Model: 2-121-051-08

Turbine Eng Turbine Disk And Hub

Special Features:

Cres, m3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 10.370 in. Min, 10.380 in. Max o/a dia, 3.915 in. Min, 3.925 in. Max o/a w, 80 blade grooves equally spaced, internally splined hub, 106 teeth, 30 degrees pressure angle, 3.3125 in. Pitch dia

Properties:

General Description
1cres, m3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 10.370 in. Min, 10.380 in. Max o/a dia, 3.915 in. Min, 3.925 in. Max o/a w, 80 blade grooves equally spaced, internally splined hub, 106 teeth, 30 degrees pressure angle, 3.3125 in. Pitch dia
NSN
2840-00-779-3854
Part Number
2-121-051-08
Description
Disk And Hub,turbine,turbine Eng
CAGE
99193

Inc 61833 cancelled/replaced by ,inc 50566, fiig a10700, app-key f ,inc 50565, fiig a10700, app-key f ,on 021513 ~(all except usa). A disk having provisions on the outer periphery for attaching turbine blades and an integral hub that provides support for the turbine and/or a means of attachment for a shaft. See also disk,turbine,turbine engine.

Part 2-121-051-08 NSN 2840-00-779-3854

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
61833
FIIG:
A23900
Concept No.:
App. Key:
A
Cond. Code:
2
Status:
C

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:
F

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
132560
UFC:
61410
LTL:
77.5
LCL:
85.0
WCC:
593
TCC:
Z
SHC:
R
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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