Model: 1-100-135-03

Turbine Rotor Sealing Disk

Properties:

End Application
T-53 series engines
General Description
Cres m3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 9.820 in. Nom o/a od, 5.590 in. Min, 5.600 in. Max od hub, one land 5.731 in. Min, 5.733 in. Max od located on hub, 0.020 in. Min, 0.030 in. Max land tip, 6 holes 0.356 in. Min, 0.363 in. Max diameter countersunk 90 degrees to 0.390 in. Diameter equally spaced on 5.000 in. Diameter bolt circle on hub, 6 holes 0.280 in. Diameter located inside 6 slots 0.380 in. W equally spaced on 5.000 in. Diameter flange bolt circle
NSN
2840-00-925-2972
Part Number
1-100-135-03
Description
Disk,turbine Rotor Sealing
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:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
RATING VARIABLE
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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