Model: 1-100-242-09

Aircraft Gas Turbin Turbine Disk

Special Features:

Steel, ams4135, black chromic anodized finish, 6.570 in. Min, 6.580 in. Max o/a od, 1.637 in. Nom o/a lg, 4.082 in. Min, 4.087 in. Max id, 34 blade grooves equally spaced on outer peripwery, 34 holes 0.094 in. Min, 0.097 in. Max diameter by 0.095 in. Min, 0.105 in. Max depth equally spaced on groove centerlines

Properties:

Overall Length
1.637 inches
Diameter
Between 6.570 inches and 6.580 inches
End Application
T-53 series engines
Design Type
Axial compressor
Engine Section Location
Compressor
Material
Steel
Material Specification
Ams 4135 assn standard single material response
Surface Treatment
Anodize
NSN
2840-00-157-2375
Part Number
1-100-242-09
Description
Disk,turbine,aircraft Gas Turbin
CAGE
99193

An item having provisions on the outer periphery for attaching a designated number of blade, turbine rotor, aircraft gas turbine engine. It also has provisions for attachment to a hub, turbine, aircraft gas turbine engine.

Part 1-100-242-09 NSN 2840-00-157-2375

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50571
FIIG:
A10700
Concept No.:
App. Key:
G
Cond. Code:
1
Status:
A

Material Classification

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

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
92.5
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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