Model: 1-100-287-04

Axial Compressor Disk And Shaft

Properties:

General Description
Isteel ams6382, rockwell c scale 34 min, 37 max hardness, 4.922 in. Min, 4.946 in. Max o/a lg, tapered od disk, 5.927 in. Min, 5.937 in. Max largest od, 5.872 in. Min, 5.882 in. Max smallest od, 0.922 in. Min, 0.924 in. Max w, 31 blade grooves equally spaced on od, first end, 3.456 in. Min, 3.466 in. Max lg from shaft end to disk, second end, 0.544 in. Min, 0.556 in. Max lg from hub end to disk, 4.4180 in. Min, 4.4185 in. Max largest hub od, 10 holes drilled longitudinally through hub, 0.319 in. Min, 0.323 in. Max dia, counterbored 0.533 in. Min, 0.543 in. Max diameter by 0.220 in. Depth, holes equally spaced on 3.560 in. Nom bolt circle dia, first end first complement, external thd 1.750 in. -16 un cl 3a thd, 0.356 in. Min, 0.376 in. Max thd lg (incl thd relief), first end second complement, external spline, 45 teeth, 30 degrees pressure angle, 0.163 in. Min, 0.173 in. Max spline lg, 1.9137 in. Min, 19167 in. Max od, 1.8750 in. Nom pitch dia, 0.506 in. Min, 0.526 in. Max distance from shaft end to spline
NSN
2840-00-898-9124
Part Number
1-100-287-04
Description
Disk And Shaft,axial Compressor
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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