Model: 2-141-073-14

Turbine Bearing Support Housing

Properties:

End Application
T-55 series engines
General Description
Titanium alloy, annealed, m3400; rockwell c scale 36 max hardness; 4.724 in. Min, 4.725 in. Max id; 6.839 in. Min, 6.840 in. Max od; 2.163 in. Min, 2.167 in. Max lg; 3 holes, 0.220 in. Diameter on 6.370 in. Boltcircle dia; 2 holes, 0.310 in. Min, 0.317 in. Max diameter on 5.300 in.Boltcircle dia; 20 holes 0.280 in. Diameter on 5.250 in. Bolt circle dia
NSN
2840-00-152-3789
Part Number
2-141-073-14
Description
Housing,turbine Bearing Support
CAGE
99193

Material Classification

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

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
013120
UFC:
05380
LTL:
100.0
LCL:
100.0
WCC:
576
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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