Model: 2-121-058-09

Turbine Engine Turbine Disk

Special Features:

Cres, m3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 9.910 in. Min od, 4.005 in. Min, 4.015 in. Max bore dia, 1.090 in. Min, 1.110 in. Max thk, 72 blade grooves equally spaced.

Properties:

End Application
T-55 series engines
General Description
Cres, m3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 9.910 in. Min od, 4.005 in. Min, 4.015 in. Max bore dia, 1.090 in. Min, 1.110 in. Max thk, 72 blade grooves equally spaced
NSN
2840-00-119-1100
Part Number
2-121-058-09
Description
Disk,turbine,turbine Engine
CAGE

Inc 61686 cancelled/replaced by ,inc 50572, fiig a10700, app-key g ,inc 50571, fiig a10700, app-key g ,on 021513 ~(all except usa). An item having provisions (generally machined slots) on the outer periphery for attaching turbine blades, having features for assembling a disk on a hub or shaft in a designated mating arrangement.

Part 2-121-058-09 NSN 2840-00-119-1100

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
61686
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:
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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