC:
9
ACC:
Construction Materials

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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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